N8324A

Part: FRAME — DEBONDED (ZONE 300) · airframe 43,055 hrs · 20,418 cycles

LEFT CONDUCTIVE FRAME AT RUDDER WAS DISBONDED REF TLD 25-155-03112 TTG8Q018TDJK. REMOVED 6.125 IN. SECTION OF DISBONDED LOWER CONDUCTIVE FRAME AT RUDDER TE IAW SRM 55-40-01-1A-3. REMOVED SIX RIVETS AT RUDDER TE TO FOM IAW SRM 51-40-02. PERFORMED PERMANENT REPAIR BY REMOVAL OF DISBONDED SECTION OF RUDDER CONDUCTIVE FRAME IAW SRM 55-40-01-1A-3. PERFORMED BALANCE BY CALCULATION METHOD AND FOUND NEW SBHM TO BE +497.195; WITHIN BALANCE WINDOW LIMITS, NO BALANCE WT CHANGE REQUIRED.

Part: HANDLE — LOOSE (ZONE 800) · airframe 41,565 hrs · 19,617 cycles

CUSTOMER WALK ITEM: L1 DOOR AFT AIRFRAME ASSIST HANDLE NEEDS SECURED. SECURED L1 DOOR AFT ASSIST HANDLE IAW B737-800 AMM 25-21-31-420-802.

Part: SKIN — DELAMINATED (ZONE 500 FLAP) · airframe 41,565 hrs · 19,617 cycles

LT. OUTBD AFT FLAP UPPER SURFACE DELAMINATED ON INBD. END<[01] 01 - REMOVED AND REPLACED PER [AMM 27-51-22-400-801-NG (OUTBOARD AFT FLAP INSTALLATION - PERMANENT)];[02] VERIFIED REMOVED AND REPLACED PER [AMM 27-51-22-400-801-NG (OUTBOARD AFT FLAP INSTALLATION - PERMANENT)

Part: CIRCUIT BREAKER — TRIPPED (ZONE 200) · airframe 40,290 hrs · 18,954 cycles

CABIN EMER LIGHTS C.B. TRIPPED CONTACTED CRAIG IN M.O.C. RESET BREAKER SYSTEM RESTORED TO NORMAL. CABIN EMER LIGHTS C.B. TRIPPED CONTACTED CRAIG IN M.O.C RESET BREAKER SYSTEM RESTORED TO NORMAL.<[01] NOTED BY MX.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 39,549 hrs · 18,568 cycles

L1 & L2 EXTERIOR SLIDE EMERGENCY LIGHTS INOP<[01] RELAMPED L1 & L2 EXTERIOR SLIDE EMERGENCY LIGHTS IAW AMM 33-51-04. OPS CHECK GOOD @ THIS TIME.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

REPLACE INTERCOSTAL WEB LOCATED BTW BS500F AND BS500G AND LBL21 W156 AT FWD CARGO COMPARTMENT DUE TO EXISTING REPAIR ON SUPPORT ZEE NOT MEETS SPACING FASTENER HOLES REQUIREMENTS GIVEN ON EA M-22-153-0 2024-512618 REPLACE INTERCOSTAL WEB LOCATED BTW BS500F AND BS500G AND LBL21 W156 AT FWD CARGO COMPARTMENT DUE TO EXISTING REPAIR ON SUPPORT ZEE NOT MEETS SPACING FASTENER HOLES REQUIREMENTS GIVEN ON EA M-22-153-01550 AND SRM 53-00-53-2R-5 REPAIR 5<[01] ON STEP 3; EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210136503; DUE DATE: 24-JUL-25;[02] REPLACED WEB INTERCOSTAL LOCATED BTW BS500F AND BS500G AND LBL21 W156 AT FWD CARGO COMPARTMENT IAW B737-800 SRM 53-30-53-2R-1 REPAIR 1 STEP 4. P TO L AND DWG: 143A7505; SHEET: 108; REV: -; SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED WEB INTERCOSTAL LOCATED BTW BS500F AND BS500G AND LBL21 W156 AT FWD CARGO COMPARTMENT IAW B737-800 SRM 53-30-53-2R-1 REPAIR 1 STEP 4. P TO L AND DWG: 143A7505; SHEET: 108; REV: -; SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED

Part: WINGLET — CORRODED (ZONE 500) · airframe 39,062 hrs · 18,292 cycles

CORROSION WINGLET TIP AT LT WING 2024-512594<[01] REPAIRED WINGLET TIP AT LT WING I.A.W B737-800 SRM 57-30-01 REPAIR 6. SEE INDIVIDUAL SIGNS OFF BELOW;[02] REPAIRED WINGLET TIP AT LT WING I.A.W B737-800 SRM 57-30-01 REPAIR 6. SEE INDIVIDUAL SIGNS OFF BELOW

Part: STRINGER — CORRODED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CORROSION ON STR 27R LOCATED BTW BS 360 TO 380 RBL 15.75 WL 159 AT ELECTRONIC COMPARTMENT 2024-512589<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130064101; CAL DUE DATE: 13-DEC-24;[02] TOOL USED ON STEP 9: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 60009161631 DUE DATE: 11-MAR-25;[03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 23-JAN-25.;[04] PERFORMED PERMANENT REPAIR ON STR27R BTW BS360 TO BS380 MOR 9' RBL15.75 WL159 AT ELECTRONIC COMPARTMENT I.A.W. B737-800 SRM 53-00-03-2R-1. <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[05] CORRECTED STEP 4<BR>PERFORMED PERMANENT REPAIR ON STR27R BTW BS360 TO BS380 MORE 9' RBL15.75 WL159 AT ELECTRONIC COMPARTMENT I.A.W. B737-800 SRM 53-00-03-2R-1.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[06] PERFORMED PERMANENT REPAIR ON STR27R BTW BS360 TO BS380 MORE 9' RBL15.75 WL159 AT ELECTRONIC COMPARTMENT I.A.W. B737-800 SRM 53-00-03-2R-1.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: ANGLE — CORRODED (ZONE 600) · airframe 39,062 hrs · 18,292 cycles

CORROSION INBOARD TRAILING EDGE BONDING JUMPER SUPPORT ANGLE OF AFT BOOST PUMP TANK 2 AT RT WING (2 EA) 2024-512553<[01] REPLACED INBOARD TRAILING EDGE BONDING JUMPER SUPPORT ANGLE OF AFT BOOST PUMP TANK 2 AT RT WING (2 EA) IAW B737-800 AMM 28-22-41-400-801. STEP 3.H.(18);(20);(21);(22). AND PERFORMED RESISTANCE TEST IS OK. TOOL USED: BONDING METER PN:M1 MILLIOHM METER; S/N:DC007485;DUE DATE:29 JUL 25.;[02] REPLACED INBOARD TRAILING EDGE BONDING JUMPER SUPPORT ANGLE OF AFT BOOST PUMP TANK 2 AT RT WING (2 EA) IAW B737-800 AMM 28-22-41-400-801. STEP 3.H.(18);(20);(21);(22). AND PERFORMED RESISTANCE TEST IS OK.

Part: ANGLE — CORRODED (ZONE 500) · airframe 39,062 hrs · 18,292 cycles

CORROSION RETAINER SEAL ANGLE TRAILING EDGE AT LEVEL SPOILER 1 LT WING 2024-512557<[01] REPLACED RETAINER SEAL ANGLE TRAILING EDGE AT LEVEL SPOILER 1 LT WING I.A.W B737-800 SRM 51-40-02-0G-0 AND DWG# 115A3551; SHEET 3; REV.-.;[02] CERTIFIED CORRECTIVE ACTION STEP 1

Part: BALANCE WEIGHT — OUT OF BALANCE (ZONE 300) · airframe 39,062 hrs · 18,292 cycles

DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR RT PN:183A0103-26 SN:006115 FOUND BALANCE WEIGHTS PN:183A0210-15 (1 EA) ON BAY 4 PN:183A0210-14 (1 EA) ON BAY 3 PN:183A0210-14 (1 EA) ON BAY 2 2024-512560<[01] ACCOMPLISHED ELEVATOR BALANCING IAW EA M-22-155-03767;[02] ACCOMPLISHED ELEVATOR BALANCING IAW EA M-22-155-03767<BR>RII CERTIFIED

Part: SUPPORT ANGLE — CRACKED (ZONE 500) · airframe 39,062 hrs · 18,292 cycles

CRACK SUPPORT ANGLE FIXED TRAILING EDGE ORSS 297 LT WING 2024-512538<[01] REPLACED SUPPORT ANGLE LOCATED FIXED TRAILING EDGE ORSS 297 LT WING IAW B737-800 SRM 51-40-02 AND DWG 115A3700 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ANGLE LOCATED FIXED TRAILING EDGE ORSS 297 LT WING IAW B737-800 SRM 51-40-02 AND DWG 115A3700 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.

Part: NUT PLATE — CORRODED (ZONE 500 LE) · airframe 39,062 hrs · 18,292 cycles

CORROSION O/B FIXED LEADING EDGE RAIL NUTPLATE OFSS 449 AT LT WING 2024-512523<[01] REPLACED O/B FIXED LEADING EDGE RAIL NUTPLATE OFSS 449 AT LT WING IAW B737-800 SRM 51-40-02 AND DWG: 112A4402; SHEET: 40; REV: A.;[02] REPLACED O/B FIXED LEADING EDGE RAIL NUTPLATE OFSS 449 AT LT WING IAW B737-800 SRM 51-40-02 AND DWG: 112A4402; SHEET: 40; REV: A.

Part: PLATE — CRACKED (ZONE 600) · airframe 39,062 hrs · 18,292 cycles

CRACK CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 218 RT WING 2024-512522<[01] TOOK MEASURE OF CRACK IS : 0.275? ON CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 218 RT WING; TOOL USED :CALIPER P/N: 500-197-30; S/N: A18135108; DUE DATE: 12 -JUL-25. EVALUATED DAMAGE AND NOT FOUND ALLOWED DAMAGE LIMITS IAW B737-800 SRM 57-51-01-1A-1 ALLOWABLE DAMAGE 1.<BR>REPLACED CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 218 RT WING IAW B737-800 SRM 51-40-02; SRM 51-10-02; ITEM 9 AND DWG: 115A2713; SHEET: 6; REV: A;[02] TOOK MEASURE OF CRACK IS : 0.275? ON CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 218 RT WING; TOOL USED :CALIPER P/N: 500-197-30; S/N: A18135108; DUE DATE: 12 -JUL-25. EVALUATED DAMAGE AND NOT FOUND ALLOWED DAMAGE LIMITS IAW B737-800 SRM 57-51-01-1A-1 ALLOWABLE DAMAGE 1.<BR>REPLACED CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 218 RT WING IAW B737-800 SRM 51-40-02; SRM 51-10-02; ITEM 9 AND DWG: 115A2713; SHEET: 6; REV: A

Part: RETAINER — CORRODED (ZONE 500) · airframe 39,062 hrs · 18,292 cycles

CORROSION RETAINER SEAL ANGLE OUTBOARD TRAILING EDGE AT LEVEL SPOILER 3 LT WING 2024-512513<[01] REPLACED RETAINER SEAL ANGLE OUTBOARD TRAILING EDGE AT LEVEL SPOILER 3 LT WING I.A.W B737-800 SRM 51-40-02-0G-0 AND DWG# 115A3551; SHEET 5; REV.-.;[02] CERTIFIED CORRECTIVE ACTION STEP 1

Part: STRINGER — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK STRINGER 26L BS 540 AT FWD CARGO COMPARTMENT 2024-512501<[01] TOOL USED ON STEP 3: P/N: 45MG; S/N: 221860711; DUE DATE: 21-NOV-24.;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 23-JAN-25.;[03] ON STEP 9; TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[04] PERFORMED PERMANENT REPAIR ON STRINGER 26L LOCATED BTW BS500I MORE 7 INCHES TO BS540 AT FWD CARGO COMPARTMENT I.A.W B737-800 SRM 53-00-03-2R-1. SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED PERMANENT REPAIR ON STRINGER 26L LOCATED BTW BS500I MORE 7 INCHES TO BS540 AT FWD CARGO COMPARTMENT I.A.W B737-800 SRM 53-00-03-2R-1. SEE INDIVIDUAL SIGN OFF BELOW. JOB COMPLETED.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE - SUPPORT BS 500I AND STRINGER 28L FWD CARGO COMPARTMENT 2024-512502<[01] REPLACED ANGLE LOCATED BS 500I AND STRINGER 28L FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902; SHEET 160; REV: B; SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE LOCATED BS 500I AND STRINGER 28L FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902; SHEET 160; REV: B; SEE INDIVIDUAL SIGN OFF BELOW.

Part: RETAINER — CORRODED (ZONE 600) · airframe 39,062 hrs · 18,292 cycles

CORROSION RETAINER SEAL ANGLE OUTBOARD TRAILING EDGE AT LEVEL SPOILER 10 AT RT WING 2024-512511<[01] REPLACED RETAINER SEAL ANGLE OUTBOARD TRAILING EDGE AT LEVEL SPOILER 10 AT RT WING IAW B737-800 SRM 51-40-02 AND DWG: 115A3551; SHEET: 5; REV: -;[02] CERTIFIED CORRECTIVE ACTION 1; COMPLETED

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE - SUPPORT BS 500I AND STRINGER 28R FWD CARGO COMPARTMENT 2024-512503<[01] REPLACED SUPPORT ANGLE LOCATED BS 500I AND STRINGER 28R FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902; SHEET 160; REV: B.;[02] CORRECTION ACTION 1<BR>REPLACED SUPPORT ANGLE LOCATED BS 500I AND STRINGER 28R FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902; SHEET 160; REV: B; SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED SUPPORT ANGLE LOCATED BS 500I AND STRINGER 28R FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902; SHEET 160; REV: B; SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK PNEUMATIC DUCT SUPPORT BRACKET BS 540 AND LBL 6 AIR CONDITIONING BAY 2024-512487<[01] REPLACED PNEUMATIC DUCT SUPPORT BRACKET BS 540 AND LBL 6 AIR CONDITIONING BAY IAW B737-800 SRM 51-40-02-0G-0. ITEM 9.;[02] REPLACED PNEUMATIC DUCT SUPPORT BRACKET BS 540 AND LBL 6 AIR CONDITIONING BAY IAW B737-800 SRM 51-40-02-0G-0. ITEM 9.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ON SUPPORT BRACKET LOCATED BS867 BTW STR2R AND STR3R AT PASSENGER CABIN 2024-512481<[01] REPLACED SUPPORT BRACKET LOCATED BS867 BTW STR2R AND STR3R AT PASSENGER CABIN I.A.W B737-800 SRM 51-40-02 AND DWG 146A7901 SHEET 66 REV ?A? MEASURE OF CRACK IS: L=0.400 TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N:B23343124 DUE DATE: 09-MAR-25;[02] TASK COMPLETED

Part: WEB — CRACKED (ZONE 500) · airframe 39,062 hrs · 18,292 cycles

CRACK WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING 2024-512484<[01] REPLACED WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2512 SHEET 16 REV-. <BR><BR>MEASURE OF CRACK IS: L 1.500? TOOL USED: ELECTRONIC CALIPER P/N: 500-196-30; S/N: A193117227 AND DUE DATE: 23-MAY-25.;[02] CORRECTED STEP 1<BR>REPLACED WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2512 SHEET 16 REV-. <BR><BR>MEASURE OF CRACK IS: L 1.500? TOOL USED: ELECTRONIC CALIPER P/N: 500-196-30; S/N: A19317227 AND DUE DATE: 23-MAY-25.;[03] REPLACED WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2512 SHEET 16 REV-. <BR><BR>MEASURE OF CRACK IS: L 1.500? TOOL USED: ELECTRONIC CALIPER P/N: 500-196-30; S/N: A19317227 AND DUE DATE: 23-MAY-25.

Part: ANGLE — CRACKED (ZONE 500) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE TRAILING EDGE ORSS 277 DEFLECTION CONTROL RIB AREA LT WING 2024-512485<[01] REPLACED ANGLE TRAILING EDGE ORSS 277 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A2512 SHEET 16 REV-.<BR><BR>MEASURE CRACK IS: L: 0.450?. TOOL USED ELECTRONIC CALIPER P/N: 500-196-30; S/N: A19317227 AND DUE DATE: 23-MAY-25.;[02] REPLACED ANGLE TRAILING EDGE ORSS 277 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A2512 SHEET 16 REV-.<BR><BR>MEASURE CRACK IS: L: 0.450?. TOOL USED ELECTRONIC CALIPER P/N: 500-196-30; S/N: A19317227 AND DUE DATE: 23-MAY-25.

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN 2024-512458<[01] REPLACED TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN I.A.W. B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 141A1110 SHEET: 39; REV: -; AND DWG: 141A8380; SHEET: 21; REV: - SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN I.A.W. B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 141A1110 SHEET: 39; REV: -; AND DWG: 141A8380; SHEET: 21; REV: - <BR>SEE INDIVIDUAL SIGN OFF BELOW.<BR>CERTIFIED AS RII.

Part: ANGLE — CRACKED (ZONE 200) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE LOCATED STA294.5 AND RBL53 WL208.1 AT PASSENGER CABIN 2024-512460<[01] REPLACED ANGLE LOCATED STA294.5 AND RBL53 WL208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 141A8310; SHEET: 33; REV: - ; SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE LOCATED STA294.5 AND RBL53 WL208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 141A8310; SHEET: 33; REV: - ; SEE INDIVIDUAL SIGN OFF BELOW.

Part: BRACKET — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK BRACKET BULKHEAD BS 727 AND RBL3 AFT CARGO COMPARTMENT 2024-512437<[01] REPLACED BRACKET LOCATED ON BS727 RBL3 AT AFT COMPARTMENT IAW B737-800 SRM 51-40-02 AND DRW 144A2600 SHEET 1084 REV. - DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM B7377-800 <BR><BR>CRACK LENGTH: 1.00? <BR><BR>TOOL USED CALIPER P/N: 500-197-30 S/N: 15120588 DUE DATE: 24/NOV/24;[02] CORRECTED STEP 1<BR>REPLACED BRACKET LOCATED ON BS727 RBL3 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DRW 144A2600 SHEET 1084 REV. - THIS BRACKET WAS REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM B7377-800 <BR><BR>CRACK LENGTH: 1.00? <BR><BR>TOOL USED CALIPER P/N: 500-197-30 S/N: 15120588 DUE DATE: 24/NOV/24;[03] REPLACED BRACKET LOCATED ON BS727 RBL3 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DRW 144A2600 SHEET 1084 REV. - THIS BRACKET WAS REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM B7377-800 <BR><BR>CRACK LENGTH: 1.00? <BR><BR>TOOL USED CALIPER P/N: 500-197-30 S/N: 15120588 DUE DATE: 24/NOV/24

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE - CLIP LOCATED STA500G AND RBL21 AFT POSITION FWD CARGO COMPARTMENT 2024-512409<[01] TOOK MEASURE OF CRACK IS : 0.267' ON ANGLE - CLIP LOCATED STA500G AND RBL21 AFT POSITION FWD CARGO COMPARTMENT TOOL USED : ELECTRONIC CALIPER P/N: 500-752-20; S/N: B21034763; DUE DATE: 03-OCT-24. EVALUATED DAMAGE AND NOT FOUND ALLOWED DAMAGE LIMITS IAW B737-800 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.<BR><BR>REPLACED ANGLE - CLIP LOCATED STA500G AND RBL21 AFT POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG: 143A7505; SHEET: 109; REV: -;[02] TOOK MEASURE OF CRACK IS : 0.267' ON ANGLE - CLIP LOCATED STA500G AND RBL21 AFT POSITION FWD CARGO COMPARTMENT TOOL USED : ELECTRONIC CALIPER P/N: 500-752-20; S/N: B21034763; DUE DATE: 03-OCT-24. EVALUATED DAMAGE AND NOT FOUND ALLOWED DAMAGE LIMITS IAW B737-800 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.<BR><BR>REPLACED ANGLE - CLIP LOCATED STA500G AND RBL21 AFT POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG: 143A7505; SHEET: 109; REV: -

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE - CLIP LOCATED STA500F AND RBL21 AFT POSITION FWD CARGO COMPARTMENT 2024-512411<[01] REPLACED ANGLE - CLIP LOCATED STA500F AND RBL21 AFT POSITION FWD CARGO COMPARTMENT AND FASTENERS IAW B737-800 SRM 51-40-02 AND SRM 51-10-02; ITEM 9 .DWG: 143A7505; SHEET:109; REV: - .SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE - CLIP LOCATED STA500F AND RBL21 AFT POSITION FWD CARGO COMPARTMENT AND FASTENERS IAW B737-800 SRM 51-40-02 AND SRM 51-10-02; ITEM 9 .DWG: 143A7505; SHEET:109; REV: - .SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE - CLIP LOCATED STA500H AND RBL21 FWD POSITION FWD CARGO COMPARTMENT 2024-512407<[01] TOOK MEASURE OF CRACK IS : 0.750? ON ANGLE - CLIP LOCATED STA500H AND RBL21 FWD POSITION FWD CARGO COMPARTMENT TOOL USED :CALIPER P/N: 500-197-30; S/N: B23316997; DUE DATE: 14-JAN-25. EVALUATED DAMAGE AND NOT FOUND ALLOWED DAMAGE LIMITS IAW B737-800 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2. <BR>REPLACED ANGLE - CLIP LOCATED STA500H AND RBL21 FWD POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02; ITEM 9 AND DWG: 143A7505; SHEET: 108; REV: -.;[02] TOOK MEASURE OF CRACK IS : 0.750? ON ANGLE - CLIP LOCATED STA500H AND RBL21 FWD POSITION FWD CARGO COMPARTMENT TOOL USED :CALIPER P/N: 500-197-30; S/N: B23316997; DUE DATE: 14-JAN-25. EVALUATED DAMAGE AND NOT FOUND ALLOWED DAMAGE LIMITS IAW B737-800 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2. <BR>REPLACED ANGLE - CLIP LOCATED STA500H AND RBL21 FWD POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02; ITEM 9 AND DWG: 143A7505; SHEET: 108; REV: -.

Part: GUSSET — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ON GUSSET LOCATED BS500I AND STR19R AT FWD CARGO COMPARTMENT 2024-512413<[01] REPLACED GUSSET LOCATED BS500I AND STR19R AT FWD CARGO COMPARTMENT AND FASTENERS IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 256 AND REV-B. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED GUSSET LOCATED BS500I AND STR19R AT FWD CARGO COMPARTMENT AND FASTENERS IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 256 AND REV-B. SEE INDIVIDUAL SIGN-OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE - CLIP LOCATED BS500G AND LBL21 AFT POSITION FWD CARGO COMPARTMENT 2024-512408<[01] REPLACED ANGLE - CLIP LOCATED BS500G AND LBL21 AFT POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM: 51-10-02 ITEM 9 AND DWG: 143A7505; SHEET: 108; REV: -; SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE - CLIP LOCATED BS500H AND LBL21 FWD POSITION FWD CARGO COMPARTMENT 2024-512406<[01] REPLACED ANGLE-CLIP LOCATED ON BS500H AND LBL21 FWD POSITION AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET:21 REV.: B <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE-CLIP LOCATED ON BS500H AND LBL21 FWD POSITION AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET:21 REV.: B<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE - CLIP LOCATED STA500G AND LBL21 FWD POSITION FWD CARGO COMPARTMENT 2024-512454<[01] REPLACED ANGLE - CLIP LOCATED STA500G AND LBL21 FWD POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM: 51-10-02 ITEM 9 AND DWG: 143A7505; SHEET: 108; REV: -;[02] CORRECTION ACTION 1<BR>REPLACED ANGLE - CLIP LOCATED STA500G AND LBL21 FWD POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM: 51-10-02 ITEM 9 AND DWG: 143A7505; SHEET: 108; REV: -; SEE INDIVIDUAL SIGN OFF BELOW.;[03] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN STA500B TO STA500G AND RBL21 WL156 AT FWD CARGO COMPARTMENT 2024-512419<[01] PERFORMED PERMANENT REPAIR ON SUPPORT ZEE LOCATED BETWEEN STA500A TO STA500I AND RBL21 WL156 AT FWD CARGO COMPARTMENT I.A.W B737-800 SRM SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550. SEE INDIVIDUAL SIGN OF BELOW.;[02] CORRECTED STEP 1<BR>PERFORMED PERMANENT REPAIR ON SUPPORT ZEE LOCATED BETWEEN STA500A TO STA500I AND RBL21 WL156 AT FWD CARGO COMPARTMENT I.A.W B737-800 SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CERTIFIED CORRECTIVE ACTION 2 AS RII <BR>PERFORMED PERMANENT REPAIR ON SUPPORT ZEE LOCATED BETWEEN STA500A TO STA500I AND RBL21 WL156 AT FWD CARGO COMPARTMENT I.A.W B737-800 SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550. SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE - CLIP LOCATED BS500H AND LBL21 AFT POSITION FWD CARGO COMPARTMENT 2024-512405<[01] REPLACED ANGLE-CLIP LOCATED ON BS500H AND LBL21 AFT POSITION AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET:21 REV.: B<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE-CLIP LOCATED ON BS500H AND LBL21 AFT POSITION AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET:21 REV.: B<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK TIE CLIP LOCATED STA500I AND STR26R FWD CARGO COMPARTMENT 2024-512418<[01] REPLACED TIE CLIP LOCATED ON BS500I STR26R AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A1234 SHEET 13 REV. A<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED TIE CLIP LOCATED ON BS500I STR26R AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A1234 SHEET 13 REV. A<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] STEP 2 CORRECTED<BR>REPLACED TIE CLIP LOCATED ON BS500I STR26R AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A1234 SHEET 13 REV. A<BR>SEE INDIVIDUAL SIGN-OFF BELOW<BR><BR>CERTIFIED AS RII

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE - CLIP LOCATED STA500E AND RBL21 FWD CARGO COMPARTMENT 2024-512424<[01] REPLACED ANGLE - CLIP LOCATED STA500E AND RBL21 FWD CARGO COMPARTMENT AND FASTENERS IAW B737-800 SRM 51-40-02 AND DWG: 143A7505; SHEET: 108; REV: -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE - CLIP LOCATED STA500E AND RBL21 FWD CARGO COMPARTMENT AND FASTENERS IAW B737-800 SRM 51-40-02 AND DWG: 143A7505; SHEET: 108; REV: -. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE - CLIP LOCATED STA500H AND RBL21 AFT POSITION FWD CARGO COMPARTMENT 2024-512404<[01] TOOK MEASURE OF CRACK IS : 0.360' ON ANGLE - CLIP LOCATED STA500H AND RBL21 AFT POSITION FWD CARGO COMPARTMENT TOOL USED : DIGITAL CALIPER P/N: 500-197-30; S/N: B23316997; DUE DATE: 14-JAN-25. EVALUATED DAMAGE AND NOT FOUND ALLOWED DAMAGE LIMITS IAW B737-800 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.<BR><BR>REPLACED ANGLE - CLIP LOCATED STA500H AND RBL21 AFT POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02;SRM 51-10-02; ITEM 9 AND DWG: 143A7505; SHEET: 109; REV: -;[02] CERTIFIED CORRECTIVE ACTION 1

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE - CLIP LOCATED STA500G AND RBL21 FWD POSITION FWD CARGO COMPARTMENT 2024-512410<[01] TOOK MEASURE OF CRACK IS : 0.298' ON ANGLE - CLIP LOCATED STA500G AND RBL21 FWD POSITION FWD CARGO COMPARTMENT TOOL USED : ELECTRONIC CALIPER P/N: 500-752-20; S/N: B21034763; DUE DATE: 03-OCT-24. EVALUATED DAMAGE AND NOT FOUND ALLOWED DAMAGE LIMITS IAW B737-800 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.<BR><BR>REPLACED ANGLE - CLIP LOCATED STA500G AND RBL21 FWD POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG: 143A7505; SHEET: 20; REV: B;[02] TOOK MEASURE OF CRACK IS : 0.298' ON ANGLE - CLIP LOCATED STA500G AND RBL21 FWD POSITION FWD CARGO COMPARTMENT TOOL USED : ELECTRONIC CALIPER P/N: 500-752-20; S/N: B21034763; DUE DATE: 03-OCT-24. EVALUATED DAMAGE AND NOT FOUND ALLOWED DAMAGE LIMITS IAW B737-800 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.<BR><BR>REPLACED ANGLE - CLIP LOCATED STA500G AND RBL21 FWD POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG: 143A7505; SHEET: 20; REV: B

Part: BRACKET — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK BRACKET BS 947.5 AND LBL 10 AFT CARGO COMPARTMENT 2024-512438<[01] REPLACED BRACKET BS 947.5 AND LBL 10 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 149A8103 SHEET 8 REV-.<BR><BR>MEASURE CRACK IS: L: 1.213?. TOOL USED: DIGITAL CALIPER P/N: 500-752-20 S/N: B21034763 AND DUE DATE: 03-OCT-24.;[02] REPLACED BRACKET BS 947.5 AND LBL 10 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 149A8103 SHEET 8 REV-.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE - SUPPORT BS 727B AND LBL 52 CEILING AREA AFT CARGO COMPARTMENT 2024-512427<[01] PERFORMED PERMANENT REPAIR ON ANGLE - SUPPORT BTW BS 727A TO BS 727C AND LBL 52 CEILING AREA AFT CARGO COMPARTMENT IAW B737-800 SRM 51-70-11-2R-0 <BR><BR>SEE INDIVIDUAL SGN-OFF BELOW;[02] PERFORMED PERMANENT REPAIR ON ANGLE - SUPPORT BTW BS 727A TO BS 727C AND LBL 52 CEILING AREA AFT CARGO COMPARTMENT IAW B737-800 SRM 51-70-11-2R-0 <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: SUPPORT — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK SUPPORT ZEE LOCATED BETWEEN STA500E TO STA500F AND LBL21 WL156 AT FWD CARGO COMPARTMENT 2024-512420<[01] PERFORMED PERMANENT REPAIR ON SUPPORT ZEE LOCATED BETWEEN STA 500D TO STA500I AND LBL21 WL156 AT FWD CARGO COMPARTMENT I.A.W 737-800 SRM 53-00-53-2R-5 REPAIR 5 AND EA M-22-153-01550. SEE INDIVIDUAL SIGN OF BELOW.;[02] PERFORMED PERMANENT REPAIR ON SUPPORT ZEE LOCATED BETWEEN STA 500D TO STA500I AND LBL21 WL156 AT FWD CARGO COMPARTMENT I.A.W 737-800 SRM 53-00-53-2R-5 REPAIR 5 AND EA M-22-153-01550. SEE INDIVIDUAL SIGN OF BELOW<BR>RII CERTIFIED

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE - CLIP LOCATED STA500F AND RBL21 FWD POSITION FWD CARGO COMPARTMENT 2024-512412<[01] REPLACED ANGLE - CLIP LOCATED STA500F AND RBL21 FWD POSITION FWD CARGO COMPARTMENT I.A.W B737-800 SRM 51-10-02 ITEM (9) SRM 51-40-02 AND DWG 143A7505 SHEET 20 REV ?B? SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 200) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA380 TO STA400 AND LBL13 AT PASSENGER CABIN 2024-512372<[01] REPLACED ANGLE LOCATED ON FLOOR STRUCTURE BETWEEN STA 380 TO STA 400 AND LBL 13 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 143A5400 SHEETS: 138 AND 142; REV: -; SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE LOCATED ON FLOOR STRUCTURE BETWEEN STA 380 TO STA 400 AND LBL 13 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 143A5400 SHEETS: 138 AND 142; REV: -; SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 39,062 hrs · 18,292 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED STA540 AND RBL2 AT PASSENGER CABIN 2024-512373<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATED STA540<BR>AND RBL2 AT PASSENGER CABIN AND FASTENERS I.A.W B737-<BR>800 SRM 51-40-02 AND DWG: 143A0060 SHEET: 64 REV: - SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE FLOOR STRUCTURE LOCATED STA540<BR>AND RBL2 AT PASSENGER CABIN AND FASTENERS I.A.W B737-<BR>800 SRM 51-40-02 AND DWG: 143A0060 SHEET: 64 REV: - SEE INDIVIDUAL SIGN OFF BELOW

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 39,062 hrs · 18,292 cycles

CORROSION INTERCOSTAL FLOOR STRUCTURE LOCATED STA947.5 AND RBL50 WL208.1 AT AFT GALLEY AREA 2024-512297<[01] REPLACED INTERCOSTAL FLOOR STRUCTURE LOCATED STA947.5 AND STA967 AND RBL50 WL208.1 AT AFT GALLEY AREA AND FASTENERS I.A.W B737-800 SRM 51-40-02 AND DWG: 147A5650 SHEET: 70 REV: A; SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,062 hrs · 18,292 cycles

CORROSION FLOOR BEAM STRUCTURE LOCATED STA986.5 AND RBL43 WL208.1 AT AFT GALLEY AREA 2024-512299<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 60009161631; DUE DATE: 11-MAR-25;[02] STEP 10 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210138003; CAL DUE DATE: 11-JUN-25;[03] REPAIRED FLOOR BEAM STRUCTURE LOCATED STA986.5 AND RBL43 WL208.1 AT AFT GALLEY AREA IAW B737-800 SRM-53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4 FIG. 205. SEE INDIVIDUAL SIGN-OFF BELOW.;[04] CERTIFIED REPAIR PER STEP 3<BR>RII ACCOMPLISHED

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 39,062 hrs · 18,292 cycles

INOP EMERGENCY EXIT LIGHT BATTERY PACK ON POSITION RH AND LH SIDE AFT LOWERED CEILING AT AFT GALLEY AREA 2024-512243<[01] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK ON POSITION RH AND LH SIDE AFT LOWERED CEILING AT AFT GALLEY AREA IAW B737-800 AMM 33-51-06-960-805;[02] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK ON POSITION RH AND LH SIDE AFT LOWERED CEILING AT AFT GALLEY AREA IAW B737-800 AMM 33-51-06-960-805<BR>TEST IS OK

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 39,062 hrs · 18,292 cycles

INOP BATTERY PACK EMERGENCY EXIT LIGHT ON LOWER WEB AREA POSITION RH SIDE BTW STA 727C TO 727D AT PASSENGER CABIN 2024-512244<[01] REPLACED BATTERY PACK EMERGENCY EXIT LIGHT ON LOWER WEB AREA POSITION RH SIDE BTW STA 727C TO 727D AT PASSENGER CABIN IAW B737-800 AMM 33-51-06-960-805.<BR>TEST IS OK;[02] CORRECTED STEP 1.<BR>REPLACED BATTERY PACK EMERGENCY EXIT LIGHT ON LOWER WEB AREA POSITION RH SIDE BTW STA 727C TO 727D AT PASSENGER CABIN IAW B737-800 AMM 33-51-06-960-805.<BR>TEST IS OK. SEE INDIVIDUAL SIGNS OFFS BELOW;[03] REPLACED BATTERY PACK EMERGENCY EXIT LIGHT ON LOWER WEB AREA POSITION RH SIDE BTW STA 727C TO 727D AT PASSENGER CABIN IAW B737-800 AMM 33-51-06-960-805.<BR>TEST IS OK. SEE INDIVIDUAL SIGNS OFFS BELOW

Part: WEB — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK WEB LOCATED ON FLOOR STRUCTURE BTW BS277 TO BS294.5 BL0 AT FWD GALLEY AREA 2024-512230<[01] REPLACED WEB AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS277 TO BS294.5 BL0 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING: 141A5400 SHEET : 20 REV: -; SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS277 TO BS294.5 BL0 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING: 141A5400 SHEET : 20 REV: -; SEE INDIVIDUAL SIGN OFF BELOW

Part: STRUCTURE — CRACKED (ZONE 200) · airframe 39,062 hrs · 18,292 cycles

CRACK INNER CHORD LOCATED BS 294.5 PLUS 8.5 INCHES; LBL 55 FWD GALLEY AND LAV 2024-512212<[01] REPLACED INNER CHORD LOCATED BS 270 TO BS 360 AND LBL 56 FWD GALLEY AREA IAW B737-800 SRM 51-40-02; DWG: 141A8110; REV: A; SHEET: 9 AND DWG: 141A8110; REV: -; SHEET: 11. SEE INDIVIDUAL SIGN OFF BELOW.;[02] JOB COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW. RII

Part: WEB — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK WEB LOCATED ON FLOOR STRUCTURE BTW BS312 TO BS328 LBL45 AT FWD GALLEY AREA 2024-512231<[01] REPLACED WEB AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS312 TO BS328 LBL45 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING: 141A5400 SHEET: 26 REV: -; SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS312 TO BS328 LBL45 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING: 141A5400 SHEET: 26 REV: -; SEE INDIVIDUAL SIGN OFF BELOW

Part: WEB — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK WEB LOCATED ON FLOOR STRUCTURE BTW BS312 TO BS328 LBL45 AT FWD GALLEY AREA 2024-512231<[01] REPLACED WEB AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS312 TO BS328 LBL45 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING: 141A5400 SHEET: 26 REV: -; SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS312 TO BS328 LBL45 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING: 141A5400 SHEET: 26 REV: -; SEE INDIVIDUAL SIGN OFF BELOW

Part: WEB — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

CRACK WEB LOCATED ON FLOOR STRUCTURE BTW BS277 TO BS294.5 BL0 AT FWD GALLEY AREA 2024-512230<[01] REPLACED WEB AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS277 TO BS294.5 BL0 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING: 141A5400 SHEET : 20 REV: -; SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS277 TO BS294.5 BL0 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING: 141A5400 SHEET : 20 REV: -; SEE INDIVIDUAL SIGN OFF BELOW

Part: LENS — CRACKED (ZONE 200) · airframe 39,062 hrs · 18,292 cycles

CRACK CEILING PANEL EMERGENCY LIGHT LENS ROW 29 RH AT PASSENGER CABIN 2024-512165<[01] REPLACED CEILING PANEL EMERGENCY LIGHT LENS ROW 29 RH AT PASSENGER CABIN I.A.W AMM 33-51-03-960-803. PERFORMED OPERATIONAL TEST IS OK.;[02] CORRECTED STEP 1<BR>REPLACED CEILING PANEL EMERGENCY LIGHT LENS ROW 29 RH AT PASSENGER CABIN I.A.W B737-800 AMM 33-51-03-960-803. PERFORMED OPERATIONAL TEST IS OK.;[03] TASK COMPLETED TEST IS OK

Part: SKIN — DAMAGED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

PERFORM PERMANENT REPAIR ON FUSELAGE SKIN AT STA 932 AND 935 STR 21L 2024-512156<[01] TOOL USED IN STEP 5: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N:60009161631; DUE DATE: 11-MAR-25;[02] PERFORMED REPAIR ON FUSELAGE SKIN BTW BS927 TO BS947.5 AND BTW STR20L TO STR23L AT LOWER FUSELAGE I.A.W. EA 24-153-02387-WIP1 & 24-153-02387-WIP2 AND EA COVER EA 24-153-02387<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] PERFORMED REPAIR ON FUSELAGE SKIN BTW BS927 TO BS947.5 AND BTW STR20L TO STR23L AT LOWER FUSELAGE I.A.W. EA 24-153-02387-WIP1 & 24-153-02387-WIP2 AND EA COVER EA 24-153-02387<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW<BR><BR>CERTIFIED AS RII

Part: LENS — CRACKED (ZONE 200) · airframe 39,062 hrs · 18,292 cycles

CRACK CEILING PANEL EMERGENCY LIGHT LENS ROW 19LH AT PASSENGER CABIN 2024-512163<[01] REPLACED CEILING PANEL EMERGENCY LIGHT LENS ROW 19LH AT PASSENGER CABIN I.A.W B737-800 AMM 33-51-03-960-803. PERFORMED OPERATIONAL TEST IS OK.;[02] TASK COMPLETED TEST IS OK

Part: LENS — CRACKED (ZONE 200) · airframe 39,062 hrs · 18,292 cycles

CRACK CEILING PANEL EMERGENCY LIGHT LENS ROW 21RH AT PASSENGER CABIN 2024-512162<[01] REPLACED CEILING PANEL EMERGENCY LIGHT LENS ROW 21RH AT PASSENGER CABIN I.A.W B737-800 AMM 33-51-03-960-803. PERFORMED OPERATIONAL TEST IS OK.;[02] TASK COMPLETED TEST IS OK

Part: LENS — CRACKED (ZONE 200) · airframe 39,062 hrs · 18,292 cycles

CRACK CEILING PANEL EMERGENCY LIGHT LENS ROW 17 RH AT PASSENGER CABIN 2024-512160<[01] REPLACED CEILING PANEL EMERGENCY LIGHT LENS ROW 17 RH AT PASSENGER CABIN I.A.W B737-800 AMM 33-51-03-960-803. PERFORMED OPERATIONAL TEST IS OK.;[02] TASK COMPLETED <BR>TEST IS OK.

Part: LIGHT — BROKEN (ZONE 200) · airframe 39,062 hrs · 18,292 cycles

BROKEN PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (6EA) 2024-512116<[01] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN IAW B737-800 AMM 33-51-15-960-801;[02] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN IAW B737-800 AMM 33-51-15-960-801

Part: SKIN — DEBONDED (ZONE 600 FLAP) · airframe 39,062 hrs · 18,292 cycles

DEBONDED OB AFT FLAP LOWER SURFACE IB SIDE AT RT WING 2024-512149<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 14-JAN-25.;[02] ON STEP 3: TOOL USED BOND TESTING UNIT PN: BONDMASTER 600M; SN: 220052310; DUE DATE: 17 NOV 24;[03] TOOL USED; HOT BONDER PN: HCS9200B-AV; SN: 18196127; DUE DATE: 25/JAN/25.;[04] TOOL USED; POSITECTOR PN: POSITECTOR 6000 NS3; SN:767584; DUE DATE: 30/AUG/25.;[05] TOOL USED: CALIPER P/N: 500-197-30 S/N: B20189443 DUE DATE: 06-MAR-25.;[06] TOOL USED: COATING THICKNESS GAUGE P/N:POSITECTOR 6000 NS3; S/N:767584; DUE DATE: 30-AUG-25.;[07] TOOL USED: BOND TESTING EQUIPMENT; PN: BONDMASTER 600M; SN: 230106912; DUE DATE: 09-JAN-25.;[08] TOOL USED BOND TESTING UNIT PN: BONDMASTER 600M; SN: 220052310; DUE DATE: 17-NOV-24;[09] PERFORMED INTERIM REPAIR ON OB AFT FLAP LOWER SURFACE IB SIDE AT RT WING IAW B737-800 SRM 57-53-01-2R-16 REPAIR 16 AND THE REPAIR REQUIRED TAP TEST INSPECTION EVERY 6;875 CYC OR 30 MONTHS. SEE INDIVIDUAL SIGNOFFS BELOW.;[10] PERFORMED INTERIM REPAIR ON OB AFT FLAP LOWER SURFACE IB SIDE AT RT WING IAW B737-800 SRM 57-53-01-2R-16 REPAIR 16 AND THE REPAIR REQUIRED TAP TEST INSPECTION EVERY 6;875 CYC OR 30 MONTHS. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

(CUSTOMER REQUEST) CRACK ON LH VAPOR BARRIER LOCATED ON BS663.75 BTW LBL24.92 TO LBL31.83 AT MAIN LANDING GEAR COMPARTMENT 2024-512104<[01] TOOL USED CALIPER P/N 500-197-30 S/N A18229508 DUE DATE 14 JAN 25;[02] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 15-FEB-25.;[03] TOOL USED SCALE P/N: CR5200 S/N: 8342514510 DUE DATE: 24 FEB 25.;[04] TOOL USED HOT BONDER P/N: HCS9200B S/N: 18165044 DUE DATE: 11 APR 25.;[05] TOOL USED: SCALE P/N:CR5200; S/N:8343110774; DUE DATE:28-FEB-25.;[06] TOOL USED HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 11-APR-25.;[07] TOOL USED ON STEP 12 UT EQUIPMENT P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 04-OCT-24;[08] REPAIRED LH VAPOR BARRIER LOCATED ON BS663.75 BTW LBL24.92 TO LBL31.83 AT MAIN LANDING GEAR COMPARTMENT IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW.;[09] REPAIRED LH VAPOR BARRIER LOCATED ON BS663.75 BTW LBL24.92 TO LBL31.83 AT MAIN LANDING GEAR COMPARTMENT IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW. RII COMPLETED

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

(CUSTOMER REQUEST) CRACK ON RH VAPOR BARRIER LOCATED ON BS663.75 BTW RBL25 TO RBL45.64 AT MAIN LANDING GEAR COMPARTMENT 2024-512103<[01] TOOL USED CALIPER P/N 500-197-30 S/N A18229508 DUE DATE 14 JAN 25;[02] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 15-FEB-25.;[03] TOOL USED SCALE P/N: CR5200 S/N: 8342514510 DUE DATE: 24 FEB 25.;[04] TOOL USED HOT BONDER P/N: HCS9200B S/N: 18165044 DUE DATE: 11 APR 25.;[05] TOOL USED: SCALE P/N:CR5200; S/N:8343110774; DUE DATE:28-FEB-25.;[06] TOOL USED HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 11-APR-25.;[07] TOOL USED ON STEP 12 UT EQUIPMENT P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 04-OCT-24;[08] REPAIRED RH VAPOR BARRIER LOCATED ON BS663.75 BTW RBL25 TO RBL45.64 AT MAIN LANDING GEAR COMPARTMENT IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW.;[09] JOB TASK COMPLETED. RII INSPECTION COMPLETED.

Part: DOOR — CRACKED (ZONE 100) · airframe 39,062 hrs · 18,292 cycles

(CUSTOMER REQUEST) CRACK ON RH MAIN LANDING GEAR CENTER DOOR 2024-512107<[01] ON STEP 5; TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[02] PERFORMED PERMANENT REPAIR ON RH MAIN LANDING GEAR CENTER DOOR I.A.W B737-800 SRM 52-80-02-2R-3 REPAIR 3<BR><BR>SEE INIDIVIDUAL SIGN-OFF BELOW;[03] JOB COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,004 hrs · 17,724 cycles

R AFT OVER WING EXIT DOOR FLOOR LEVEL EGRESS SIGN HAS MULTIPLE BULBS INOP<[01] RELAMPED IAW AMM 33-51-01. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,961 hrs · 17,703 cycles

AFT LH EMERGENCY LIGHTS INOP<[01] R&R BATTERY PACK ON POWER SUPPLY M1673 REF AMM 33-51-06

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 37,061 hrs · 17,233 cycles

AFT ENTRY DOOR EXIT/SALIDA LENS MISSING<[01] REPLACED EXIT LENS ON AFT ENTRY DOOR PER AMM 33-51-01

Part: ACCESS PANEL — CORRODED (ZN 100 FUS LOWER) · airframe 36,666 hrs · 17,008 cycles

FWD CARGO DOOR ACCESS PANEL 821 BR SHOWS SIGNS OF CORROSION ACCESS PANEL 821BR SHOWS SIGNS OF CORROSION.<[01] INSTALLED PANEL REF AMM 52-31-00

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 35,094 hrs · 16,129 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED PER AMM 33-51-04

Part: LIGHT — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 34,518 hrs · 15,806 cycles

CABIN LIGHT OVER SEAT 10D IS LOOSE AND HANGING FROM BULKHEAD.<[01] RE-SECURED O/H LT ASSEMBLY @ ROW 10 DEF; FOR GOOD OPS CK. REF. 33-51-00 AMM.;[02] CORRECTED LOG PAGE NUMBER FROM 041202E; TO - 0410202E. PER EMAIL FROM JC INSUA; TPA.;[03] CERTIFIED

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 34,220 hrs · 15,651 cycles

LH HORIZONTAL STABILIZER UPPER FRONT SPAR SLIDING SEAL IS CRACKED.<[01] REMOVED AND REPLACED LH HORIZONTAL STABILIZER UPPER FRONT SPAR SLIDING SEAL PER AMM 53-31-31.

Part: GIRT BAR — OUT OF ADJUST (ZN 800 DOOR) · airframe 34,220 hrs · 15,651 cycles

AFT ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] ADJUSTED AFT ENTRY DOOR SLIDE GIRT IAW AMM SIP;[02] ADJUSTED AFT ENTRY DOOR SLIDE GRIT BAR IAW AMM 25-66-01

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 34,220 hrs · 15,651 cycles

RH HORIZONTAL STABILIZER UPPER FRONT SPAR SLIDING SEAL IS CRACKED.<[01] REMOVED AND REPLACED R/H HORIZONTAL STABILIZER; FRONT SPAR; UPPER SLIDING SEAL IAW BOEING 737 AMM 53-31-31.

Part: WINGLET — DELAMINATED (ZN 500 LEFT WING) · airframe 33,991 hrs · 15,503 cycles

L/H UPPER WING TIP; AFT. DELAM.<[01] REMOVED DELAM PER SRM 57-30-01.<BR>REF. LP# 0463925E FOR PAINT DEFERRAL.

Part: LIGHT — INOPERATIVE (ZN 900 LAV/GALLE) · airframe 33,195 hrs · 15,050 cycles

SUPPLEMENTAL INFORMATION: SIDEWALL LIGHT ABOVE EMERGENCY EXIT DOOR ROW 14 DEF; INOP. / [01] OK TO CONTINUE PER MEL 33-2-04<BR>SP1B;[02] REMOVED AND REPLACED R/H SIDEWALL LIGHT AT ROW 14DEF IAW AMM 33-21-00-960-805. OPS CHECK GOOD. NO OTHER DEFECTS NOTED. THIS CLEARS MEL 33-2-04

Part: LIGHT — INOPERATIVE (ZN 900 LAV/GALLE) · airframe 33,115 hrs · 15,003 cycles

ROW 14A OVER WING EMERGENCY LIGH LENS BROKEN / [01] REMOVED & REPLACED ROW 14A OVER WING EMEREGENCY LIGHT ASSY PER AMM <BR>33-51-01

Part: NONE — DAMAGED · airframe 32,867 hrs · 14,875 cycles

PIECE OF PLASTIC ON EMER EXIT SIGN ON CEILING AT MID CABIN BROKEN / [01] SECURED PIECE OF PLASTIC WITH TAPE <BR>OK TO CONTINUE PER MEL 5-10-01 SP1B AUTHORIZATION NUMBER 91298;[02] SECURED PIECE OF PLASTIC WITH TAPE<BR>OK TO CONTINUE PER MEL 25-10-01 SP1B AUTHORIZATION NUMBER 91298;[03] REMOVED AND REPLACED EMERGENCY EXIT SIGN ACCESS COVER IAW SIP.

Part: BATTERY PACK — INOPERATIVE · airframe 32,619 hrs · 14,746 cycles

LIGHTS ON EMERGENCY EXIT DOORS; FO SIDE INOP / [01] REMOVED AND REPLACED RH OVER WING EXIT EMERGENCY LIGHT POWER SUPPLY EQUIPMENT NUMBER M1695 PER AMM 33-51-06;[02] REMOVED AND REPLACED BATTERY PACK AT CHARGER M1695 PER AMM 33-51-06;[03] REMOVED AND REPLACED RH OVER WING EXIT EMERGENCY LIGHT POWER SUPPLY EQUIPMENT NUMBER M1695 PER AMM 33-51-06. REMOVED AND REPLACED BATTERY PACK AT CHARGER M1695 PER AMM 33-51-06

Part: HANDLE — LOOSE (FWD ENTRY DOOR) · airframe 32,568 hrs · 14,719 cycles

FORWARD ENTRY DOOR ASSIST HANDLE LOOSE. / [01] REMOVED AND REPLACED HARD WEAR ON UPPER ASSIST HANDLE PER AMM 52-11-31.

Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 32,568 hrs · 14,719 cycles

FWD CARGO COMPARTMENT AFT BULK HEAD PANEL SUPPORT LOWER L-ANGLE AT STA. 500I HAS CORROSION. / [01] REMOVED DAMAGED ANGLE PER SRM 51-40-02. REMOVED DAMAGE PER SRM 51-10-02 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. MATCH DRILLED NEW ANGLE PER SRM 51-40-05.;[02] INSTALLED NEW ANGLE PER SRM 51-40-02.;[03] ALL WORK ACCOMPLISHED PER SRM 53-00-53-1A-2 AND SRM 51-40-02.<BR>NO DEFECT NOTED.

Part: FLAP — DELAMINATED (LH WING) · airframe 32,568 hrs · 14,719 cycles

LH OUTBOARD AFT FLAP HAS LARGE DELAMINATION ON THE INBOARD END. / [01] OK TO INSTALL L/H O/B AFT FLAP;[02] REMOVED AND INSTALLED NEW FLAP PER AMM 27-51-26;[03] COMPLIED WITH ADJUSTMENT CHECK AMM 27-51-22;[04] VERIFIED ADJUSTMENT CHECK AMM 27-51-22

Part: FLOOR SUPPORT — CRACKED · airframe 32,568 hrs · 14,719 cycles

CABIN FLOOR SUPPORT CRACKED AT BS540 RBL1. / [01] REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER SRM 51-40-02.;[02] REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER SRM 51-40-02.<BR>RII INSPECTION C/W.

Part: SUPPORT — CRACKED (CABIN FLOOR) · airframe 32,568 hrs · 14,719 cycles

CABIN FLOOR SUPPORT CRACKED AT BS540 LBL1. / [01] REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER SRM 51-40-02.;[02] REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER SRM 51-40-02.<BR>RII INSPECTION C/W.

Part: CHARGER — INOPERATIVE (L/H CABIN) · airframe 32,312 hrs · 14,578 cycles

INTERIOR EMERGENCY EXIT LIGHT ABOVE SEAT 8ABC AND 12ABC INOP AND LEFT FWD EMERGENCY EXIT DOOR LIGHT INOP (OUTSIDE) / [01] R&R M2335 BATTERY PACK AND CHARGER PER AMM 33-51-06. OPS CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (L/H CABIN) · airframe 32,312 hrs · 14,578 cycles

INTERIOR EMERGENCY EXIT LIGHT ABOVE SEAT 8ABC AND 12ABC INOP AND LEFT FWD EMERGENCY EXIT DOOR LIGHT INOP (OUTSIDE) / [01] R&R M2335 BATTERY PACK AND CHARGER PER AMM 33-51-06. OPS CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (L/H OVERWING) · airframe 31,954 hrs · 14,399 cycles

LH OVERWING EXIT EMERGENCY EXIT SIGN & FWD & AFT EXIT LIGHT MODULES LIGHTS INOP / [01] REPLACED BATTERY PACK IN POWER SUPPLY M1694 FOR LH OVERWING EXIT LIGHTS PER AMM 33-51-06. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 30,897 hrs · 13,862 cycles

R2 DOOR AREA EMERGENCY LIGHTS INOP ; / [01] REPLACED M1672 BATTER PACK PER AMM 33-51-06. OPS GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 30,445 hrs · 13,617 cycles

RIGHT AFT OVERWING EXIT LIGHT INOP ; / [01] REMOVED AND REPLACED BOTH EMERGENCY BATTERY PACK CHARGER AND BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 30,445 hrs · 13,617 cycles

RIGHT AFT OVERWING EXIT LIGHT INOP ; / [01] REMOVED AND REPLACED BOTH EMERGENCY BATTERY PACK CHARGER AND BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EXTERIOR EMERGENCY LIGHT AFT OF RIGHT HAND FLAP INOP / RELAMPED PER AMM 33-51-04. OPS CHECK GOOD.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR SLIDE) · airframe 28,468 hrs · 12,746 cycles

L-1 DOOR SLIDE; GIRT BAR; GIRT TOO LONG; NEEDS TO BE REINSTALLED / REPLACED L1 DOOR SLIDE GIRT PER MT725-61-06AMT# 117477INSP# 52251

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 28,424 hrs · 12,718 cycles

ROW 14F FIRST OFFICER SIDE OVERWING EXIT LOWER EMERGENCY EXIT SIGN COVER MISSING. / INSTALLED MISSING LENS COVER AT ROW 14F LOWER EMERGENCY EXIT SIGN IAW AMM 33-51-03. OPS CHK GOOD

Part: ANGLE — CORRODED (BS 727E-727J) · airframe 26,819 hrs · 11,842 cycles

DISCREPANCY TRANSFERRED FROM N/R D165728 TO CORRECT STATION LOCATIONS AFT CARGO; L/H TRANSITION ANGLE HAS CORROSION AROUND NUTPLATE HOLES FROM STA. 727E +10 TO STA 727J + 10 AREAS MARKED / REPLACED L/H TRANSITION ANGLE (SIDE PLATE) P/N 146A7502-31 FROM STA 727-847 PER SRM 51-40-02.. ( PER SAM 326 ATTACHED A1200667)

Part: ANGLE — CORRODED (BS 727J-847) · airframe 26,819 hrs · 11,842 cycles

DISCREPANCY TRANSFERRED FROM N/R D165741 TO CORRECT STATION LOCATIONS. AFT CARG; L/H TRANSITION ANGLE HAS CORROSION AROUND NUTPLATE HOLES FROM STA 727 J + 10 TO STA 847 AREAS MARKED / REPLACED L/H TRANSITION ANGLE (SIDE PLATE) P/N 146A7502-31 FROM STA 727-847 PER SRM 51-40-02 (PER SA-M 326 ATTACHED) A1200668

Part: ANGLE — CORRODED (BS 727-727E) · airframe 26,819 hrs · 11,842 cycles

DISCREPANCY TRANSFERRED FROM N/R D165723 TO CORRECT STATION LOCATIONS AFT CARGO; L/H TRANSITION ANGLE HAS CORROSION AROUND NUTPLATE HOLES FROM STA 727 TO STA 727E +10 AREAS MARKED / REPLACED L/H TRANSITION ANGLE (SIDE PLATE) P/N 146A7502-31 FROM STA 272 - 847; PER SRM 51-40-02. (PER SAM 326 ATTACH A1200666)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,819 hrs · 11,842 cycles

AFT MID CABIN L/H EMERGENCY AISLE LIGHTS INOP / REMOVED AND REPLACED BATTERY PACK PER MM 33-5106. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-00PN OFF D717-01-100 SN OFF 216567 PN ON D717-01-100SWA SN ON 43880

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,819 hrs · 11,842 cycles

FWD GALLEY L/H EMERGENCY LTS INOP / REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-00P/N OFF D717-01-100 SN OFF 216736PN ON D717-01-100SWA SN ON 43780

Part: GUSSET — CRACKED (BS 500I S19R) · airframe 26,819 hrs · 11,842 cycles

FWD CARGO GUSSET CRACKED BS 500I STR 19R / REMOVED & REPLACED FORWARD CARGO GUSSET AT STATION 500I; STR 19 IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (BS 747-767) · airframe 26,819 hrs · 11,842 cycles

AFT CARGO; INTERCOSTAL AT STA 747 TO STA 767; RBL 21 IS CRACKED / INSTALLED INTERCOSTAL AT STA 747 TO 767 RBL 21 PER SRM 51-40-02.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 26,819 hrs · 11,842 cycles

CABIN FLOOR PANEL 241VF HAS DAMAGE. / REMOVED AND REPLACED CABIN FLOOR PANEL 241 VF PER AMM 53-21-00

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 26,819 hrs · 11,842 cycles

CABIN FLOOR PANEL 241WF HAS DAMAGE. / REMOVED AND REPLACED CABIN FLOOR PANEL 241 WF PER AMM 53-21-00

Part: WEB — CORRODED (AFT CARGO) · airframe 26,819 hrs · 11,842 cycles

AFT CARGO ENTRY FLOOR WB HAS CORROSION ON SURFACE IN SEVERAL PLACES / AFT CARGO ENTRY DOOR REMOVED AND REPLACED DOOR SILL WEB PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 771) · airframe 26,819 hrs · 11,842 cycles

AFT CARGO STA. 771 RBL 14; CORROSION ON FLOOR SUPPORT CHANNEL NUTPLATE HOLE. / ACCOMPLISHED REPAIR @ STA 771 RBL 14 IN AFT CARGO IAW SRM 53-00-53-2R-3. (SA-M 326 A1200659)

Part: ANGLE — CRACKED (BS 867) · airframe 26,819 hrs · 11,842 cycles

AFT CARGO 'L' ANGLE CRACKED BS 867 LBL 16 / REMOVED AND REPLACED AFT CARGO 'L' ANGLE AT BS867; LBL 16' PER SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 771) · airframe 26,819 hrs · 11,842 cycles

AFT CARGO STA. 771 RBL 3; CORROSION ON FLOOR SUPPORT CHANNEL NUTPLATE HOLE. / REPAIRED FLOOR BEAM RBL3 STA 771 PER SRM 53-00-53-2R-2 & TASKCARD # 20-153-01438SEE SA-M 326 : A1200658

Part: ANGLE — CORRODED (BS 727J-787) · airframe 26,819 hrs · 11,842 cycles

AFT CARGO STA. 727J TO 787; CORROSION AROUND NUTPLATES HOLES; RT TRANSITION ANGLE / REPLACED TRANSITION ANGLE PER SRM 51-40-02.SEE INDIVIDUAL SIGNOFFS FOR ALL WORK ACCOMPLISHED.SA-M 326 ATTACHED (A1164758)

Part: WEB — CRACKED (NR 1 NACELLE) · airframe 26,819 hrs · 11,842 cycles

#1 ENGINE I/B FAN COWL INTERIOR WEB CRACKED (ENGINE OIL ACCESS). MARKED / R/R #1 ENGINE I/B FAN COWL INTERIOR WEB IAW SRM 51-10-02 AND SRM 51-40-02.

Part: SEAL — CHAFED (HORIZONTL STAB) · airframe 26,819 hrs · 11,842 cycles

GAP PANEL 343 AT SLIDING SEAL CHAFED (R/H HORIZ STAB) / REMOVED & REPLACED SEAL IAW SRM 51-40-02

Part: SEAL — CHAFED (HORIZONTAL STAB) · airframe 26,819 hrs · 11,842 cycles

GAP PANEL 33319T SLIDING SEAL CHAFED (L/H) HORIZ STAB) / REMOVED & REPLACED SEAL I/A/W SRM 51-40-02

Part: PLATE — GOUGED (L1 DOOR GIRT BAR) · airframe 26,819 hrs · 11,842 cycles

FWD ENTRY DOOR; FWD GIRT BAR FLOOR ATTACH PLATE GOUGED/WORN / GIRT BAR ATTACH PLATES R&R'D ON NR D165632.

Part: PLATE — GOUGED (L1 DOOR GIRT BAR) · airframe 26,819 hrs · 11,842 cycles

FWD ENTRY DOOR; AFT GIRT BAR FLOOR ATTACH PLATE GOUGED/WORN / GIRT BAR ATTACH PLATES R&R'D ON N/R D165632 (TALLY 189)

Part: ATTACH ANGLE — CORRODED (BS 294-328) · airframe 26,819 hrs · 11,842 cycles

FWD GALLEY DOOR LOWER Z ANGLE HAS CORROSION FROM BS294- BS328 / R/R ATTACH L-ANGLE IAW SRM 51-10-02 AND SRM 51-40-02.

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 26,819 hrs · 11,842 cycles

FWD ENTRY DOOR BOTH GIRT BAR ATTACH PTS HAVE LIGHT CORROSION IN HOLES / REMOVED 2 EA GIRT BAR ATTACH PTS PER SRM 51-40-02. REPLACE 2 EA GIRT BAR ATTACH POINTS PER SRM 51-40-02

Part: NUT PLATE — CORRODED (LT EMER EXIT) · airframe 26,819 hrs · 11,842 cycles

L/H FWD + AFT OVERWING EMEGENCY EXIT DOORS LOWER LIFT HANDLE NUTPLATES CORRODED / REMOVED AND REPLACED I/A/W SRM 51-40-02

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 26,465 hrs · 11,655 cycles

CENTER WING REAR SPAR VAPOR WEB HAS A 10' DIAGONAL CRACK THAT EXTENDS FROM RBL 30.83 TO RBL 35. THE CRACK EXTENDS UNDER STIFFENER AT RBL 31.83. THIS IS THE LOWER RIGHT WEB (GFRP) REPAIRED CRACK PER SRM 57-10-10-2R-2REPETITIVE ACTION REQUIRED: DO A DETAILED VISUAL INSPECTION EVERY 3;000 FLIGHT CYCLES.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,189 hrs · 11,033 cycles

R1 DOOR SIDE EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 25,126 hrs · 11,010 cycles

R1 DOOR EMERGENCY LIGHT EXTERIOR LIGHT BEHIND INOP. / RELAMPED LIGHT IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 24,733 hrs · 10,832 cycles

L/H EMERGENCY LIGHT STRIP BETWEEN SEAT 11 TO SEAT 12 LOOSE ON FLOOR. SECURED EMERGENCY LIGHT STRIP PER SIP.

Part: SEAL — CRACKED (LH) · airframe 23,244 hrs · 10,104 cycles

LH HORIZONTAL STABILIZER UPPER SLIDING SEAL IS CRACKED / R&R L/H HORIZONTAL STABILIZER UPPER SLIDING SEAL REF AMM 53-31-31(INSP P56)

Part: BATTERY — FAILED (CABIN) · airframe 22,919 hrs · 9,980 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 22,919 hrs · 9,980 cycles

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

Part: SEAL — CRACKED (RH) · airframe 23,244 hrs · 10,104 cycles

R/H HORIZONTAL STABILIZER UPPER SLIDING SEAL IS CRACKED / R&R R/H HORIZONTAL STABILIZER UPPER SLIDING SEAL REF AMM 53-31-31(INSP P56)

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 21,876 hrs · 9,511 cycles

PHOTOLUMINESCENT STRIP LOOSE AT ROW 12. SECURED STRIP PER AMM.

Part: BRACKET — BROKEN (LEFT WING) · airframe 21,098 hrs · 9,130 cycles

LH WING TRAILING EDGE PANEL 551FB LEADING EDGE BRACKET (P/N 287A9152-23) BROKEN / REMOVED + REPLACED L/H WING TYRAILING EDGE PANEL 551FB LEADING EDGE BRACKET IAW SRM 51-40-02-0G-0 + AIPC 57-50-00-38

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 21,098 hrs · 9,130 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140DF HAS CORROSION ALONG EDGES. / FABRICATED NEW FLOOR PANEL 140DF FOR FWD CARGO IAW DWG PL453A2010 REV K

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 21,098 hrs · 9,130 cycles

PASSENGER CABIN FLOORBOARD 231TF HAS SEPARATED COMPOSITE PLIES. / REPAIRED SEPARATED PLY'S ON FACESHEET ON PANEL 231TF. IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1; SRM 53-00-50-2R-0 REPAIR GENERAL

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 21,098 hrs · 9,130 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140CF HAS CORROSION ALONG EDGES. / REPLACED AFT CARGO FLOOR PANEL 140CF P/N 453A2610-18 WN3580 IAW AIPC 25-52-10-19 & DWG 453A2610 REV D

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 21,098 hrs · 9,130 cycles

FWD CARGO COMPT; FLR PNL 120DF HAS CORROSION ALONG EDGES. / FABRICATED FWD CARGO CEILING PANEL 120DF IAW DWG PL453A2610 REV K

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 21,098 hrs · 9,130 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140AF HAS CORROSION ALONG EDGES. / REPLACED AFT CARGO PANEL 140 AF IAW AIPC 25-52-10-19 P/N 453A2610-38 WN8330 DAW 453A2610-38 REV D

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 21,098 hrs · 9,130 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140EF HAS CORROSION ALONG EDGES. / REPLACED AFT CARGO FLOOR PANEL 140EF IAW AIPC 25-52-10-19 P/N 453A2610-58 WN8267 & DWG 453A2610 REV D

Part: NONE — CORRODED (FWD CARGO BAY) · airframe 21,098 hrs · 9,130 cycles

FWD CARGO COMPARTMENT FLOOR SUPPORT SHIELD AFT OF CARGO DOOR STA. 490 TO 500A HAS 4 EACH AREA'S OF CORROSION (MARKED) / REMOVED AND REPLACED DAMAGED FWD CARGO FLOOR SUPPORT SHIELD AFT OF CARGO DOOR STA 440 TO 500A IAW SRM 51-40-02-0G-0. NEW SHEILD FABRICATED IAW DWG 143A8126 REV;G ORIG. MAT 0.032' CORROSION FOUND TO BE 100% OUT OF LIMITS IAW SRM 53-00-53-1A-2

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 21,098 hrs · 9,130 cycles

FWD CARGO COMPT; FLR PNL 120AF HAS CORROSION ALONG EDGES. / REPLACED FWD CARGO FLOOR PANEL 120AF P/N 453A1610-14 WN6405 IAW AIPC 25-52-10-17 & 453A1610 REV C

Part: SPLICE — CORRODED (AFT CARGO BAY) · airframe 21,098 hrs · 9,130 cycles

AFT CARGO COMPARTMENT FLOOR BOARD SPLICE PLATE STA 777 HAS CORROSION. / REPLACED AFT CARGO COMPARTMENT FLOORBOARD SPLICE PLATE P#146A9401/3030573 TAG#WN5132 IAW IPC 737-800 53-42-11-26 PG 26-28 AND BOEING DWG #146A9401 REV C

Part: SHIELD — CORRODED (FUSELAGE) · airframe 19,766 hrs · 8,553 cycles

FORWARD CARGO COMPARTMENT FLOOR SUPPORT SHIELD CORRODED BETWEEN BS 490 TO BS 500A. R&R SHIELD IAW DWG & SRM.

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 21,098 hrs · 9,130 cycles

FWD CARGO COMPT; FLR PNL 120CF HAS CORROSION ALONG EDGES. / REPLACED FWD CARGO FLOOR PANEL 450 CF P/N 453A1610-103 WN 7281 IAW AIPC 25-52-10-17 & DWG 453A1610 REV A

Part: COVER — CRACKED (CABIN) · airframe 19,766 hrs · 8,553 cycles

RT OVERHEAD STOWBIN EMERGENCY LIGHT LENS COVER CRACKED BETWEEN ROW 24 TO ROW 25. R&R COVER IAW AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 21,019 hrs · 9,098 cycles

L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: WINDOW — CRACKED (COCKPIT) · airframe 20,274 hrs · 8,786 cycles

L2 WINDOW LOWER RT CORNER ARCED AND CRACKED. R&R LT NR 2 SLIDING WINDOW IAW MT.

Part: WEB — CRACKED (WHEEL WELL RH) · airframe 20,258 hrs · 8,780 cycles

CENTER WING REAR SPAR VAPOR WEB HAS A 10' DIAGONAL CRACK THAT EXTENDS FROM RBL 30.83 TO RBL 35. THE CRACK EXTENDS UNDER STIFFENER AT RBL 31.83. THIS IS THE LOWER RIGHT WEB (GFRP). / REPAIRED PER SRM 57-10-10-2R-2.

Part: STRIP — CRACKED (CABIN) · airframe 20,175 hrs · 8,740 cycles

FORWARD LT EMERGENCY FLOOR PATH STRIP CRACKED. R&R STRIP PER AMM.

Part: LENS — CRACKED (CABIN) · airframe 18,717 hrs · 8,075 cycles

RT EMERGENCY EGRESS LIGHT LENS CRACKED AT ROW 10. R&R LENS PER SIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,851 hrs · 7,675 cycles

RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM.

Part: FAN — FAULTY (CABIN) · airframe 14,845 hrs · 6,326 cycles

AIR TURNBACK, ELECTRIC SMELL THROUGHOUT CABIN AND COCKPIT. R&R RECIRCULATION FAN PER AMM.

Part: FAN — ODOR (CABIN) · airframe 14,852 hrs · 6,328 cycles

ON TAKEOFF, WHILE PLANE SMELL OF ELECTRICAL BURNING OILS. SMELL QUICKLY DISSIPATED. NO OVERWEIGHT LANDING. R&R RECIRCULATION FANS IAW MM.

Part: COVER — MISSING (CABIN) · airframe 14,782 hrs · 6,296 cycles

CEILING EMERGENCY LIGHT COVER MISSING BETWEEN ROW 9 TO ROW 10. INSTALLED COVER IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 13,005 hrs · 5,507 cycles

RIGHT EMER LIGHT LENS COVER MISSING ABOVE ROW 14. INSTALLED LENS IAW MM.

Part: MOUNT — BROKEN (CABIN) · airframe 11,974 hrs · 5,073 cycles

FORWARD ENTRY DOOR EMER LIGHT MOUNTING PLATE BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 10,615 hrs · 4,500 cycles

LEFT CABIN CEILING EMER LIGHT LENS CRACKED, BETWEEN ROW 23 - 27. R & R LENS IAW AMM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 9,694 hrs · 4,124 cycles

AFT RT EMER EXIT LIGHT SIGN COVER BROKEN. R & R SIGN IAW AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 7,538 hrs · 3,155 cycles

RIGHT EEPLS STRIP DAMAGED AT ROW 1. R & R EEPLS IAW CMM.

Part: LENS — MISSING (CABIN) · airframe 7,187 hrs · 2,986 cycles

RIGHT OVERHEAD EMER AISLE LIGHT AT ROW 25 LENS MISSING. INSTALLED LENS IAW MM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 5,706 hrs · 2,357 cycles

CENTER CABIN OVERHEAD EMERGENCY SIGN COVER LOOSE. R & R COVER IAW MM.

Part: LENS — MISSING (CABIN) · airframe 4,561 hrs · 1,861 cycles

R2 DOOR EMERGENCY LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: LIGHT — MISSING (CABIN) · airframe 2,573 hrs · 1,037 cycles

L1 DOOR EXIT LIGHT MISSING. REPLACED LIGHT ASSEMBLY IAW MM.