N8315C

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 42,510 hrs · 20,171 cycles

FWD SERVICE DOOR GIRT BAR FALLS FROM STOWED POSITION WHEN DOOR IS OPEN. ADJUSTED AND RESECURED FWD SERVICE DOOR GIRT BAR IN REF TO AMM 25-66-01. NO DEFECTS NOTED.

Part: GIRT BAR — UNSECURE (ZONE 800) · airframe 41,762 hrs · 19,787 cycles

R2 DOOR ESCAPE SLIDE GIRT HANGS TOO LOW.<[01] RE-SECURED R2 DOOR ESCAPE SLIDE GIRT REF AMM 25-66-01.

Part: VALVE — READS HIGH (ZONE 100) · airframe 41,427 hrs · 19,598 cycles

ANTI SKID INOP <[01]. 05 - OK TO CONTINUE PER [MEL 32-2-01; ANTISKID SYSTEM ]. WITH SP 1 & 2 AND AUTHORIZATION NUMBER 243942. FOUND FC# PARKBRK IN HISTORY AND SP CO LI. TROUBLESHOT PER FIM 32-42 TASK 811. FOUND HIGH RESISTANCE ON PIN 8 AND 9 OF PARKING BRAKE VALVE. REMOVED AND REPLACED PARKING BRAKE VALVE IAW AMM 32-44-21. PERFORMED RESISTANCE CHECK OF ALL TRANSDUCERS FROM AACU. FOUND NO COUNTINUITY BETWEEN AACU AND L INBOARD TRANSDUCER. FOUND PIN 2 AND 3 AT D46006P SWAPPED IN WRONG CONFIGURATION. RE-CONFIGURED PER WDM 32-41-11. OPS CHECK GOOD PER AMM 32-42-00.

Part: CIRCUIT BREAKER — TRIPPED (ZONE 200) · airframe 40,209 hrs · 18,963 cycles

INFLIGHT CB B-10 ON PANEL P-18-3 (CA-SIDE) POPPED.<[01] PERFORMED OPS CHECK PER AMM 33-51-00-720-801-NG (EMERGENCY LIGHTS - OPERATIONAL CHECK - PERMANENT)] OPS CHECKS NORMAL

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 40,212 hrs · 18,964 cycles

EMERGENCY EXIT LIGHTS REMAIN ON IN ARM POSITION. FOUND BREAKER P18-3 B10 TO BE POPPED. OVERWING EXIT SIGN LIGHT IN CABIN STAYED ON IN THE ARMED POSITION. RESET BREAKER LIGHTS STAYED OFF DURING ARMED POSITION.<[01] REFERENCE WDM 33-51-11 PAGE 10 SHEET 2: EMERGENCY LIGHTS OPERATION CHECKS OK. REFERENCE M/M 33-51-00. SHOOK DOWN CONNECTIONS AT BATTERY PACK ASSEMBLIES M1695; M1671 AND M1672 PER SWPM?NO FAULTS FOUND. REPLACED M1695; M1671 AND M1672 CHARGER ASSEMBLIES AND BATTERY PACKS FOR TROUBLESHOOTING PER M/M 33-51-06. OPS CHECKS OK

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 39,788 hrs · 18,726 cycles

AFT L/H EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 39,555 hrs · 18,590 cycles

HYDRAULIC LEAK ON #1 BRAKE<[01] RESECURED B-NUT ON #1 BRAKE IAW AMM 32-41-00; NO LEAKS NOTED. A/C OK FOR SERVICE.

Part: LENS — MISSING (ZONE 200) · airframe 39,314 hrs · 18,463 cycles

A/C LEFT AT ROW 14; EXIT LIGHT COVER MISSING<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY REPLACEMENT - PERMANENT)]

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 39,133 hrs · 18,372 cycles

EMERGENCY EXIT LIGHT LENS COVER AT ROW 14; CAPTAIN'S SIDE BROKEN OFF.<[01] REATTACHED LENS COVER PER SIP.

Part: ROPE — LOOSE (COCKPIT) · airframe 37,928 hrs · 17,729 cycles

CUSTOMER WALK: EMERGENCY ESCAPE ROPE DOOR LOOSE.<[01] RESECURED FLIGHT DECK LH & RH ESCAPE ROPES REF AMM 25-61-10-400-801;[02] VERIFIED SECURITY

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 37,928 hrs · 17,729 cycles

FOUND EPL PATHWAYS STRIPS AT ROW 1DEF; 30ABC AND 30DEF INOP.<[01] REMOVED AND REPLACED EPL PATHWAYS STRIPS AT ROW 1DEF; 30ABC AND 30DEF; REF. B737-800 SWA WORK INSTRUCTION NO. 733-080-00-01.;[02] VERIFIED REPLACEMENT

Part: CRADLE — CRACKED (FWD FLASHLIGHT) · airframe 37,928 hrs · 17,729 cycles

FWD OUTBOARD FLASHLIGHT BRACKET IS CRACKED.<[01] PART TRANSACTION ONLY.;[02] REMOVED AND REPLACED FWD OUTBOARD FLASHLIGHT BRACKET; REF. ASTRONICS CMM 25-60-02;[03] VERIFIED.

Part: SIGN — CRACKED (EMERGENCY LIGHTS) · airframe 37,928 hrs · 17,729 cycles

AFT LOWER CEILING EXIT SIGN ASSY CRACKED.<[01] REMOVED AND REPLACED AFT LOWER CEILING EXIT SIGN ASSY. REF. B737-800 AMM 33-51-01-960-802.;[02] PARTS TRANSACTION ONLY.;[03] VERIFIED REPLACEMENT

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHTS) · airframe 37,928 hrs · 17,729 cycles

FOUND EMERGENCY BATTERY PACK AT POS. M1671 DEFECTIVE EMERGENCY LIGHT BATTERY PACK M1671 IS LOCATED AT STA 727C+13 WL 212 RBL 68.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT POS. M1671 AND PERFORMED TEST AS PER B737 AMM 33-51-06-960-805. TEST PASS.;[02] VERIFIED STEP 1.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 37,928 hrs · 17,729 cycles

LEFT WING LOWER MID T/E ACCESS PANEL 561BB HAS SEVERAL FASTENERS HOLES WICTH SMALL CRACKS.<[01] APPLIED REPAIR AT PANEL# 561BB PER B737 SRM 51-70-04-2R-9 AND 737SRM 51-70-04-2R-0 PARAGRAPH 4.N.2 MATERIAL USED RESIN EY3804 PO#2038047 FIBERGLASS PO#1690463.APPLIED TOPCOAT PER MANUFACTURE SPECIFICATIONS ON PANEL 561BB AS PER B737 AMM 51-21-99-300-802 (PARA 3-C STEP 3-E). MATERIALS USED PO#2033904;[02] VERIFIED STEP 1.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 37,928 hrs · 17,729 cycles

LEFT WING LOWER MID T/E ACCESS PANEL 561CB HAS SEVERAL FASTENERS HOLES WICTH SMALL CRACKS.<[01] **SUMMARY**<BR>1.ACCOMPLISHED PULSE-ECHO ULTRASONIC INSP. FOR DELAMINATION IAW B737 NDT P. 1; 51-01-02 AND P. 4; 51-00-01. DAMAGE NOTED AND LOCATION IDENTIFIED. EQUIP: EPOCH 600 B/C 19498 CAL DUE: 3/24<BR><BR>2.ACCOMPLICHED DRY OUT AT PANEL#561CB ON REPAIR AREA 24 HRS AS PER B737 SRM 51-70-04-2R-9 EQUIPMENT USED TEMPERATURE CONTROL ID-160354 DUE DATE 02-23-24 VACCUM ID- 173239 DUE DATE 02-23-24<BR><BR>3. REPAIRED PANEL AT DAMAGED HOLES PER B737 SRM 51-70-04-2R-9; SRM 51-70-04-2R-0 PARA 4.L.7. TOOL USED TEMPERATURE CONTROL ID-160354 DUE DATE 02-23-24 VACCUM ID- 173239 DUE DATE 02-23-24. MATERIAL USED RESIN P/O#1791128; CLOTH P/O#1690463<BR><BR>4. PERFORMED ULTRASOUND INSPECTION OF REPAIRED AREA AND MINIMUM OF 6 INCHES ALL AROUND USING CONTACT THROUGH TRANSMISSION ULTRASONIC REF B737 NDT PT 1; 51-01-01; NDT PT4 51-00-02. NO DAMAGE NOTED<BR>TOOL: EPOCH 600 B/C: 19498 DUE: 03/21/2024<BR><BR>5. RESTORED FINISH OF PANEL #561CB AS PER AMM 51-21-73-370-803.;[02] VERIFIED.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 37,928 hrs · 17,729 cycles

LEFT WING LOWER MID T/E ACCESS PANEL 561AB HAS SEVERAL FASTENERS HOLES WICTH SMALL CRACKS.<[01] MEASUREMENTS;[02] REPAIRED DAMAGE AREA AT LEFT WING LOWER T/EDGE ACCESS PANEL #561ABAS PER SRM 51-70-04-2R-9.MATERIAL USED EY 3804 A/B PO 20038047 PLUS BMS9-3-120 TYD CL7 PO 1690453.;[03] VERIFIED STEP 2.

Part: ATTACH ANGLE — CRACKED (BS 663 RBL 53) · airframe 37,928 hrs · 17,729 cycles

CRACK FOUND AT EXTERNAL OPEN FASTENER HOLE (1 EA) RH VAPOR BARRIER UPPER ATTACH ANGLE AT STA 663 ; RBL 53. CRACK FOUND AT EXTERNAL OPEN FASTENER HOLE (1 EA) RH VAPOR BARRIER UPPER ATTACH ANGLE AT STA 663 RBL 53.<[01] TRIMMED OUT CRACKED ANGLE AND FABRICATED NEW REPLACEMENT ANGLE AND SPLICE AT RH VAPOR BARRIER UPPER ATTACH ANGLE STA 663; RBL 53 IN REFERENCE TO B737-800 SRM 57-10-10-2R-5-B01456 (REPAIR 5).;[02] TRIMMED OUT CRACKED ANGLE; FABRICATED AND INSTALLED NEW REPLACEMENT ANGLE AND SPLICE AT RH VAPOR BARRIER UPPER ATTACH ANGLE STA 663; RBL 53 IN REFERENCE TO B737-800 SRM 57-10-10-2R-5-B01456 (REPAIR 5).;[03] FOR LEAK CHECK REF: TTG8Q00BAPZR.;[04] VERIFIED REMOVED; FABRICATED AND REPLACED ANGLE AND SPLICE.<BR>FOR LEAK CHECK REF TTG8Q00BAPZR;[05] VERIFIED STEP 4

Part: HANDLE — LOOSE (R2 DOOR) · airframe 37,928 hrs · 17,729 cycles

AFT GALLEY SERVICE DOOR (R2) INTERIOR HANDLE CAM PLATE LOOSE<[01] RE-SECURED AFT GALLEY SERVICE DOOR INTERIOR HANDLE CAM PLATE PER B737 AMM 52-41-00-700-801-NG /AMM 20-50-11-910-801 (TORQUE WRENCH B/C 175283 CAL DUE DATE 6-19-2024);[02] VERIFIED SECURED

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 37,928 hrs · 17,729 cycles

FOUND PANEL 231JF CABIN FLOOR DELAMINATED.<[01] REPLACED FLOOR PANEL 231JF PER SRM 53-00-50-1A-1.;[02] INSTALLED NEW FLOOR PANEL 231JF AT MAIN CABIN PER AMM 53-21-00-400-801.TOOL USED: SCREW GUN ID #176009; DUE CAL DATE:07/JUN/24.;[03] (LATE ENTRY) REMOVED FLOOR PANEL 231JF TO REPLACE PER SRM 51-40-02-0G-0;[04] (LATE ENTRY) VERIFIED REMOVED.<BR>VERIFIED INSTALLATION.

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 37,928 hrs · 17,729 cycles

FOUND PANEL 231HF CABIN FLOOR BROKEN.<[01] REPAIRED DAMAGE AREA AT FLOOR PANEL#231HF PER B737 SRM 53-00-50-2R-1 PARAGRAPH(5.J) MATERIAL USED RESIN 50A PO#2040692 FIBERGLASS SPO#1690463<BR>AND PERFORMED TAP TEST INSP AT REWORKED AREA; IAW B 737 NDT PART 1 51-05-01. NO DAMAGE NOTED. TOOL: ST8842; BC 167796.;[02] RII- VERIFIED REPAIR

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 37,928 hrs · 17,729 cycles

PANEL 242UF DELAMINATED<[01] VERIFIED; OK TO INSTALL.;[02] RECEIVED NEW FLOOR PANEL: P/N: 147A5810-136<BR><BR>INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD: 'TTG8Q00QDZXV';[03] STEP 1 ENTERED IN ERROR.<BR>VERIFIED; RECEIVED NEW FLOOR PANEL: P/N: 147A5810-136;[04] STEP 1 ENTERED IN ERROR.<BR>VERIFIED; RECEIVED NEW FLOOR PANEL: P/N: 147A5810-136

Part: SUPPORT ANGLE — CRACKED (BS 500F S26L) · airframe 37,928 hrs · 17,729 cycles

FWD CARGO COMPARTMENT BILGE SUPPORT CLIP CRACKED AT S-26L STA 500F BELOW Z CHANNEL MKD DOT<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT BILGE SUPPORT CLIP AT S-26L STA 500D BELOW Z CHANNEL PER REF SRM 51-40-02-0G-0 AND DWG#143A7505.;[02] VERIFIED SUPPORT CLIP INSTALLATION

Part: SUPPORT ANGLE — CRACKED (BS 500D S26R) · airframe 37,928 hrs · 17,729 cycles

FWD CARGO COMPARTMENT BILGE SUPPORT CLIP CRACKED AT S-26R STA 500D BELOW Z CHANNEL MKD DOT<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT BILGE SUPPORT CLIP CRACKED AT S-26R STA 500D BELOW Z CHANNEL PER REF SRM 51-40-02-0G-0 AND DWG#143A7505.;[02] CORRECTION STEP#1; REMOVED AND REPLACED FWD CARGO COMPARTMENT BILGE SUPPORT CLIP AT S-26R STA 500D BELOW Z CHANNEL PER REF SRM 51-40-02-0G-0 AND DWG#143A7505.<BR>PART REQUIREMENTS;[03] VERIFIED SUPPORT CLIP INSTALLATION

Part: GUSSET — CRACKED (BS 500I S19R) · airframe 37,928 hrs · 17,729 cycles

FWD CARGO COMPARTMENT AFT R/H GUSSET CRACKED AT S-19R STA 500I MKD DOT<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT AFT R/H GUSSET AT S-19R STA 500I PER REF SRM 51-40-02-0G-0 AND DWG#143A9481.;[02] VERIFIED GUSSET INSTALLATION

Part: SUPPORT ANGLE — CRACKED (BS 500H S26L) · airframe 37,928 hrs · 17,729 cycles

FWD CARGO COMPARTMENT BILGE SUPPORT CLIP CRACKED AT S-26L STA 500H BELOW Z CHANNEL MKD DOT<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT BILGE SUPPORT CLIP CRACKED AT S-26L STA 500H BELOW Z CHANNEL PER REF SRM 51-40-02-0G-0 AND DWG#143A7505.;[02] CORRECTION STEP#1; REMOVED AND REPLACED FWD CARGO COMPARTMENT BILGE SUPPORT CLIP AT S-26L STA 500H BELOW Z CHANNEL PER REF SRM 51-40-02-0G-0 AND DWG#143A7505.;[03] VERIFIED SUPPORT CLIP INSTALLATION

Part: SUPPORT ANGLE — CRACKED (BS 500H S26R) · airframe 37,928 hrs · 17,729 cycles

FWD CARGO COMPARTMENT BILGE SUPPORT CLIP CRACKED AT S-26R STA 500H BELOW Z CHANNEL MKD DOT<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT BILGE SUPPORT CLIP CRACKED AT S-26R STA 500H BELOW Z CHANNEL PER REF SRM 51-40-02-0G-0 AND DWG#143A7505.;[02] CORRECTION STEP#1;REMOVED AND REPLACED FWD CARGO COMPARTMENT BILGE SUPPORT CLIP AT S-26R STA 500H BELOW Z CHANNEL PER REF SRM 51-40-02-0G-0 AND DWG#143A7505.;[03] VERIFIED SUPPORT CLIP INSTALLATION

Part: SUPPORT — CRACKED (BS 500G S26R) · airframe 37,928 hrs · 17,729 cycles

FWD CARGO COMPARTMENT BILGE SUPPORT CLIP CRACKED AT S-26R STA 500G BELOW Z CHANNEL MKD DOT<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT BILGE SUPPORT CLIP AT S-26R STA 500G BELOW Z CHANNEL PER REF SRM 51-40-02-0G-0 AND DWG#143A7505.;[02] VERIFIED SUPPORT CLIP INSTALLATION

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 37,928 hrs · 17,729 cycles

FWD CABIN WET AREA FLOOR PANEL 221BF O/B EDGE DELAMINATES AND AFT CORNER CRACKED MKD DOT<[01] RECEIVED NEW FLOOR PANEL <BR><BR>P/N: 141A5810-729<BR><BR>INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD: 'TTG8Q00QE00Z';[02] VERIFIED

Part: FLOOR SUPPORT — CRACKED (BS 380-400 BL0) · airframe 37,928 hrs · 17,729 cycles

FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED AT BL-0 BETWEEN STA 380 AND 400 MKD DOT<[01] REMOVED AND REPLACED ANGLE AT FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL AT BL-0 BETWEEN STA 380 AND 400 IAW SRM 51-40-02-0G-0 AND DWG 143A5400;[02] VERIFIED FINAL STEP 1

Part: FLOOR SUPPORT — CRACKED (BS 380-400 LBL13) · airframe 37,928 hrs · 17,729 cycles

FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED AT LBL-13 BETWEEN STA 380 AND 400 MKD DOT<[01] FABRICATE ; REMOVED AND REPLACED UPPER CHORD AT FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL AT LBL-13 STA 380 - STA 400 IAW DWG 143A5400 AND B737 SRM 51-40-02-0G-0;[02] RII: VERIFIED STEP 1

Part: FLOOR SUPPORT — CRACKED (BS 540 RBL 1) · airframe 37,928 hrs · 17,729 cycles

MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED @ RBL 1 STA 540 MKD DOT<[01] REMOVED FLOOR SUPPORT AS PER SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW FLOOR SUPPORT AS PER SRM 51-40-05-0G-0 AND INSTALLED NEW FLOOR SUPPORT ON MAIN CABIN STA 540 RBL=1 TO RBL-24 AS PER SRM 51-40-02-0G-0;[02] VERIFIED;[03] VERIFIED REMOVED FLOOR SUPPORT AS PER SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW FLOOR SUPPORT AS PER SRM 51-40-05-0G-0 AND INSTALLED NEW FLOOR SUPPORT ON MAIN CABIN STA 540 RBL=1 TO RBL-24 AS PER SRM 51-40-02-0G-0

Part: FLOOR SUPPORT — CORRODED (BS 294-312 LBL12) · airframe 37,928 hrs · 17,729 cycles

CORROSION** AT FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL BETWEEN STA 294.5 AND STA 312 LBL 12 WL 208.1 MKD DOT<[01] REMOVED AND REPLACED FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL BETWEEN STA 294.5 AND STA 312 LBL 12 WL 208.1 AS PER SRM 51-40-02-0G-0 AND DWG 141A5600.;[02] VERIFIED STEP 1

Part: FLOOR SUPPORT — CRACKED (BS 540 LBL1) · airframe 37,928 hrs · 17,729 cycles

MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED @ LBL 1 STA 540 MKD DOT<[01] REMOVED AND REPLACED MAIN CABIN CENTER SECTION FLOOR SUPPORT AT LBL 1 STA 540 AS PER B 737 SRM 51-40-02-0G-0 AND DWG 143A.5240;[02] VERIFIED.

Part: FITTING — CORRODED (NR 1 DOOR SLIDE) · airframe 37,928 hrs · 17,729 cycles

CORROSION ** AT FWD ENTRY L-1 DOOR ESCAPE SLIDE FWD LATCH FITTING MKD DOT<[01] SUMMARY <BR>REMOVED CORROSION AT FWD ENTRY L-1 DOOR ESCAPE SLIDE FWD LATCH FITTING AS PER SRM 51-10-02-0G-0. ORIGINAL MATERIAL 0.050' MATERIAL LOST 0.015' MATERIAL REMAINING 0.035' FOUND OUT OF LIMITS AS PER SRM 53-10-51-1A-1. FIG. 105. USED CALIPER B/C 165957 DUE: 03-NOV-24. REMOVED AND REPLACED NEW LATCH FITTING AT FWD. ENTRY L-1 DOOR ESCAPE SLIDE FWD. SIDE AS PER B-737 SRM 51-40-02-0G.

Part: SHIELD — CRACKED (NR 2 NACELLE) · airframe 37,928 hrs · 17,729 cycles

NUMBER 2 ENG OUB FAN COWL INNER SHIELD UPPER EDGE CRACKED @ OIL SERVICE ACCESS PANEL MKD DOT<[01] REMOVED AND REPLACED INNER SHIELD AT NO-2 ENGINE O/B FAN COWL AT OIL SERVICE ACCESS PANEL PER BOEING 737-800 SRM 51-40-02-0G-0;[02] VERIFIED REPLACEMENT

Part: SHIELD — CRACKED (NR 1 NACELLE) · airframe 37,928 hrs · 17,729 cycles

NUMBER 1 ENG INB FAN COWL ASSY INNER SHIELD CRACKED @ ENG OIL SERVICE PANEL MKD DOT<[01] REMOVED AND REPLACED INNER SHIELD AT NO-1 ENG INB FAN COWL ASSY AT ENG OIL SERVICE PANEL PER BOEING 737-800 SRM 51-40-02-0G-0;[02] VERIFIED REMOVED;[03] VERIFIED REPLACEMENT

Part: STRAP — LOOSE (ESCAPE ROPE) · airframe 37,928 hrs · 17,729 cycles

LEFT OVERWING EXIT ESCAPE ROPE RED HOOK AND LOOP STRAP IS NOT ADHERED TO CUT OUT<[01] REMOVED AND REPLACED VELCRO STRAP AT LEFT OVERWING EXIT ESCAPE ROPE PER BOEING 737-800 AMM 20-10-06-400-801;[02] VERIFIED STEP 1

Part: SUPPORT — CRACKED (RT WING) · airframe 37,928 hrs · 17,729 cycles

R/W REAR SPAR DEFLECTION CONTROL RIB FIXED PANEL LOWER HORIZONTAL BULB SEAL RETAINER O/B SUPPORT CLIP CRACKED MKD DOT<[01] REMOVED AND REPLACED O/B SUPPORT CLIP AT R/W REAR SPAR DEFLECTION CONTROL FIXED PANEL LOWER HORIZONTAL BULB SEAL RETAINER AS PER B-737 SRM 51-40-02-0G-0;[02] VERIFIED; REMOVED AND REPLACED O/B SUPPORT CLIP AT R/W REAR SPAR DEFLECTION CONTROL FIXED PANEL LOWER HORIZONTAL BULB SEAL RETAINER

Part: DOOR — CORRODED (WASTE SERVICE) · airframe 37,928 hrs · 17,729 cycles

CORROSION** AFT LOWER FUSELAGE TOILET SERVICE DOOR 145AL @ BONDING WIRE ATTACHED POINT MKD DOT<[01] REMOVED AND REPLACED CORRODED BONDING WIRE AT AFT LOWER TOILET SERVICE DOOR AS PER REF AMM 20-10-37-120-801.BONDING METER DUE DATE 13/MAR/24;[02] VERIFIED. REMOVED AND REPLACED CORRODED BONDING WIRE AT AFT LOWER TOILET SERVICE DOOR AS PER REF AMM 20-10-37-120-801.BONDING METER DUE DATE 13/MAR/24;[03] CORRECT MEASUREMENT TABLE QUESTION 3;[04] ENTRY'S NUMBER 1 & 2 WERE ENTERED IN ERROR.<BR> (PLEASE FOLLOW STEPS BELOW.);[05] SUMMARY :REMOVED BOUNDING WIRE FOR ACCESS AS PER SRM 51-40-02-0G-0.REMOVED CORROSION AFT LOWER FUSELAGE TOILET SERVICE DOOR AS PER 51-10-02-0G-0.PERFORMED UT THICKNESS INSP ON REWORKED AREA;<BR>IAW B737 NDT PART 4 51-00-00 PROC. 3<BR>TOOLS: 27MG; B/C 172139; CAL. DUE 30-MAR-2024. MIN. THICKNESS 0.046?.EVALUATED REWORKED AREA ORG MAT. 0.060 MAT REMOVED.014 MAT REMAINING 0.046 FOUND TO BE OUT OF LIMITS AS PER B 737 SRM 52-40-01-1A-4 REMOVED AND REPLACED ACCESS DOOR 145AL AS PER B 737 SRM 51-40-02-0G-0.;[06] NDT FINISHED

Part: FRAME — CRACKED (BS 312) · airframe 37,928 hrs · 17,729 cycles

FWD CABIN WET AREA SIDE WALL FUS. SUPPORT FRAME FLANGE CUTOUT AREA CRACKED ABOVE L-1 DOOR UPPER CUTOUT FWD STA 312 MKD DOT<[01] ACCOMPLISHED EA: M-22-153-01244;[02] VERIFIED ACCOMPLISHED EA: M-22-153-01244

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 37,928 hrs · 17,729 cycles

LOWER FUSELAGE REAR SPAR CENTER WING R/H VAPOR BARRIER CRACKED MKD DOT<[01] DUPLICATED CARD; REF TASK CARD: TTG8Q00QW1LN FOR VAPOR BARRIER WEB REPAIR.;[02] VERIFIED STEP 1

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 37,928 hrs · 17,729 cycles

L/H HORIZONTAL L/E FAIRING 331B INT SUPPORT RIB # 4 CRACKED MKD DOT<[01] (SUMMERY)<BR>REMOVED DAMAGED #4 RIB AT L/HORIZONTAL STAB L/E FAIRING 331B AS PER REF SRM 51-40-02-0G-0<BR>LOCATED AND DRILLED L/H HORIZONTAL INT SUPPORT RIB # 4 AS PER B-737 SRM 51-40-05-0G-0<BR>INSTALLED INT SUPPORT RIB # 4 AS PER B-737 SRM 51-40-02-0G-0 & DWG 186A1301;[02] VERIFIED REMOVED DAMAGED #4 RIB AT L/HORIZONTAL STAB L/E FAIRING 331B AS PER REF SRM 51-40-02-0G-0<BR>LOCATED AND DRILLED L/H HORIZONTAL INT SUPPORT RIB # 4 AS PER B-737 SRM 51-40-05-0G-0<BR>INSTALLED INT SUPPORT RIB # 4 AS PER B-737 SRM 51-40-02-0G-0 & DWG 186A1301

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 37,928 hrs · 17,729 cycles

L/W OUB AFT FLAP INB LOWER T/E SPOT DELAMINATE 7INC FROM I/B EDGE AND 3INC. FROM TRAILING EDGE MKD DOT<[01] REPLACED L/W OUB AFT FLAP IN REF B737 AMM 27-51-22-400-801 AND ACCOMPLISHED L/W OUTBOARD AFT FLAP ADJUSTMENT /CHECK PER B737 AMM 27-51-22-400-801-NG CALIPER B/C 175908 CAL DUE DATE 25 MAY 24;[02] RII- VERIFIED REPLACEMENT AND ADJUSTMENT CHECK

Part: BULKHEAD WEB — CRACKED (ZN 100 FUS LOWER) · airframe 37,928 hrs · 17,729 cycles

RH VAPOR WEB FOUND CRACKED<[01] APPLIED REPAIR AT VAPOR BARRIER ON BOTHS SIDE PER B737SRM 51-70-04-2R-10 PARAGRAPH (4.D); B737SRM 51-70-04-2R-0 PARAGRAPH (4.L.7) AND CURE REPAIR PER B737 SRM 51-70-04-2R-10 PARAGRAPH (4.F); B737 SRM 51-70-04-2R-0 PARAGRAPH (4.N.2) MATERIAL USED RESIN EY 3804 PO#2040614 FIBERGLASS PO#1690463 AND EQUIPMENT USED TEMPERATURE CONTROLLER ID 160354 DUE DATE 02/16/24 AND VACUUM GAGEID173239 DUE DATE 02/23/24;[02] RII-VERIFIED REPAIR

Part: SLIDE — LOOSE (ZN 800 DOOR) · airframe 37,767 hrs · 17,642 cycles

R1 SLIDE FELL OUT OF CONTAINER<[01] RESECURED EMERGENCY EXIT SLIDE ON R1 DOOR IAW MT 725-61-06.

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 37,500 hrs · 17,487 cycles

EMER EXIT SIGN ON FWD EMER EXIT DOOR MISSING ON FO SIDE<[01] INSTALLED LENS IAWMM 33-51-01

Part: SLIDE — OUT OF LIMITS (ZN 800 DOOR) · airframe 37,463 hrs · 17,470 cycles

FE ESCAPE SLIDE PRESSURE OUT OF GREEN BAND<[01] R & R FE ESCAPE SLIDE IAW AMM 25-66-01 AND MT725-61-06

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 36,915 hrs · 17,165 cycles

BATTERY PACKS AT POSITIONS M2816 AND M1675 FAILED TIME CHECK<[01] R/R BATTERY PACKS AT POSITIONS M2816 AND M1675 REF AMM 33-51-00.

Part: ACCESS DOOR — OUT OF ADJUST (ZN 100 FUS LOWER) · airframe 36,911 hrs · 17,164 cycles

EXTERNAL CONDITIONED AIR COMPARTMENT DOOR NOT FUNCTIONING PROPERLY<[01] REMOVED AND REPLACED GROUND AIR CONDITIONING FWD FAIRING ACCESS PANEL PER AMM 52-49-01. OPS CHECK GOOD.

Part: BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 33,773 hrs · 15,433 cycles

RIGHT MLG WHEEL WELL LOWER RIGHT VAPOR WEB BARRIER HAS A CRACK APPROXAMATLY 6 INCHES LONG BETWEEN RBL 32.00 AND RBL 36.00. CRACK INITIATES AT A FASTENER AT TERMINATES AT A FASTENER. / [01] AS PER AVIATION PARTNERS BOEING SRM SUPPLEMENT 57-10-10 ALLOWABLE DAMAGE 2 SEALED CRACK WITH SPEED TAPE PER SRM 57-10-10-1A-2; PARAGRAPH 2; C; (4) ; (2)/ ALLOWABLE DAMAGE 2. CRACK IS IN ZONE 1. DO A DETAIL VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY.

Part: SCUFF PLATE — BROKEN (FWD FUSELAGE) · airframe 31,946 hrs · 14,472 cycles

CAPTAIN SIDE SLIDING WINDOW SCUFF WEDGE BROKEN ON FRAME SIDE / [01] R&R CAPTAIN SIDE SLIDING WINDOW SCUFF PLATE ASSY PER AMM 56-12-11. OP CK GOOD

Part: SWITCH — LOOSE (L1 DOOR) · airframe 31,852 hrs · 14,423 cycles

FORWARD ENTRY DOOR SWITCH S1147 WILL NOT CONTROL DOOR WARNING LIGHT. / [01] RESECURED GROUND WIRE#W3058-0029-22 AT GD4170-DC IAW SOPM 20-11-02. FWD ENTRY DOOR WARNING SWITCH TEST IS GOOD IAW AMM 52-71-01.

Part: PANEL — CORRODED (L/H WING) · airframe 31,852 hrs · 14,423 cycles

FUEL ACCESS PANEL 532QB POSSIBLE CORROSION ON SCREW INSET AND PANEL. (MARKED) / [01] PURGED FUEL ACCESS PANEL ASSY 532QB FROM INVENTORY AND REPLACED WITH NEW FUEL ACCESS PANEL ASSY 532QB. PANEL ASSY TO BE INSTALLED ON AIRCRAFT ON MT 757-160-01-01.;[02] PURGED FUEL ACCESS PANEL ASSY 532QB FROM INVENTORY AND REPLACED WITH NEW FUEL ACCESS PANEL ASSY 532QB. PANEL ASSY TO BE INSTALLED ON AIRCRAFT ON MT 757-160-01-01. C/W INSPECTION

Part: FLAP — DELAMINATED (L/H WING) · airframe 31,852 hrs · 14,423 cycles

L/H O/B AFT FLAP LOWER SURFACE I/B EDGE HAS A DELAM AREA OF APPROX. 14'X14'. MPN:113A3700-25 SN: 004021 / [01] OK TO INSTALL FLAP;[02] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22;[03] INSPECTED WORK PERFORMED ON C/A # 2;[04] 2. SAMUEL SMITH (TECHNICIAN); 11-MAR-2022 19:14 UTC<BR>REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22.;[05] VERIFIED ADJUSTMENT IS GOOD

Part: PANEL — ELONGATED (FUSELAGE) · airframe 31,852 hrs · 14,423 cycles

PANEL 553ET HAS ELONGATED HOLE (MARKED) / [01] DRILLED UP AND COUNTERSUNK NEW PANEL IAW SRM 51-40-02.;[02] VERIFIED DRILLED UP AND COUNTERSUNK NEW PANEL IAW SRM 51-40-02.;[03] PAINT PANEL 553ET PER AMM 51-21-00;[04] INSPECTED WORK PERFORMED

Part: PANEL — CRACKED (R/H WING) · airframe 31,852 hrs · 14,423 cycles

R/H WING PANEL 642BB AFT END CRACKED JUST AFT OF CUT OUT BOTH SIDES.(MARKED) / [01] RESIN SWEPT VOID PER SRM 51-70-08 AND REFINISHED PER AMM 51-21-00.;[02] VERIFIED

Part: COUNTERWEIGHT — CORRODED (R/H WING) · airframe 31,852 hrs · 14,423 cycles

RIGHT WING O/B COUNTER BALANCE WEIGHTS ARE CORRODED. / [01] REPAIRED PER EA 22-157-00365.;[02] VERIFIED REPAIRED PER EA 22-157-00365. OK TO INSTALL WEIGHTS.;[03] VERIFIED WEIGHT INSTALLATION PER AVIATION PARTNERS BOEING MM 57-44-02 ON STEPS 1 AND 2.;[04] OK TO INSTALL WRAP AROUND PANEL OVER COUNTER BALANCE WEIGHTS;[05] VERIFIED COMPLETION OF WORK

Part: COUNTERWEIGHT — CORRODED (L/H WING) · airframe 31,852 hrs · 14,423 cycles

LEFT WING O/B COUNTER BALANCE WEIGHTS ARE CORRODED. / [01] REPAIRED PER EA 22-157-00365.;[02] VERIFIED REPAIRED PER EA 22-157-00365. OK TO INSTALL WEIGHTS.;[03] VERIFIED WEIGHT INSTALLATION PER AVIATION PARTNERS BOEING MM 57-44-02 ON STEPS 1 AND 2.;[04] OK TO INSTALL WRAP AROUND PANEL OVER COUNTER BALANCE WEIGHTS;[05] VERIFIED COMPLETION OF ALL WORK

Part: PLATE — CRACKED (L/H WING) · airframe 31,852 hrs · 14,423 cycles

LEFT WING T/E WAFFLE PLATE I/B OF # 3 FLAP TRANSMISSION IS CRACKED.(FOR PNL 551DB). / [01] REMOVED AND REPLACED LEFT WING T/E WAFFLE PER SRM 51-40-02.;[02] SELECT REFERENCE NOT SELECTED. MUST NOT BE TYPED PER THE POD. I'M UNABLE TO COMPLETE CARD;[03] C/W INSPECTION

Part: LIGHT — CRACKED (CABIN) · airframe 31,852 hrs · 14,423 cycles

CABIN EMER. LIGHT LENS CRACKED 10DEF / [01] REPLACED EPL/AREA AISLE LIGHT LENSE AT O/H BIN 10DEF IN REFERENCE TO AMM 33-51-03;[02] REPLACED EPL/AREA AISLE LIGHT LENSE AT O/H BIN 10DEF IN REFERENCE TO AMM 33-51-03 C/W INSPECTION;[03] REMOVED AND REPLACED EMERGENCY PATH LIGHT ROW 10DEF; OPS CHECKS GOOD PER MM 33-51-00

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

2EA EXTERIOR LH OVERWING EMERGENCY EXIT LIGHTS INOP / REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACKS M1670 AND M2335 PER AMM 33-51-06-960-805 AND PERFORMED SATISFACTORY OPERATIONAL TEST PER AMM 33-51-00-710-801 57563U 18AUG21

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

EXTERIOR LH EMERGENCY EXIT LIGHT INOP AFT OF WING TO BODY FAIRING / REPLACED EMERGENCY BATTERY (M1670) PERFORMED GOOD FUNCTIONAL TEST OF EXTERIOR LH EMERGENCY EXIT LIGHT AFT OF WING TO BODY FAIRING PER AMM 33-51-06-960-805

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EXTERIOR RH EMERGENCY EXIT LIGHT INOP AFT OF WING TO BODY FAIRING / REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK M1671 PER AMM 33-51-06-960-805 AND PERFORMED SATISFACTORY OPERATIONAL TEST PER AMM 33-51-00-710-801 57563 18AUG2021 REPLACEMENT PERFORMED ON DEFECT U363186

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EXTERIOR RH AFT OVERWING EMERGENCY EXIT LIGHT INOP / REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK M1671 PER AMM 33-51-06-960-805 AND PERFORMED SATISFACTORY OPERATIONAL TEST PER AMM 33-51-00-710-801 57563U 18AUG2021

Part: LANYARD — MISSING (FWD CARGO DOOR)

FORWARD CARGO BAY DOOR LANYARD IS MISSING HARDWARE / REPLACED FORWARD CARGO BAY DOOR LANYARD IAW MM 52-31-00-000-801 PAR D STEP 1(A)(B)(C); MM 52-31-00-400-801 PAR F STEP 5(G)1-3

Part: STRINGER — CRACKED (BS 267 S8L)

DAMAGE CRACK COMMON TO S-8L APPROX AT 267 / REPAIRED PER EA NO: 21-153-02199 PART 2 STEP 2E105567

Part: STRINGER — DAMAGED (BS 259 S7L)

DAMAGE FROM STR 7L TO STR 10 L 10 INCHES AFT OF STA 259.5 / DAMAGED REWORK COMPLETED PER E/A NO: 21-152-02206SA-M 326: A1155845E105567

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,489 hrs · 29,781 cycles

EMERGENCY LIGHTS L1526; L1507 (X2) L1209 INOP / R+R BATTERY PACK M1676 PER MM 33-51-06 OPS CHECK GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,678 hrs · 12,365 cycles

DURING EXTERIOR WALK FOUND LT OVERWING EMERGENCY LIGHT INOPERABLE. RELAMPED LT OVERWING EMERGENCY LIGHT PER AMM 33-51-04 OPS CHECK GOOD

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 26,629 hrs · 11,728 cycles

L1 EMERGENCY SLIDE LIGHT WILL NOT COME ON WHEN TESTED. REMOVED AND REPLACED FWD L/H POWER SUPPLY IAW AMM 33-51-06-960-806. INSTALLATION TEST GOOD. REMOVED AND REPLACED FWD L/H POWER SUPPLY BATTERY PACK IAW AMM 33-51-06-960-805. INSTALLATION TEST GOOD. WN7392

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 26,629 hrs · 11,728 cycles

EMERGENCY EXIT LIGHTS WILL NOT COME ON THE LAST STOWBIN ON RIGHT SIDE, G4 EXIT LIGHT ON SURROUND, AND R 2 EXTERIOR SLIDE LIGHT, ALL CONTROLED BY POWER SUPPLY M1672 REMOVED AND REPLACED POWER SUPPLY M1672 IAW AMM / 33-51-06-960-805. REMOVED AND REPLACED BATTERY / M1672 IAW AMM 33-51-06-960-805. INSTALLATION TEST / GOOD. ATAG: WN7391

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,629 hrs · 11,728 cycles

L1 EMERGENCY SLIDE LIGHT WILL NOT COME ON WHEN TESTED. REMOVED AND REPLACED FWD L/H POWER SUPPLY IAW AMM 33-51-06-960-806. INSTALLATION TEST GOOD. REMOVED AND REPLACED FWD L/H POWER SUPPLY BATTERY PACK IAW AMM 33-51-06-960-805. INSTALLATION TEST GOOD. WN7392

Part: STRIP — CRACKED (AFT CARGO) · airframe 26,646 hrs · 11,735 cycles

AFT CARGO BAY; FLOOR PANEL 140AF TOP HORSESHOE CAP STRIP IS CRACKED / RECEIVED NEW CAP STRIP; INSTALLED IAW AMM 25-52-10-400-801 P/N 453A2611-12 A TAG A24866

Part: PLATE — CORRODED (AFT CARGO) · airframe 26,646 hrs · 11,735 cycles

AFT CARGO COMPARTMENT; AFT TRANSITION PLATE FOR DOOR SURROUND PANEL 142LW TO FLOOR PANEL 140CF HAS CORROSION ON UPPER AND LOWER SURFACE / REPLACED PLATE P/N 453A2611-2 ON AFT CARGO FLOOR I.A.W SRM 51-40-02-0G-02. NO WRITTEN LIMITS FOR TRANSITION PLATE AT STA 847 RBL 25 PART OUT OF LIMITS A-TAG # A96311 P/N 453A2611-2

Part: ATTACH ANGLE — CORRODED (BS 767-780) · airframe 26,150 hrs · 11,494 cycles

AFT CARGO FORWARD SHIELD ATTACH ANGLE FOUND CORRODED AFTER SHIELD BETWEEN BS. 767 TO BS. 780, RBL 22. / R&R ANGLE IAW SRM, AMM, AND DWG.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 26,646 hrs · 11,735 cycles

AFT CARGO FWD SHIELD ATTACH ANGLE FOUND CORRODED AFTER SHIELD REMOVAL STA 767 TO 780 RBL 22 WL 157 / AFT CARGO FWD SHIELD ATTACH ANGLE FOUND TO BE OUT OF LIMITS. NO ALLOWABLE DAMAGE FOUND IN SRM. REMOVED AND REPLACED AFT CARGO FWD FLOOR SHIELD ATTACH ANGLE IAW SRM 51-40-02-0G-0 AND DWG 146A5125 REV A. APPLIED CIC IAW AMM 51-21-91-620-802 146A8125-53 ATAG: HU1254

Part: ANGLE — CORRODED (BS 500C) · airframe 26,646 hrs · 11,735 cycles

FWD CARGO COMPARTMENT STA. 500C+7' AND STA. 500C+11.5' 'Z' ANGLE HAS CORROSION AT THE SCREW HOLES WL 155 RBL 25. / WORK ACCOMPLISHED FOR THE REPAIR OF 'Z' ANGLE FROM STA 500A TO 500G +10'; IAW B737-800 SRM 53-00-53-2R-5 ON NRC Y179602.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,150 hrs · 11,494 cycles

AFT CARGO COMPARTMENT RIGHT SIDEPLATE STA 727F+20 TO 767 RBL21 WL155 HAS CORROSION ON UPPER SURFACE REMOVED CORROSION IN AFT CARGO R/H SIDE ZEE ANGLE AT STA 727I ORIG "T" IS .040. REMAINING .033 LOSS OF .007 OUT OF LIMITS IAW SRM 53-00-53-1A-2 REPLACED R/H ZEE ANGLE SECTION FROM STA 727 TO 767 IAW SRM 53-00-53-2R-5 ACCOMPLISHED BONDED NUTPLATE CHECK IAW SRM 51-40-01-2R-0 INSTALLED IAW BOEING DRAWING 146A7500 SHEET 213

Part: FLOORBOARD — BROKEN (CABIN) · airframe 26,646 hrs · 11,735 cycles

PASSENGER COMPARTMENT FLOOR BOARD 221 AF BOTTOM SKIN R/H EDGE SKIN PLIES AS MARKED ARE BROKEN / REPAIRED BOTTOM R/H EDGE SKIN ON FLOORBOARD PANEL (221 AF) WITH LAY UP REPAIR IAW B737-800 SRM 53-00-50-2R-1 (3) A-N (REV68)

Part: FLOORBOARD — BROKEN (CABIN) · airframe 26,646 hrs · 11,735 cycles

PASSENGER COMPARTMENT FLOOR BOARD 221EF AFT R/H CORNER IS BROKEN / REPAIRED CORNER ON FLOORBOARD PANEL (221EF) WITH WET LAY-UP REPAIR IAW B737-800 SRM 53-00-50-2R-1 (3) A-N (REV 68)

Part: SUPPORT BRACKET — CRACKED (BS 867) · airframe 26,646 hrs · 11,735 cycles

AFT CARGO COMPARTMENT WASTE TANK ENCLOSURE STRUCTURE L-SUPPORT BRACKET STA 867 LBL11 IS CRACKED / REMOVED AND REPLACED L-SUPPORT BRACKET AT STA 869 LBL 11; IN AFT CARGO COMPARTMENT WASTE TANK; IAW B737-800 SRM 51-40-02-0G-0 AND BOEING DWG # 1441A8102 REV A APPLIED CIC. IAW B737-800 AMM 51-21-91-220-802.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 26,150 hrs · 11,494 cycles

AFT CARGO COMPARTMENT FLOOR TRACK STA 767+6 RBL13.8 WL157 HAD CORROSION ON UPPER SURFACE REMOVED CORROSION AT AFT CARGO TRACK STA 767+6 RBL 13.8 WL157 IAW SRM 53-00-53-1A-2 VERIFIED MATERIAL LOSS ORIGINAL .080 REMOVED .028 REMAIN .052 ALLOWABLE 10% MAX FOUND OUT OF LIMITS USED AAR TOOL #3 6285 DUE 06FEB21 IAW SRM 53-00-53-1A-2. REMOVED TRACK FROM STA 747+10 TO STA 887 I.E. SRM 51-40-02-0G-0. DRILLED NEW TRACK AND REPAIR SPLICE I.E. SRM 53-00-53-2R-3. INSTALLED NEW TRACK AND REPAIR SPLICE I.E. SRM 53-00-53-2R-3 AND BOEING DWG 146A7500 146A7501-23

Part: ANGLE — CORRODED (BS 500D) · airframe 26,646 hrs · 11,735 cycles

FWD CARGO COMPARTMENT STA. 500D+2' TO STA. 500D+10' 'Z' ANGLE HAS CORROSION WL 155 RBL 25. / WORK ACCOMPLISHED FOR THE REPAIR OF 'Z' ANGLE FROM STA 500 A TO 500G + 10'; IAW B737-800 SRM 53-00-53-2R-5 ON NRC Y179602.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,646 hrs · 11,735 cycles

PASSENGER COMPARTMENT FLOOR BOARD 221AF TOP SKIN OF FLOOR BOARD 3EA AREAS SKIN PLY FIBERS ARE DAMAGED / REPAIRED UPPER FACESHEET SKIN MISSING FIBERS ON FLOORBOARD PANEL 221 AF) WITH LAY UP REPAIR IAW B737-800 SRM 53-00-50-2R-1 (3) A-N (REV 68)_

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,646 hrs · 11,735 cycles

PASSENGER COMPARTMENT FLOOR BOARD 222AF TOP SKIN OF FLOOR BOARD IN SEVERAL AREAS SKIN PLY FIBERS ARE DAMAGED / REPAIRED UPPER SURFACE PLY ON FLOORBOARD 222AF IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS 3 (A-M).

Part: ANGLE — CORRODED (BS 500D) · airframe 26,150 hrs · 11,494 cycles

FORWARD CARGO COMPARTMENT "Z" ANGLE HAD CORROSION AT THE SCREW HOLE AT BS. 500D+6.5, LBL 25. / R&R Z ANGLE IAW SRM.

Part: FLOORBOARD — BROKEN (CABIN) · airframe 26,150 hrs · 11,494 cycles

PASSENGER COMPARTMENT FLOOR BOARD 221EF AFT R/H CORNER BROKEN. / REPAIRED FLOOR BOARD PANEL (221EF) IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 26,150 hrs · 11,494 cycles

AFT CARGO COMPARTMENT FLOOR TRACK STA 787+8 RBL13.8 WL158 HAD CORROSION ON UPPER SURFACE CARGO TRACK AT AFT CARGO FROM STA 747+10 TO STA 887 R/H RBL 13.8 BEEN REPLACED ON N/R Y179552. REMOVED CORROSION IAW SRM 51-10-02-0G-0. ORIGINAL .070 REMAINING LOSS .011 P/N 146A7501-23 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,646 hrs · 11,735 cycles

PASSENGER COMPARTMENT FLOOR BOARD 221EF TOP SKIN OF FLOOR BOARD IN SEVERAL AREAS SKIN PLY FIBERS ARE DAMAGED / REPAIRED UPPER FACESHEET DAMAGED FIBERS ON FLOORBOARD PANEL (221EF) WITH W ET LAY-UP REPAIR IAW B737-800 SRM 53-00-50-2R-1 (3) A-N) REV 68

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,646 hrs · 11,735 cycles

PASSENGER COMPARTMENT FLOOR BOARD 221GF TOP SKIN OF FLOOR BOARD IN SEVERAL AREAS SKIN PLY FIBERS ARE DAMAGED / SKIN PLY FIBERS ON FLOOR BOARD 221 GF TP SKIN REPAIRED IAW SRM 53-00-51-2R-1 PARA 3 STEPS ATO 0.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,646 hrs · 11,735 cycles

PASSENGER COMPARTMENT FLOOR BOARD 221DF L/H AFT BOTTOM SIDE OF BOARD SKIN PLIES AND CORE IS DAMADED (BROKEN/ MISSING) / PASSENGER COMPARTMENT FLOORBOARD 221DF; REPAIRED W/H AFT BOTTOM SIDE OR BOARD SKIN PLIES AND CORE DAMAGE IAW SRM 53-00-50-2R-1 PARA 3 STEPS A THROUGH O

Part: ISOLATOR — CRACKED (R2 DOOR) · airframe 26,646 hrs · 11,735 cycles

RIGHT AFT SERVICE DOOR (R2) PANEL 844DZ FORWARD BRACKET IS CRACKED. / REPLACED RIGHT AFT SERVICE DONE (R-2) PANEL 844DZ ON BENCH I.A.W IPC 52-41-31-10 ITEM 405. A -TAG - WN6340.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,646 hrs · 11,735 cycles

PASSENGER CABIN FLOORBOARD 241WF AFT EDGE IS DAMAGED / REPAIRED AFT EDGE ON FLOORBOARD 241 WF IAW SRM 53-00-50-2R-1; PG'S 1; 2; STEPS 3(A-M).

Part: FRAME — CORRODED (BS 947 BULKHEAD) · airframe 26,646 hrs · 11,735 cycles

AFT CARGO COMPARTMENT AFT BULKHEAD STRUCTURE LOWER CHORD STA 947 LBL10-RBL21 WL178 HAS CORROSION ON UPPER SURFACE / EVALUATED CORROSION ON AFT CARGO AFT B/H STRUCTURE LOWER CHORD AT STA 947 LBL 10 TO LBL 21 ANS WATER LINE 178; FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA IAW SRM 51-10-02-0G- STEP 9.C. REMOVED AND REPLACED; LOWER CHORD; P/N 149A8118-29 IAW SRM 51-40-02-0G-0 AND DRAWING 149A8110 REV B AND DRAWING 149A8117 REV - 149A8118-29

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,646 hrs · 11,735 cycles

PASSENGER COMPARTMENT FLOOR BOARD 221CF BOTTOM SKIN AFT EDGE IS DAMAGED / DISBONDED FROM CORE AS MARKED / REPAIRED PASSENGER COMPARTMENT FLOOR BOARD 221CF BOTTOM SKIN AFT EDGE DISBOND IAW B737-800 SRM'S 53-00-50-2R-6 REV 68 AND 53-00-50-2R-0 REV 68 (A98115) (A94414) (A89485)

Part: FLOORBOARD — BROKEN (CABIN) · airframe 26,150 hrs · 11,494 cycles

PASSENGER COMPARTMENT FLOOR BOARD 221 AF BOTTOM SKIN R/H EDGE SKIN PLIES WERE BROKEN. / REPAIRED SKIN ON FLOOR BOARD PANEL (221 AF) IAW SRM.

Part: CARGO TRACK — CORRODED (BS 737 RBL14) · airframe 26,646 hrs · 11,735 cycles

AFT CARGO COMPARTMENT FLOOR TRACK STA 767+6 RBL13.8 WL157 HAS CORROSION ON UPPER SURFACE / REMOVED CORROSION AT AFT CARGO TRACK STA 767+6 RBL 13.8 WL157 IAW SRM 53-00-53-1A-2 VERIFIED MATERIAL LOSS ORGINAL .080 REMOVED .028 REMAIN .052 ALLOWABLE 10% MAX FOUND OUT OF LIMITS USED AAR TOOL #3 6285 DUE 06FEB21 IAW SRM 53-00-53-1A-2. REMOVED TRACK FROM STA 747+10 TO STA 887 I.A.W SRM 51-40-02-0G-0. DRILLED NEW TRACK AND REPAIR SPLICE I.A.W SRM 53-00-53-2R-3. INSTALLED NEW TRACK AND REPAIR SPLICE I.A.W SRM 53-00-53-2R-3 AND BOEING DWG 146A7500 146A7501-23

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,646 hrs · 11,735 cycles

PASSENGER COMPARTMENT FLOOR BOARD 221BF LAV DUMP TUBE CUTOUT TOP SKIN PLIES AND CORE IN 2EA AREAS AS MARKED ARE DAMAGED / REPAIRED PASSENGER COMPARTMENT FLOORBOARD #221BF OF DAMAGE TO SKIN PLIES AND CORE IN 2(EA) AREAS (AS MARKED) AT LAV DUMP TUBE CUTOUT IAW B737-800 SRM 53-00-50-2R-0 REV 68 AND B737-800 SRM 53-00-50-2R-1 REV 68. A94414 A89485 A98815

Part: CARGO TRACK — CORRODED (BS 787 RBL14) · airframe 26,646 hrs · 11,735 cycles

AFT CARGO COMPARTMENT FLOOR TRACK STA 787+8 RBL13.8 WL158 HAS CORROSION ON UPPER SURFACE / CARGO TRACK AT AFT CARGO FROM STA 747+10 TO STA 887 R/H RBL 13.8 BEEN REPLACED ON N/R Y179552. REMOVED CORROSION IAW SRM 51-10-02-0G-0. ORIGINAL .070 REMAINING LOSS .011 P/N 146A7501-23 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,646 hrs · 11,735 cycles

PASSENGER COMPARTMENT FLOOR BOARD 221BF TOP SKIN OF FLOOR BOARD IN SEVERAL AREAS SKIN PLY FIBERS ARE DAMAGED / REPAIRED PASSENGER COMPART;MENT FLOORBOARD #221BF OF TOP SKIN WITH SEVERAL AREAS OF PULLED AND FRAYED FIBERS (AS MARKED) IAZW B737-800 SRM 53-00-50-2R-0 REV 68 AND B737-800 SRM 53-00-50-2R-1 REV 68 A94414; A98054

Part: ANGLE — CORRODED (FWD CARGO) · airframe 26,646 hrs · 11,735 cycles

FWD CARGO COMPARTMENT STA.500D+6.5' WL 155 LBL 25 'Z' ANGLE HAS CORROSION AT THE SCREW HOLE. / REMOVED AND REPLACED FWD CARGO COMPARTMENT 'Z' ANGLE WL 155; LBL 25' FROM STA. 500C TO 6' TO 500G + 10' IAW 737 SRM 53-00-53-2R-5 REPAIR 5. P/N 143A7501-187. EVALUATED CORROSION ON FWD CARGO L/H Z ANGLE AT STA 500D + 6.5'; WL155 AND LBL25; ORIGINAL .040' LOSS OF .017' REMAINING .023' FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 26,646 hrs · 11,735 cycles

AFT CARGO COMPARTMENT FORWARD SHIELD STA 767 TO 787 RBL22 WL157 HAS CORROSION ON UPPER AND LOWER SURFACE / REMOVED CORROSION IAW B737 SRM 51-10-02-0G-0 AND INSPECTED WITH 10X MAG GLASS. NO DEFECTS NOTED. VERIFIED MATERIAL LOSS ORIGINAL T=.050 REMAING T=.043 LOSS=.007'. IS OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED AFT CARGO BAY FWD FLOOR SHIELD IAW SRM 51-40-02-0G-0 AND DWG 146A0081 REV- APPLIED CIC IAW AMM 51-21-91-620-802 ATAG WN5952

Part: FLOORBOARD — DAMAGED (PAX CABIN) · airframe 26,646 hrs · 11,735 cycles

PASSENGER COMPARTMENT FLOOR BOARD 222DF R/H FWD CORNER OF BOARD INSERT RIPPED OUT CORE; UPPER AND LOWER SKIN PLIES ARE DAMAGED / REPAIRED PASSENGER COMPARTMENT FLOORBOARD 222DF R/H FWD CORNER IAW B737 SRM 53-00-50-2R-6 REPAIR REV 68 PARA 3

Part: ANGLE — CORRODED (AFT CARGO) · airframe 26,646 hrs · 11,735 cycles

AFT CARGO COMPARTMENT RIGHT SIDEPLATE STA 727F+20 TO 767 RBL21 WL155 HAS CORROSION ON UPPER SURFACE / REMOVED CORROSION IN AFT CARGO R/H SIDE ZEE ANGLE AT STA 727I ORIG 'T' IS .040. REMAINING .033 LOSS OF .007 OUT OF LIMITS IAW SRM 53-00-53-1A-2 REPLACED R/H ZEE ANGLE SECTION FROM STA 727 TO 767 IAW SRM 53-00-53-2R-5 ACCOMPLISHED BONDED NUTPLATE CHECK IAW SRM 51-40-01-2R-0 INSTALLED IAW BOEING DRAWING 146A7500 SHEET 213

Part: SHIELD — CORRODED (BS 767-787) · airframe 26,150 hrs · 11,494 cycles

AFT CARGO COMPARTMENT FORWARD SHIELD HAD CORROSION ON UPPER AND LOWER SURFACE BETWEEN BS. 767 TO BS. 787, RBL 22. / R&R SHIELD IAW SRM AND DWG.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,150 hrs · 11,494 cycles

FLOOR BOARD 221DF L/H AFT BOTTOM SIDE OF BOARD SKIN PLIES AND CORE WAS DAMAGED (BROKEN/ MISSING). / REPAIRED FLOORBOARD IAW SRM.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 26,646 hrs · 11,735 cycles

PASSENGER CABIN FLOOR SUPPORT T-CAP AT STA 947 FROM LBL 12-RBL12 W/L 208 HAS AREAS OF CORROSION ON THE UPPER AND LOWER AFT FLANGE / EVALUATED CORROSION ON UPPER AND LOWER SURFACE STA ' 'STA 947; T-CAP; P/N 147A5504-29; LBL 12 TO RBL 12 ' 'AND WL 208; ORIGINAL THICKNESS .180' LOSS OF .045' ' 'REMAINING .135' FOUND TO BE OUT OF LIMITS IAW SRM ' '53-70-51-1A-1. REPAIRED T-CAP IAW EA 200180 IR AND ' 'SWA EA REPAIR-53EA-07848 P/N 147A5504-29

Part: FLOOR SUPPORT — CRACKED (BS 277-294 RBL1) · airframe 26,646 hrs · 11,735 cycles

PASSENGER COMPARTMENT BETWEEN STA 277 AND 294.5 RBL 01 INTERCOSTAL IS CRACKED AS MARKED / REMOVED AND REPLACED PASSENGER COMPARTMENT FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 277 AND 294.5 BL O' SRM 51-40-02-0G-0 DWG 141A5400 SHEET 20 REV- AND AMM 51-21-91-620-802. VERIFIED NEW PART IAW DWG 141A5400 SHEET 1 REV - P/N 141A5410-3 ATAG WN6747

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 26,150 hrs · 11,494 cycles

PASSENGER COMPARTMENT BETWEEN INTERCOSTAL WAS CRACKED BETWEEN BS. 277 TO BS. 294.5, RBL 01. / R&R INTERCOSTAL IAW SRM & DWG.

Part: LENS — MISSING (CABIN) · airframe 26,150 hrs · 11,494 cycles

MAIN CABIN COMPARTMENT FORWARD LAV EMERGENCY LIGHT HANGING INSIDE THE LAV WAS MISSING IT'S LENS. MAIN CABIN COMPARTMENT FORWARD LAV, EMERGENCY LIGHT LENS REPLACED IAW AMM 33-51-01-960-802 A-TAG WN7967 P.N . 5330007

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,150 hrs · 11,494 cycles

PASSENGER CABIN FLOOR SUPPORT T-CAP AT STA 947 FROM LBL 12-RBL12 W/L 208 HAS AREAS OF CORROSION ON THE UPPER AND LOWER AFT FLANGE EVALUATED CORROSION ON UPPER AND LOWER SURFACE STA / STA 947, T-CAP, P/N 147A5504-29, LBL 12 TO RBL 12 / AND WL 208, ORIGINAL THICKNESS .180" LOSS OF .045" / REMAINING .135" FOUND TO BE OUT OF LIMITS IAW SRM / 53-70-51-1A-1. REPAIRED T-CAP IAW EA 200180 IR AND / SWA EA REPAIR-53EA-07848 P/N 147A5504-29

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 26,646 hrs · 11,735 cycles

FWD CARGO COMPARTMENT AFT CORNER SCUFF PLATE IS CRACKED / RECEIVED WELDED FWD CARGO COMPARTMENT AFT CORNER SCUFF PLATE ON W/O 40508-1400-0002. WELD ACCOMPLISHED IAW SRM 53-30-15-2R-1

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 26,646 hrs · 11,735 cycles

FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE IS CRACKED / RECEIVED WELD FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE ON W/O 40508-1400-0001. WELD ACCOMPLISHED IAW SRM 53-30-15-2R-1

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 26,646 hrs · 11,735 cycles

AFT CARGO PIT PANEL 140CF L/H UPPER SURFACE EDGE HAS SIGNS OF CORROSION FROM AFT EDGE TO 3' FROM AFT EDGE. / AFT CARGO PIT PANEL 140CF L/H UPPER SURFACE EDGE HAS SIGNS OF CORROSION FROM AFT EDGE TO 3' FROM AFT EDGE. EVALUATED CORROSION IAW SRM 53-00-53-1A-1 FIG 102; FOUND TO BE OUT OF LIMITS. PART REPLACEMENT ACCOMPLISHED ON WORK ORDER 40506/1000/0037. P/N 453A2610-18

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 26,646 hrs · 11,735 cycles

FWD CARGO COMPARTMENT FLOOR PANEL #120CF HAS A SMALL AMOUNT OF CORROSION ALONG THE EDGES. / BLENDED OUT CORROSION ON PANEL 120CF ON EDGE OF PANEL FOUND TO BE OUT OF LIMITS FABRICATED NEW ONE IAW BOEING DWG 146A1610 P/N 43341610-103.

Part: PLATE — CORRODED (AFT CARGO) · airframe 26,646 hrs · 11,735 cycles

AFT CARGO PIT PANEL 140CF FWD TRANSITION PLATE LOWER SURFACE HAS SIGNS OF CORROSION. / REMOVED CORROSION FROM AFT CARGO PANEL 140 CF FWD TRANSITION PLATE LOWER SURFACE IAW SRM 51-10-02-0G-0. CORROSION ON PLATE OVER 30 PERCENT OF THE PART. OUT OF LIMITS IAW SRM 53-00-53-1A-1. RECIEVED NEW PART IAW IPC 25-52-10-02 ITEM 70 SH 4. REPLACED AFT CARGO PIT TRANSITION PLATE IAW SRM 51-40-02-0G-0 A TAG# A23480

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 26,646 hrs · 11,735 cycles

FWD CARGO COMPARTMENT FLOOR PANEL #120DF HAS CORROSION ALONG THE EDGES. / BLENDED OUT CORROSION ALONG THE EDGE'S FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A-1; FABRICATED NEW ONE IAW BOEING 737 DWG 453A1610 AND AMM 25-52-01-70-1-80.P/N 433A1610-20.

Part: PLATE — CORRODED (AFT CARGO) · airframe 26,646 hrs · 11,735 cycles

AFT CARGO PIT PANEL 140CF AFT TRANSITION PLATE LOWER SURFACE HAS SIGNS OF CORROSION. / RECIEVED NEW TRANSITION PLATE OLD PLATE WAS OUT OF LIMITS NEW PLATE PARTS # IS 146A9401 IAW BOEING DRAWING 146A9401 REV D EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA

Part: ANGLE — CRACKED (RT WING TE) · airframe 26,629 hrs · 11,728 cycles

R/H WING TRAILING EDGE ORSS. 271, ATTACH ANGLE FROM LATERAL WEB COMMON TO DEFLECTION CONTROL RIB CRACKED AT FASTENER LOCATIONS APPROXIMATELY 12" FROM REAR SPAR GOING AFT. / R&R ATTACH ANGLE IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (RT WING TE) · airframe 26,646 hrs · 11,735 cycles

RH WING TRAILING EDGE. ORSS 271; ATTACH ANGLE FROM LATTERAL WEB COMMON TO DEFLECTION CONTROL RIB IS CRACKED AT FASTNER LOCATIONS. APPROX 12' FROM REAR SPAR GOING AFT. / REMOVED AND REPLACED RH WING TRAILING EDGE ORSS 271 ATTACH ANGLE COMMON TO DEFLECTION CONTROL RIB IAW SRM 51-40-02-0G-0 AND DWG 15A6200 SHEET 7 REV A. VERIFIED NEW ATTACH ANGLE P/N 115A6260-2 IAW AIPC 52-42-51-03 AND DWG 115A6200 SHEET 7 REV A. ATAG A17229

Part: LENS — CRACKED (CABIN) · airframe 26,150 hrs · 11,494 cycles

PASSENGER CABIN SMALL EMERGENCY LIGHT LENSE AND RETAINER IN LIGHT BALENCE ABOVE SEAT ROW 23 ABC STOWBIN PLACARD HAS MULTIPLE CRACKS REPLACED LIGHT LENSE ON SEAT ROW (23 ABC) STOWBIN ON BULL NOSE PANEL I/A/W B737-800 AMM 35-51-03-960-803 (A23942)

Part: NOZZLE — DEBONDED (NR 2 ENG EXHAUST) · airframe 26,614 hrs · 11,722 cycles

# 2 ENG EXHAUST NOZZLE PERFORATED SKIN HAS DISBOND IN AREA ZONE 1 @ 2.1 BY 3.6 INCHES AT 6 OCLOCK POSITION / R & R ENGINE EXHAUSE NOZZLE PER AMM 78-11-01 SEE NON-ROUTINE 0020349E; 0020350E. POS #2 TAG 93366 P/N OFF: 314A2630 S/N OFF: B63382 PN ON: 314A2630-103 S/N ON: B63405

Part: NOZZLE — CRACKED (NR 1 ENG EXHAUST) · airframe 26,614 hrs · 11,722 cycles

# 1 ENG HAS MULTIPLE CRACKS ON PRIMARY EXHAUST NOZZLE AT 6 O'CLOCK POSITION ON THE PERFORATED SKIN AREA. / R & R PRIMARY EXHAUST NOZZLE PER AMM 78-11-01. POS # 1; TAG/GRB NO. 1047362; P/N OFF 314A2630-103; S/N OFF B63389; P/N ON 314A2630-103; S/N ON B362542

Part: THRESHOLD WEB — CORRODED (AFT CARGO BAY) · airframe 25,040 hrs · 10,952 cycles

TRANSFERED FROM LOG PAGE 0194027E CORROSION DAMAGE FOUND ON AIRCRAFT STRUCTURE UNDER AFT CARGO SCUFF PLATE LENGTH = 1.50' X WIDTH = 0.875' X DEPTH = 0.1875 / REMOVED AND REPLACE CORRODED WEB UNDER AFT CARGO DOOR THRESHOLD PER SRM 51-40-02AMT 102665

Part: LENS — MISSING (EXIT SIGN) · airframe 23,650 hrs · 10,299 cycles

FORWARD RT SIDE LOWER OVER WING EMERGENCY EXIT SIGN COVER MISSING. INSTALLED LENS IAW AMM.

Part: SKIN — DELAMINATED (RH INBD MAIN FLA) · airframe 22,805 hrs · 9,916 cycles

RT WING INBD MAIN FLAP OUTBD AFT T/E WEDGE PANEL LOWER SKIN DELAMINATED 4.800 IN WIDE BY 12 IN LONG AND EXTENDS TO THE T/E EDGE. DELAM STARTS 6.25 IN INBD OF OUTBD EDGE. / C/W EA REPAIR - 57EA -06019 THSI IS A TIME LIMITED REPAIRINSP P44

Part: SKIN PANEL — DELAMINATED (TE FLAP) · airframe 22,430 hrs · 9,752 cycles

RT WING INBOARD MAIN FLAP OUTBOARD AFT TRAILING EDGE WEDGE PANEL LOWER SKIN DELAMINATED. REPAIRED AFT FLAP PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,652 hrs · 9,853 cycles

FORWARD LOWER OVERWING EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,652 hrs · 9,853 cycles

R1 OVERHEAD EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,652 hrs · 9,853 cycles

L1 LOWER EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,656 hrs · 9,397 cycles

OVER WING EXIT LIGHT INOP. R&R BATTERY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,105 hrs · 9,149 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT FAULTY. R&R BATTERY PACK IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 21,105 hrs · 9,149 cycles

CENTER AISLE EMERGENCY EXIT LIGHT INOP. R&R FUSES IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,105 hrs · 9,149 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. R&R LIGHT IAW AMM.

Part: ANGLE — CRACKED (BS 500H) · airframe 19,464 hrs · 8,388 cycles

FORWARD CARGO COMPARTMENT BAFFLE ANGLE CRACKED AT BS 500H. R & R THE ANGLE IAW DWG.

Part: NONE — CRACKED (FWD CARGO BAY) · airframe 20,292 hrs · 8,764 cycles

FWD CARGO COMPARTMENT; BAFFLE CLIP CRACKED AT BS 500H (AFT SIDE OF FRAME); LOCATED UNDER RH Z ANGLE / REMOVED & REPLACED FWD CARGO COMPARTMENT BAFFLE CLIP AT BS 500H IAW BOEING DWG# 143A7505 REV B

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 20,292 hrs · 8,764 cycles

PAX CABIN FLOOR BOARD 241AF; UPPER SURFACE CENTER SECTION LENGTHWISE; BANDS OF FIBERGLASS STRANDS PULLED OUT. / REPAIRED PAX CABIN FLOOR BOARD 241AF OF LOOSE FIBERGLASS STRANDS ONE LAYER ONLY ON TOP OF BOARD IAW B737 SRM 53-00-50-2R-1 REV 61 AND B737 SRM 53-00-50-2R-0 REPAIR GENERAL REV 61.

Part: STRINGER CLIP — CRACKED (BS 500I) · airframe 19,464 hrs · 8,388 cycles

FORWARD CARGO STRINGER CLIP CRACKED AT BS 500I, STRINGER 26R. R & R THE STRINGER CLIP IAW DWG & SRM.

Part: SUPPORT ANGLE — CORRODED (FWD CARGO BAY) · airframe 20,292 hrs · 8,764 cycles

FWD CARGO AFT BLKD SUPPORT ANGLE CORRODED AT BS 500IRBL 18'. MARKED. / EVALUATED CORROSION ON SUPPORT ANGLE AT BS 500I; RBL18 100% MATERIAL LOSS OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPACED DAMAGED ANGLE IAW SRM 51-40-02-0G-0 AND DWG# 143A9485 REV B

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,292 hrs · 8,764 cycles

AFT PIT FLOOR PANEL 140 DF IS CORRODED / CORROSION EXCEEDED ALLOWABLE DAMAGE LIMITS. FABRICATED NEW AFT PIT FLOOR PANEL 140 DF IAW BOEING DWG #453A2610 REV:K SMAL #7253767-06

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,292 hrs · 8,764 cycles

AFT PIT FLOOR PANEL 140 EF IS CORRODED / REPLACED AFT PIT FLOOR PANEL 140 EF IAW SRM 51-40-02-0G-0 & IPR 25-52-10-19 ATAG WT 0868.

Part: STRINGER CLIP — CRACKED (FWD CARGO BAY) · airframe 20,292 hrs · 8,764 cycles

FWD CARGO STRINGER CLIP CRACKED AT 500I S 26R. MARKED. / REMOVED & REPLACED FWD CARGO STRINGER CLIP AT 500I S 26R IAW BOEING DWG# 143A7505 REV B & SRM 51-40-02-0G-0

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 20,292 hrs · 8,764 cycles

PAX CABIN FLOOR BOARD 241EF; UPPER SURFACE OTBD AFT CORNER PEELED UP. / REPAIRED PAX CABIN FLOORBOARD 241EF OF UPPER SURFACE DAMAGE ONE PLY ONLY IAW B737 SRM 53-00-50-2R-9 REV 61 AND B737 SRM 53-00-50-2R-0 REPAIR GENERAL REV 61.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,292 hrs · 8,764 cycles

AFT PIT FLOOR PANEL 140 BF IS CORRODED / RECEIVED NEW AFT PIT FLOOR PANEL 140BF A-TAG# WN1399; PN# 453A2610-32; SI# 7253513; IAW IPC 25-52-10-19 PANEL IS ON WORK ORDER 37045 1000 0011 PANEL WILL BE INSTALLED ON W/O TASK CARD PANEL SIGN OFF SHEET SA-M 565S

Part: SUPPORT ANGLE — CORRODED (BS 500I) · airframe 19,464 hrs · 8,388 cycles

FORWARD CARGO AFT BULKHEAD SUPPORT ANGLE CORRODED AT BS. 500I, RBL 18. / R&R ANGLE IAW SRM AND DWG.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 20,292 hrs · 8,764 cycles

FORWARD CARGO PIT FLOOR PANEL 120AF HAS CORROSION AROUND EDGES / RECEIVED NEW FWD CARGO PIT FLOOR PANEL 120AF; A-TAG# WN1757; PN# 453A1610-14. SI# 7253765; OLD PANEL FOUND TO BE OUT OF LIMITS WITH 100% MATERIAL LOSS IAW SRM 53-00-53-1A-1; PANEL TO BE INSTALLED ON WORK ORDER 37045 1000 0011 SA-M 565S

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 20,292 hrs · 8,764 cycles

FORWARD CARGO PIT FLOOR PANEL 120DF HAS CORROSION AROUND EDGES / RECEIVED NEW FWD CARGO PIT FLOOR PANEL 120DF P/N 453A1610-20 A TAG WT 0867 IAW IPC 25-52-10-17 AFTER REMOVING CORROSION AND CHECKED LIMIT FOUND TO BE OUT OF LIMIT EXCCEDED LIMIT ALLOWED IAW SRM 51-10-02 SRM 53-00-53-1A-1

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 20,292 hrs · 8,764 cycles

AFT PIT FLOOR PANEL 140 CF IS CORRODED / RECEIVED NEW AFT PIT FLOOR PANEL 140CF; A-TAG# WN 9028; PN# 7253512; PN# 453A2610-18; IAW IPC 25-52-10-19; NEW PANEL WILL BE RETURED BACK TO THE RACK; SI# 725-3512 PANEL IS ON WORK ORDER 37045 1000 0011 FOR INSTALL.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,292 hrs · 8,764 cycles

AFT PIT FLOOR PANEL 140 AF IS CORRODED / CORROSION EXCEEDED ALLOWABLE DAMAGE LIMITS. FABRICATED NEW AFT PIT FLOOR PANEL 140AF IAW BOEING DWG #453A2610 REV E AND SMAL #270151097.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 20,292 hrs · 8,764 cycles

AFT CARGO COMPARTMENT R/H Z ANGLE AT STA 767-787+7 IS CORRODED / REMOVED AND INSTALLED A NEW AFT CARGO COMPARTMENT R/H Z ANGLE AT STA 767-787+7 (SHEILD) I/A/W SRM 51-40-02-0G-0 AND BOEING DRAWING 146A8127

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 20,292 hrs · 8,764 cycles

AFT CARGO COMPARTMENT R/H Z ANGLE AT STA 727F+10 TO 767 IS CORRODED / DRILLED OFF AFT CARGO R/G ZEE CHANNL AT STA 727 H+10 TO 767 AND REPLACED 2 ANGLE AND REPAIR SPLICE IAW SRM 53-00-53-2R-5 AND BOEING 737 DWG 146A7500 ID 0065 REV 1-

Part: PLATE — CRACKED (RT WING) · airframe 20,292 hrs · 8,764 cycles

RIGHT WING LOWER TRAILING EDGE WIGGLE PLATE JUST INBOARD OF #6 FLAP TRACK IS CRACKED ON OUTBOARD END / REMOVED AND REPLACED WIGGLE PLATE JUST INBD OF #6 FLAP TRACK IAW SRM 51-40-02

Part: PLATE — CRACKED (RT WING) · airframe 19,464 hrs · 8,388 cycles

RIGHT WING LOWER TRAILING EDGE WIGGLE PLATE JUST INBOARD OF THE NR 6 FLAP TRACK, CRACKED ON THE OTBD END. R & R THE WIGGLE PLATE IAW SRM.

Part: ANGLE — CORRODED (BS 727E-807) · airframe 19,464 hrs · 8,388 cycles

AFT CARGO BAY LT ZEE ANGLE CORRODED BETWEEN BS 727E TO 807. REPAIRED THE ZEE ANGLE IAW SRM.

Part: ANGLE — CORRODED (BS 767-787) · airframe 19,464 hrs · 8,388 cycles

AFT CARGO BAY RT ZEE ANGLE CORRODED BETWEEN BS 767 TO 787+7. R & R THE ZEE ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 727F-767) · airframe 19,464 hrs · 8,388 cycles

AFT CARGO BAY RT ZEE ANGLE CORRODED BETWEEN BS 727F+10 TO 767. R & R THE ANGLE IAW SRM AND DWG.

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 20,292 hrs · 8,764 cycles

LH MAIN WHEEL WELL STA 663 VAPOR BARRIER BULKHEAD CRACKED. / ACCOMPLISHED COMPOSITE REPAIR ON STA 663 VAPOR BARRIER LH BULKHEAD IAW SRM 51-70-04-2R-10 AND 5710-10-2R-2

Part: BULKHEAD — CRACKED (BS 663) · airframe 19,464 hrs · 8,388 cycles

LEFT MAIN WHEEL WELL BULKHEAD CRACKED AT BS 663. REPAIRED THE BULKHEAD IAW SRM.

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 19,435 hrs · 8,371 cycles

LEFT WING BOX; PANEL 192CL; VAPOR BARRIER 8' CRACK; WHEEL LOWER LEFT PANEL / ACCOMPLISHED INTERIM REPAIR IAW SRM 57-10-10 (SRM 57-10-10-1A-2)

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 17,942 hrs · 7,697 cycles

LT WING BOX WHEEL LOWER LT PANEL192CL VAPOR BARRIER CRACKED. REPAIRED BARRIER IAW SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 17,979 hrs · 7,713 cycles

MAIN CABIN PHOTO LUMINESCENT TRACK LIGHT DIRTY CRACKED. R&R LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 17,979 hrs · 7,713 cycles

EXTERNAL EMERGENCY LIGHT INOP AT BS 727F+12, BETWEEN STR 21R TO STR 22R. RELAMPED LIGHT PER AMM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 17,979 hrs · 7,713 cycles

SKIN CREASED AT BS 727G, STR 23L. REPAIRED SKIN PER ER AND EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 17,979 hrs · 7,713 cycles

SKIN CREASED AT BS 727G, STR 23R. REPAIRED SKIN PER ER AND EA.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 14,620 hrs · 6,199 cycles

LEFT OVERWING EMERGENCY EXIT DOOR SIGN LENS MISSING. INSTALLED LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 12,575 hrs · 5,291 cycles

LEFT EMER LIGHT LENS CRACKED, BETWEEN ROW 8 - 12. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 12,575 hrs · 5,291 cycles

RIGHT EMER LIGHT LENS CRACKED AT ROW 25. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 12,575 hrs · 5,291 cycles

RIGHT EMER LIGHT LENS CRACKED AT ROW 14. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 11,668 hrs · 4,893 cycles

LEFT OVERHEAD BIN EMER LIGHT LENS CRACKED, BETWEEN ROW 15 - 27. R & R LENS IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 10,911 hrs · 4,564 cycles

RIGHT REAR GALLEY EMER EXIT LIGHT COVER LOOSE. SECURED LENS IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 8,964 hrs · 3,703 cycles

RIGHT AFT OVERWING EMER EXIT EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 5,580 hrs · 2,227 cycles

FWD ENTRY DOOR EMERGENCY EXIT SIGN LIGHT BROKEN. R & R LIGHT IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 5,538 hrs · 2,206 cycles

R1 DOOR EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS IAW SIP.

Part: BATTERY — DISCHARGED (CABIN) · airframe 4,289 hrs · 1,675 cycles

MID CABIN EMERGENCY EXIT SIGN INOPERATIVE. R&R BATTERY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,613 hrs · 1,411 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE. SECURED LIGHT IAW MM.

Part: WIRE — LOOSE (CABIN) · airframe 3,607 hrs · 1,408 cycles

LT OVERWING EMERGENCY LIGHTS INOPERATIVE. SECURED WIRES IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,613 hrs · 1,411 cycles

OVERWING EMERGENCY LIGHT INOPERATIVE. SECURED LIGHT IAW MM.

Part: CLOSEOUT PANEL — MISSING (EXIT SIGN) · airframe 3,425 hrs · 1,340 cycles

CENTER AISLE EMERGENCY EXIT SIGN MISSING AFT CLOSEOUT PANEL. INSTALLED SIGN IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 2,878 hrs · 1,123 cycles

RIGHT EMERGENCY LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM.

Part: COVER — BROKEN (CABIN) · airframe 2,878 hrs · 1,123 cycles

RIGHT EMERGENCY LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 2,159 hrs · 826 cycles

MID CABIN CEILING MOUNTED EMERGENCY EXIT LIGHT HOUSING OUT OF POSITION. REPOSITIONED COVER PER MM.