N918WN

ATA 3350

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,268 hrs · 25,178 cycles

FWD ENTRY DOOR EXTERIOR EMERGENCY LIGHT IS INOPERABLE. RELAMPED FWD ENTRY DOOR EXTERIOR EMERGENCY LIGHT AND PERFORMED GOOD OPERATIONAL TEST, PER AMM 33-51-04-960-801.

ATA 5347

Part: SEAT TRACK — WORN (COCKPIT) · airframe 42,267 hrs · 25,177 cycles

F/O'S INBOARD AFT SEAT TRACK WORN AT LOCK HOLES. REMOVED & REPLACED F/O'S INBOARD AFT SEAT TRACK, PER SOPM 20-50-01 & AMM 25-11-01-400-801 & AMM 25-11-11-400-801. OPERATIONAL CHECK OF F/O'S SEAT GOOD.

ATA 5347

Part: SEAT TRACK — WORN (COCKPIT) · airframe 42,267 hrs · 25,177 cycles

CAPTAIN INBOARD AFT SEAT TRACK WORN AT LOCK HOLES. REMOVED & REPLACED CAPTAINS INBOARD AFT SEAT TRACK, PER SOPM 20-50-01 AMM 25-11-11-400-801 & AMM 25-11-01-400-801. OPERATIONAL CHECK OF CAPTAINS SEAT GOOD.

ATA 5347

Part: SEAT TRACK — CORRODED (BS 580) · airframe 42,253 hrs · 25,177 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT BS 580 RBL 24.5 WL 208.1. REMOVED CORROSION ON PASSENGER CABIN SEAT TRACK BS 580 RBL 24.5 WL 208.1. MAXIMUM MATERIAL LOSS ON THE TOP SURFACE OF THE TRACK L=1.3' D=0.017' AND L=1.8' D=0.009' IN THE BOTTOM OF THE TRACK, FOUND TO BE WITHIN LIMITS. APPLIED CHEMICAL CONVERSION COATING AND ALUMINIZED EPOXY PRIMER, IAW SRM 53-00-52-1A-1 89004U 09SEP20.

ATA 5347

Part: SEAT TRACK — CORRODED (BS 594) · airframe 42,267 hrs · 25,177 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT BS 594 RBL 45 WL 208.1. REMOVED CORROSION ON PASSENGER CABIN SEAT TRACK BS 594 RBL 45 WL 208.1. MAXIMUM MATERIAL LOSS ON THE TOP SURFACE OF THE TRACK L=3.7' D=0.008' AND L=3' D=0.015' IN THE BOTTOM OF THE TRACK, FOUND TO BE WITHIN LIMITS. APPLIED CHEMICAL CONVERSION COATING AND ALUMINIZED EPOXY PRIMER, IAW SRM 53-00-52-1A-1 89004U 09SEP20.

ATA 3350

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 42,267 hrs · 25,177 cycles

ALL EMERGENCY LIGHT BATTERY PACKS FAIL CAPACITY CHECK. REPLACED & PERFORMED A GOOD INSTALLATION TEST OF ALL EMERGENCY LIGHT BATTERY PACKS, PER AMM 33-51-06-960-805.

ATA 2560

Part: HOOK — OUT OF ADJUST (L1 DOOR GIRT BAR) · airframe 42,179 hrs · 25,128 cycles

FO SIDE FWD ENTRY DOOR GIRT BAR J HOOK DIFFICULT TO ENGAGE / ADJUSTED FWD SERVICE DOOR GIRT J HOOK IAW SIP OK TO CONTINUE SERV

ATA 2565

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 41,842 hrs · 24,910 cycles

L1 DOOR SLIDE DROPPING. REPOSITIONED L-1 FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE AS PER MT 725-61-06.

ATA 3350

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,374 hrs · 24,603 cycles

AISLE LIGHT @ SEAT 9 & 11 ABC INOP (REPLACE EMERGENCY BATTERY PACK M1675) / RECHARGE BATTERY PACKS IAW AMM 33-51-06-610-802 PERFORMED EMERGENCY LIGHT OPERATIONAL TEST IAW 33-51-00-710-801. CHECK GOOD. AISLE LIGHT AT SEATS 9 AND 11 CHECK GOOD.

ATA 5330

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

POWER RECEPTACLE DOOR INTERNAL SURROUND DOUBLER CRACKED ON AFT SIDE WHERE DOOR CONTACTS / REPAIRED INTERNAL SURROUND DOUBLER OF POWER RECEPTACLE DOOR IAW B737 SRM 53-10-15-2R-4. ATAG A41234

ATA 5753

Part: SKIN — DELAMINATED (TE FLAP) · airframe 41,374 hrs · 24,603 cycles

REFERENCE INBOUND DMI D197994: R/H O/B AFT FLAP; LOWER SURFACE; 82' O/B OF I/B EDGE AND 4.75' FWD OF T/E HAS A DELAMINATED DENT (MARKED) / REPAIRED LOWER SURFACE OF R/H O/B AFT FLAP; 82' O/B OF I/B EDGE AND 4.75' FWD OF T/E; IAW SRM 51-70-10-2R-0

ATA 5321

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN FLOOR PANEL;242LF PUNCTURE MID PANEL AND 9' AFT OF FWD END / REPAIRED PUNCTURE ON FLOOR PANEL 242LF LOCATED MID PANEL AND 9' AFT OF FWD END IAW SRM 53-00-50-2R-3 PARA 3

ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN FLOOR PANEL;231AF AFT LH CORNER DELAMINATED / PASSENGER CABIN FLOOR PANEL 231AF; AFT L/H CORNER DELAMINATION REPAIRED IAW SRM 53-00-50-2R-10 PARA 3 STEPS A TO G

ATA 5321

Part: INSERT — MISSING (FLOOR PANEL) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN FLOOR PANEL;231DF MISSING MID INSERT 20' AFT OF FWD END / FABRICATED FLOOR BOARD 231DF PER SAMPLE IAW SRM 53-00-50-2R-0 PER DRW# 143A5810/513 & BAC 5085

ATA 5321

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN FLOOR PANEL;242AF PUNCTURE OUTBD EDGE 31' AFT OF FWD END / REPAIRED PUNCTURE IN FLOOR PANEL 242AF 31' AFT OF FWD EDGE ON OUTBD SIDE IAW SRM 53-00-50-2R-2 PARA 3

ATA 5321

Part: FLOOR PANEL — PEELING (CABIN) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN FLOOR PANEL;232FF FWD INBD CORNER COVERING PEELING / REPAIRED FWD INBD CORNER ON FLOORBOARD 232FF IAW SRM 53-00-50-2R-4; PG'S 1; 2; STEPS 3(A-N). CURED INSERTS 4 EA FOR 1 HOUR AT 150 DEGREES BY HEAT LAMP IAW SRM 53-00-50-2R-0; PG'S 11; 12; STEPS 5(A-H).

ATA 5210

Part: ACCESS PANEL — CRACKED (L2 DOOR) · airframe 41,374 hrs · 24,603 cycles

L2 DOOR ACCESS PANEL 834DZ; AFT ATTACH FRAME CRACKED. / REMOVED AND REPLACED L2 DOOR ACCESS PANEL 834DZ ASSEMBLY IAW SRM 51-40-02-0G-0 STEPS 8 E; AND 9B ATAG: WN7232

ATA 5342

Part: SKATE ANGLE — WORN (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

UPPER FUSELAGE L/H FWD SKATE ANGLE IS WORN AS MARKED / REMOVED DAMAGE AT L/H FWD SKATE ANGLE IAW SRM 53-80-13-1A-1. ORIGINAL THICKNESS .063' AFTER REWORK. .053'; .010' MATERIAL LOSS; OUT OF LIMITS IAW SRM 53-80-13-1A-1 FIG 104. TOOL: 18173 DUE: 11/27/20. REMOVED OUT OF LIMITS L/H FWD SLATE ANGLE AND INSTALLED NEW FWD SKATE ANGLE ALL IAW SRM 51-40-02-0G-0 AND DWG: 147A0030 REV A. RESTORED FINISH IAW AMM 51-21-73-370-804. ATG#A96309

ATA 5342

Part: SKATE ANGLE — WORN (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

UPPER FUSELAGE R/H FWD SKATE ANGLE IS WORN AS MARKED / REMOVED DAMAGE AT RH FWD SKATE ANGLE IAW SRM 53-80-13-1A-1. ORIGINAL THICKNESS .063'; AFTER REWORK .050' .013' MATERIAL LOSS OUT OF LIMITS IAW SRM 53-80-13-1A-1 FIG 104. TOOL: 18173 DUE: 11/27/20 REMOVED OUT OF LIMITS SKATE ANGLE AND INSTALLED NEW SKATE ANGLE ALL IAW SRM 51-40-02-0G-0 AND DWG 147A0030 REV A. RESTORED FINISH IAW AMM 51-21-73-370-804. ATAG# SU1144

ATA 5321

Part: FLOOR PANEL — PEELING (CABIN) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN FLOOR PANEL # 221AF UPPER SURFACE PEELING. REPAIRED UPPER SURFACE PLY ON FLOORBOARD 221AF IAW SRM 53-00-50-2R-1, PG'S 1,2, STEPS 3(A+M)

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

FWD PASSENGER CABIN FLOOR BEAM STA 344 WL 208 LBL 9 UPPER SURFACE CORRODED. / REMOVED CORROSION AT FWD PASSENGER CABIN FLOOR BEAM STA 344 WL 208 LBL 9 UPPER SURFACE I/A/W SRM 51-10-02-0G-0; VERIFIED MATERIAL LOSS; ORIG .175 REMAING .132 LOSS OF .043 OUT OF LIMITS I/A/W SRM 53-10-51-1A-1; INSTALLED PERFORMED REPAIR #9 OF I/A/W SRM 53-10-51-2R-9 P/N 141A5505-19

ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN FLOOR SUPPORT STA 328+12' WL 208 LBL 11 UPPER SURFACE CORRODED. / REMOVED CORROSION AT PASSENGER CABIN FLOOR SUPPORT STA 328+12 WL208 LBL 11 UPPER SURFACE I/A/W SRM 51-10-02-0G-0; VERIFIED MATERIAL LOSS; LOSS OF ORIG. .080 REMAINING .066 LOSS OF .014 IS OUT OF LIMITS I/A/W SRM 53-10-51-1A-1; REMOVED AND INSTALLED NEW FLOOR SUPPORT AT STA 328 TO 344 WL208 LBL 11 I/A/W SRM 51-40-02-0G-0 AND BOEING DWG # 141A5400 REV:- P/N 141A5410-17

ATA 5321

Part: FLOOR PANEL — PEELING (CABIN) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN FLOOR PANEL # 222DF UPPER SURFACE PEELING. / REPAIRED UPPER SURFACE PLY ON FLOORBOARD 222DF IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS 3(A-M)

ATA 5320

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN, STA 500D+6, BL0, WL 208, FLOOR SUPPORT ANGLE IS CRACKED AT 2EA FLOOR PANEL HOLES. REMOVED FLOOR SUPPORT ANGLE @ STA 500A BL0 WL 208 IAW SRM 51-40-02-0G-0, VERIFIED NEW ANGLE AS P/N 143A5410-170 A-TAG A34417 IAW BOEING DWG 143A5400 REV: A, LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05-0G-0, AND INSTALLED NEW FLOOR SUPPORT ANGLE @ STA 500D BL0 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A5400 REV:D

ATA 5321

Part: FLOOR PANEL — PEELING (CABIN) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN FLOOR PANEL # 222CF UPPER SURFACE PEELING. REPAIRED UPPER SUFACE PLY ON FLOORBOARD 222CF IAW SRM 53-00-50-2R-1, PG'S 1,2, STEPS 3 (A-N). A21946, A29109

ATA 5310

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN STA 312 TO 344, WL 208, LBL 58, INNER CREASE BEAM CORD HAS CORROSION. REMOVED CORROSION FROM LH CREASE BEAM STA 312 TO 344 WL208 LBL58 IAW SRM 51-10-02-0G-0. VERIFIED MAT.LOSS ORIG "T" .080, MAT LOSS .011, REMAINING "T" .069 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED LH SIDE CREASE BEAM STA 259.5 TO 360 WL 208 LBL58 IAW B737 SRM 51-40-02-0G-0 AND DRAWING 141A8110 REV A MAT LOSS VERIFIED IAW SRM 53-10-15-1A-1 FIG 108 DETAIL D P/N 141A8112-1 AAR

ATA 5321

Part: FLOOR PANEL — PEELING (CABIN) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN FLOOR PANEL # 221FF UPPER SURFACE PEELING. / REPAIRED UPPER FACESHEET DAMAGED FIBERS SURFACE ON FLOORBOARD PANEL (221 FF) WITH WET-LAY-UP REPAIR I/A/W B737-700 SRM 53-00-50-2R-1 (3) A-N (REV70)

ATA 5320

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN AT STA 540 BETWEEN LBL 24 AND BL 0 EXPANSION JOINT FLOOR BOARD SUPPORT STRUCTURE IS CRACKED AT BL 0 BOTTOM SIDE AS MARKED / REMOVED CRACKED EXPANSION JOINT AT MAIN CABIN STA 540 LBL24-BLO L/H IAW SRM 51-40-02-0G-0. DRILLED NEW EXPANSION IAW SRM 51-40-05-0G-0 AND BOEING DWG 143A0060. INSTALLED NEW EXPANSION IAW SRM 51-40-02-0G-0 AND BOEING DWG 1430060

ATA 5320

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

FWD CARGO. STA 500D, STR 19R, STRINGER CLIP GUSSET IS CRACKED IN UPPER RADIUS REMOVED & REPLACED FWD CARGO STA 500D STR 19R GUSSET I/A/W SRM 51-40-02-0G-0 & BOEING DWG 143A7902 SHEET 209.

ATA 3350

Part: LIGHT — BROKEN (CABIN) · airframe 41,374 hrs · 24,603 cycles

EMERGENCY EXIT LIGHT ON FWD LAV AFT EXTERIOR WALL IS BROKEN / REMOVED AND INSTALLED NEW EMERGENCY EXIT LIGHT ON FWD LAV AFT EXTERIOR IAW AMM 33-51-01-960-802 AND PERFORMEED TEST ON EMERGENCY LIGHT ON FWD LAV AFT EXTERIOR IAW AMM 33-51-01-960-802. OP CHECK IS GOOD. A-TAG A33015.

ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

FWD PASSENGER CABIN FLOOR SUPPORT STA 312 + 13' WL 208 RBL 10 UPPER SURFACE CORRODED. / REMOVED AND REPLACED CABIN FLLOR SUPPORT AT STA 312+13' WL 208 RBL 10 IAW SRM 51-40-02 AND DRAWING 141A5400 FLOOR SUPPORT P/N 141A5410-14 REMOVED CORROSION ON CABIN ON CABIN FLOOR SUPPORT AT STA 312+13' WL 208 AND RBL 10; VERIFIED ORIGINAL THICKNESS .080' LOSS OF .011' REMAINING .069' FOUND OUT OF LIMITS IAW SRM 53-10-051--01-2 24785 23MAR20

ATA 5321

Part: FLOOR PANEL — PEELING (CABIN) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN FLOOR PANEL # 222BF UPPER SURFACE PEELING. REPAIRED UPPER SURFACE PLY ON FLOORBOAR 222BF IAW SRM 53-00-50-2R-1, PG'S 1,2 STEPS 3 (A-M)

ATA 5320

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

FWD CARGO. STA 500D, STR 19L, STRINGER CLIP GUSSET IS CRACKED IN UPPER RADIUS REMOVED AND REPLACED FWD CARGO STA 500D STR 19L GUSSET I/A/W SRM 51-40-02-0G-0 & BOEING DWG 143A7902 SHEET 209.

ATA 5321

Part: FLOORBOARD — PEELING (CABIN) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN FLOOR PANEL # 221CF UPPER SURFACE PEELING. REPAIRED UPPER SURFACE PLY ON FLOORBOARD 221CF IAW SRM 53-00-50-2R-1, PG'S 1,2, STEPS 3(A-N)

ATA 5321

Part: FLOOR PANEL — PEELING (CABIN) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN FLOOR PANEL # 221BF UPPER SURFACE PEELING. / BONDED REPAIR APPLIED TO UPPER SURFACE PEELING ON FLOOR PANEL 221BF. REPAIR C/W IAW SRM 53-00-50-2R-1 PARA 3

ATA 5320

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN AT STA 540 BETWEEN RBL 24 AND BL 0 EXPANSION JOINT FLOOR BOARD SUPPORT STRUCTURE IS CRACKED AT BL 0 BOTTOM SIDE AS MARKED / REMOVED CRACKED EXPANSION JOINT AT MAIN CABIN STA 540 BETWEEN RBL24-BLO R/H IAW SRM 51-40-02-0G-0. DRILLED NEW EXPANSION IAW SRM 51-40-05-0G-0 AND BOEING DWG 143A0060. INSTALLED NEW EXPANSION IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A0060

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

FWD PASSENGER CABIN FLOOR BEAM STA 328 WL 208 RBL 55 UPPER SURFACE CORRODED. REMOVED CORROSION AT CABIN FLOOR BEAM UPPER SURFACE STA 328 RBL 55 IAW SRM 51-10-02-0G-0 AND SRM 53-10-51-1A-1, VERIFIED WITH 10X MAGNIFICATION. ORIGINAL THICKNESS .125" AFTER REWORK .092", .033" MATERIAL LOSS OF OF LIMITS IAW SRM 53-10-51-1A-1 FIG 103. TOOL: 31896 DUE: 03/11/21. REPAIRED STA 328 FLOOR BEAM IAW SRM 53-10-51-2R-8

ATA 5347

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

MAIN CABIN SEAT TRACK AT LBL 24 STA 520 WL 208 CROWN GOUGED. / REMOVED DAMAGE TO SEAT TRACK AT STA 520 LBL24 IAW B737 SRM 51-10-02-0G-0 AND 53-00-52-1A-1. FOUND OUT OF LIMITS WITH .025' REMOVED. MAX ALLOWED .020' IAW B737 SRM 53-00-52-1A-1. REPAIRED SEAT TRACK IAW B737 SRM 53-00-52-2R-4. CHANNEL ATAG#WN7230 SEAT TRACK ATAG#WN1883

ATA 5340

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN. STA 277, STR 10R, STRINGER CLIP IS CRACKED AT FASTNER HOLE COMMON TO FRAME. ( FWD SIDE OF FRAME) REPLACED NEW STRINGER CLIP AT STA 277, STR 10R I.A.W SRM 51-40-02-0G & BOEING DWG 141A1110, TY : DWG ID:0051, REV:- A-TAG# WN6976 SI#7531655

ATA 5730

Part: PANEL — CRACKED (RT WING) · airframe 41,374 hrs · 24,603 cycles

RH WING LOWER MID SPAN TRAILING EDGE PANEL 661CB SEVERAL FASTENER HOLES CRACKED OUT ON BACK SIDE OF PANEL REPAIRED PANEL 661CB 30 CRACKED FASTENER HOLES. IAW B737-700 SRM 57-51-01-2R-1 REV 70, SRM 51-70-04-2R-9 REV 70, SRM 51-70-04-2R-0 REV 70, AMM 51-21-81-370-802 REV 70, AMM 51-21-99-300-802 REV 20, AMM 51-21-99-300-801 REV 70 A05500, A87850, A00754, A33188, A13438

ATA 5310

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN AFT WET AREA BETWEEN STA 989.5 +7' AND 947.5 RBL 51 AREA WL 208.1 R2 DOOR INNER CRESE BEAM CHORD TOP AND SIDE SURFACES AS MARKED IS CORRODED IN SEVERAL AREAS / REMOVED CORROSION ON R2 DOOR CREASE BEAM STA 989.5 RBL 51 WL 205 VERIFIED WITH 10X MAG. IAW B-737 SRM 51-10-02-0G-0. VERIFIED MAT. LOSS ORG 'T' .080; MAT LOSS .012; REMAINING MAT .068 FOUND TO BE OUT OF LIMITS. AAR TOOL 36646 DUE 05OCT20 IAW B-737 SRM 53-20-13-1A-1 FIG 103 DETAIL D. REMOVED AND REPLACED DAMAGED CREASE BEAM. IAW B-737 SRM 51-40-02-0G-0 AND DRAWING 147A8501 REV: A. ATAG# WN3366 PN 147A8540-8

ATA 5320

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

PASSENGER CABIN STA 291.5+2, STR 17R, ATTACH ANGLE IS CRACKED IN RADIUS. ANGLE COMMON TO CREASE BEAM WEB TO INNER CREASE BEAM CORD. REPLACED NEW CLIP AT STA 291.5+2", STR 17R IAW SRM 51-40-02-0G-0 & BOEING DWG # 141A8310, TY" DWG ID: 0001, REV:D.

ATA 3397

Part: CONNECTOR — MISSING (EXIT SIGN) · airframe 41,374 hrs · 24,603 cycles

FWD LAV; EMERGENCY EXIT SIGN HAS A ELECTRICAL CONNECTOR MISSING. / REPLACED; & PERFORMED OPS CHECK ON FWD LAV EMERGENCY EXIT SIGN IAW SWPM 20-30-12 PG 349-350; & AMM 33-51-00-710-801; OPS CHECK GOOD REPLACED CONNECTOR A TAG: A95882; A91184

ATA 5347

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

MAIN CABIN SEAT TRACK AT LBL 45 STA 520 WL 208 CROWN GOUGED. / BLENDED OUT GOUGED AREA AT MAIN CABIN SEAT TRACK AT LBL 44 STA 520 WL208 IAW SRM 53-00-52-1A-1. VERIFIED MATERIAL LOSE REMOVED .038 ON TOP ALLOWABLE .020 MAX FOUND OUT OF LIMITS US OF AAR TOOL #3606 DUE 06/26/20 IAW SRM 53-00-52-1A-1. CUTOUT DAMAGED SEAT TRACK AT STA 500 C+10 IAW SRM 53-00-52-2R-4 DRILLED AND C/S REPAIR SEAT TRACK AND REPAIR CHANNEL IAW SRM 53-00-52-2R-4 INSTALLED REPAIR PARTS IAW SRM 53-00-52-2R-4

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

AFT CARGO COMPT. BS 887; LBL9 - RBL22; WL169 FLOOR BOARD SUPPORT HAS CORROSION UPPER SURFACE / REMOVED AND REPLACED AFT CARGO STA 887 LBL 9- RBL 22 FLOOR SUPPORT / PANEL SPLIED I/A/W SRM 51-40-02-0G-0 & BOEING DWG 146A9401 SHEET 12 REV A. SUPPOT PANEL SPLICE FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED SRM LIMITS REPAIRED BY REPLACEMENT I/A/W SRM 51-10-02-0G-0 PARA 9C. P/N 146A9401-39

ATA 5320

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

AFT CARGO COMPT. BS 727B+10 - BS 767, RBL22, WL155 Z-ANGLE HAS CORROSION ON UPPER SURFACE (MARKED) REMOVED AND REPLACED "Z" ANGLE AFL CARGO RBL 22 STA 727-807 I/A/W SRM 51-40-02-0G-0 & BOEING DWG 146A7502 SHEET 28. W/ NEWLY FABRICATED 146A7502-30 "Z" ANGLE. EXISTING "Z" ANGLE WAS OUT OF LIMITS ORIG "T" .032", REMAINING .022" LOSS OF .010 I/A/W SRM 53-00-53-1A-2. P/N 146A7502-30

ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

AFT CARGO COMPARTMENT; STA 767; FRAME UPPER FLANGE DENTED JUST BELOW STR 24L. / EVALUATED DENT ON AFT CARGO STA 767 FRAME UPPER FLANGE BELOW STR 24L IAW B737 SRM 53-00-07-1A-1. NO DENTS ALLOWED. REPAIRED ON NRC Y188939 USING EA 200279 REV P1; IR AND SWA EA 1-753-36732 REV IR

ATA 5347

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 41,374 hrs · 24,603 cycles

AFT CARGO COMPT. BS 767+5; RBL8; WL156 RAIL HAS CORROSION UPPER SURFACE / REPAIRED AFT CARGO RAIL STA 767+5 RBL8 WL156 IAW EA # 1-A53-4982 REV 3. P/N 146A7503-6

ATA 5320

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

AFT CARGO COMPT. BS 727D+8 - BS 807; LBL22; WL155 Z-ANGLE UPPER & LOWER SURFACE HAS CORROSION (MARKED) / EVALUATED AFT CARGO 'Z' ANGLE STA 727D+8-807 LBL 22 ORIG 'T' .032'; REMAINING .022'; LOSS OF .010' OUT OF LIMITS I/A/W SRM 53-00-53-1A-2. REPAIRED 'Z' ANGLE FROM STA 747+10 TO STA 847 I/A/W SRM 53-00-53-2R-5. STA 727D+8 TO STA 747+10 REPAIRED ON W/O # 40560/1600/0013 DEFECT #Y188942

ATA 5347

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 41,374 hrs · 24,603 cycles

AFT CARGO COMPT. BS 767+5; RBL14; WL156 TRACK HAS CORROSION UPPER SURFACE / REPAIRED AFT CARGO TRACK STA 767+5 RBL14 WL156 IAW SRM 53-00-53-2R-3 ALT 3. P/N 146A7501-25

ATA 5320

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

AFT CARGO COMPARTMENT, WASTE TANK CLOSEOUT PANEL SUPPORT STRUCTURE HAS CRACKED ANGLE AT STA 867 LBL 10 REMOVED WASTE TANK SUPPORT BRACKET STA 867 LBL 10 IAW SRM 51-40-02-0G-0. VERIFIED NEW MATERIALS IAW BOEING DRAWING 149A8102 REV A FRAME 3 PN: 149A8109-114. DRILLED AND LOCATED NEW BRACKET IAW SRM 51-40-05-0G-0 AND BOEING DRAWING 149A810-2 REV A FRAME 3. ISNTALLED SUPPORT BRACKET IAW SRM 51-40-02-0G-0 AND BOEING DRAWING 149A8102 REV A FRAME 3. ATAG # A23474

ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

AFT CARGO COMPARTMENT; STA 767; FRAME UPPER FLANGE DENTED JUST ABOVE STR 24L. / EVALUATED DENT ON STA 767 FRAME UPPER FLANGE ABOVE STR 24L IAW B737 SRM 53-00-07-1A-1. NO DENTS ALLOWED. REPAIRED FRAME IAW EA 200279 REV P1; IR AND SWA EA 1-753-36732 REV IR

ATA 5320

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

AFT CARGO COMPT. BS 727B+6; LBL22; WL155 Z-ANGLE HAS CORROSION UPPER SURFACE (MARKED) / EVALUATED AFT CARGO 'Z' ANGLE @ STA 727B+6 LBL 22; ORIG 'T' .032; REMAINING .022 LOSS OF .010 OUT OF LIMITS I/A/W SRM 53-00-53-1A-2. REPAIRED 'Z' ANGLE FROM STA 727 TO STA 747+10 I/A/W SRM 53-00-53-2R-5. P/N 146A7502-27

ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

AFT CARGO COMPARTMENT; STA 727D; UPPER FLANGE ON FORWARD SIDE OF FRAME DENTED JUST ABOVE STR 24L. / EVALUATED AFT CARGO STA 727D ANGLE FWD SIDE OF FRAME ABOUVE STR 24L; REPAIRABLE BY REPLACEMENT I/A/W SRM 51-10-02-0G-0 PARA 9C DUE TO NO LIMITS. REPLACED ANGLE / CHANNEL I/A/W SRM 51-40-02-0G-0 & BOEING DWG 146A1220 SHEET 52 REV-.

ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

AFT CARGO COMPARTMENT; STA 727B; FRAME UPPER FLANGE DENTED AT STR 22L. / REMOVED DENT DAMAGE FROM AFT CARGO STA; 727B FRAME UPPER FLANGE @ STR 22L IAW B737 SRM 51-10-02-0G-0. REPAIRED IAW EA 200287 REV P1; IR & SWA EA 1-753-36754 REV IR.

ATA 5347

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 41,374 hrs · 24,603 cycles

AFT CARGO COMPT. BS 767+5; LBL17; WL156 TRACK HAS CORROSION UPPER SURFACE / REPAIRED AFT CARGO TRACK STA 767+5 LBL17 WL156 IAW SRM 53-00-53-2R-3 ALT 3. 146A7501-1

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,374 hrs · 24,603 cycles

AFT CARGO COMPT. BS 767+5; LBL22 - RBL22; WL156 FLOOR BOARD SUPPORT HAS CORROSION UPPER SURFACE / EVALUATED CORROSION ON AFT CARGO FLOOR BOND ED AUPPORT SPLICE STA 767+5 RBL 22-LBL22; NO PUBLISHED LIMITS REPAIRABLE BY REPLACEMENT I/A/W N SRM 51-20-02-0G-0 PARA 9C. REPLACED SUPPORT W/ NEW P/N 146A9401-4 ATAG# WN 4356 I/A/W SRM .065 LOSS 51-40-02-0G-0 & BOEING DWG 146A7500 SHEET 113. ORGINAL .065 LOSS .010 REMAINING .055 146A9401-4

ATA 5514

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 41,374 hrs · 24,603 cycles

L/H HORI. STAB.; STAB STA 120.4 RIB; CRACK IN RIB STIFFENER AT 3RD STIFFENER RIB FROM FRONT 1.0' UP FROM LOWER ATTACH FLANGE / TRIMMED OUT DAMAGED AREA OF STAB RIB AT LH STAB STA 120.4 3RD STIFFENER FROM FRONT AND FABRICATED AND INSTALLED RIB STIFFENER REPAIR IAW SRM 55-10-09-2R-4. RESTORED CIC TO DISTURBED AREA IAW AMM 51-21-91-620-802

ATA 5511

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 41,374 hrs · 24,603 cycles

RH HORIZONTAL STAB; RIB AT STAB STA 129.50 HAS CRACKED VERTICAL STIFFENER 3RD FROM L/E / TRIMMED OUT DAMAGED AREA OF STAB RIB AT RH STAB STA 129.5 3RD FROM LEADING EDGE AND FABRICATED AND INSTALLED RIB STIFFENER REPAIR IAW SRM 55-10-09-2R-4. RESTORED CIC TO DISTURBED AREA IAW AMM 51-21-91-620-802

ATA 5514

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 41,374 hrs · 24,603 cycles

RH HORIZONTAL STAB; RIB AT STAB STA 129.50 HAS CRACKED VERTICAL STIFFENER 2ND FROM L/E / TRIMMED OUT DAMAGED AREA OF STAB RIB AT RH STAB STA 129.5 2ND STIFFENER FROM LEADING EDGE AND FABRICATED AND INSTALLED RIB STIFFENER REPAIR IAW SRM 55-10-09-2R-4. RESTORED CIC TO DISTURBED AREA IAW AMM 51-21-91-620-802

ATA 5320

Part: SHIELD — CORRODED (BS 420-440) · airframe 41,374 hrs · 24,603 cycles

FWD CARGO COMPARTMENT SHIELD STA 420 TO 440; RBL 23 AND WL 156 HAS CORRSION. / REMOVED CORROSION ON FWD CARGO SHIELD 420-440-22C23 IAW SRM 51-10-02-0G-0 USED 10X MAGNIFYING GLASS NO FURTHER DAMAGE. FOUND TO BE OUT OF LIMITS IAW 53-30-15-1A-1 FIG 103. '0'THICKNESS .032 LOSS OF .006 REMAINING .026 AAR TOOL 36647 CAL 6-7-20. VERIFIED MATERIALS IAW BOEING DWG 143A0080 REV P/N: 143A8126-21. LOCATED AND DRILLED IAW SRM 51-40-05-06. INSTALLED CARGO

ATA 5320

Part: SHIELD — CORRODED (BS 492-500A) · airframe 41,374 hrs · 24,603 cycles

FWD CARGO COMPARTMENT SHIELD STA 492 TO 500A; RBL 23 AND WL 156 HAS CORRSION. / REMOVED CORROSION ON FWD CARGO SHIELD STA 492-500A RBL 23 IAW SRM 51-10-02-03-0. USED 10X MAGNIFYING GLASS NO FURTHER DEFECTS FOUND TO BE OUT OF LIMITS. IAW 53-30-15-1A-1 FIG 103. 'O' THICKNESS.032 LOSS AT .005 REMAING .027. AAR TOOL 36647 CAL DUE 6-7-20. VERIFIED MATERIALS IAW BOEING DWG 143A0080 REV- AND BOEING PARTS PAGE PN 143A812603. LOCATED AND DRILLED IAW SRM 51-40-05-06-0.