N8318F

Part: CIRCUIT BREAKER — BROKEN (ZONE 200) · airframe 44,098 hrs · 20,867 cycles

CIRCUIT BREAKER P6-11 A9 BROKEN. CABIN EMER LIGHTS. REMOVED AND REPLACED CIRCUIT BREAKER P6-11 A9 IAW AMM 20-60-05.

Part: HANDLE — BROKEN (ZONE 800) · airframe 43,854 hrs · 20,750 cycles

R1 DOOR CLOSING ASSIST HANDLE BROKEN., REPLACED HANDLE NUT IN REF W/ MM 52-41-31.

Part: GROUND WIRE — LOOSE (ZONE 800) · airframe 43,178 hrs · 20,402 cycles

AFT ENTRY DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. FOUND SHORT IN EMERGENCY LIGHT ASSY. BEGIN REMOVAL PROCCESS IAW AMM 33-51-04-960-802. COMPLIED UP TO STEP F, 2. FOUND GROUND LOOSE AT HOUSING FIXTURE. SECURED GROUND AND REASSEMBLED IAW AMM 33-51-04. OPS CHECKED NORMAL.

Part: LIGHT — MISSING (ZONE 200) · airframe 42,844 hrs · 20,221 cycles

MID CABIN OVERHEAD CEILING EXIT LIGHT ASSY IS MISSING 2X CLOSE OUT COVERS<[01] INSTALLED CLOSE OUT COVERS ON MID CABIN OVERHEAD EXIT LIGHT ASSEMBLY PER AMM 33-51-01-960-802 STEP 3.C.(10);[02] VERIFIED CORRECTIVE ACTION STEP 1.

Part: HANDLE — LOOSE (ZONE 800) · airframe 42,241 hrs · 19,920 cycles

FWD ENTRY DOOR L1 UPPER ASSIST HANDLE IS LOOSE. RESECURED FWD ENTRY DOOR UPPER ASSIST HANDLE REF AMM 20-50-11.

Part: SKIN — DELAMINATED (LT TE FLAP) · airframe 39,388 hrs · 18,408 cycles

LH WING; OUTBOARD AFT FLAP; LOWER SKIN DELAMINATED. 7 1/2 INCH X 7 1/2 INCH; 5 INCHES FROM TRAILING EDGE; 6 INCHES FROM INBOARD EDGE.<[01] REPLACED LH WING; O/B AFT FLAP PER AMM 27-51-22. OPS CHECK GOOD;[02] 02 - INSPECTED PER [AMM 27-51-22-401-NG (OUTBOARD AFT FLAP - REMOVAL/INSTALLATION - PERMANENT)]

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHTS) · airframe 38,855 hrs · 18,136 cycles

EMERGENCY LIGHTS AT L1 DOOR DO NOT STAY 'ON' FOR MORE THAN TEN SECONDS WHEN SWITCH IS SELECTED TO ON POSITION.<[01] PERFORMED TROUBLESHOOTING OF EMERGENCY LIGHTS L1 AS PER B737 SSM 33-51-12; FOUND BATTERY PACK M1675 DEFECTIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT POS M01675 AND PERFORMED INSTALLATION TEST AS PER B737 AMM TASK 33-51-06-960-805. TEST PASS.;[02] VERIFIED STEP 1

Part: WEB — DAMAGED (HORIZONTAL STAB) · airframe 38,855 hrs · 18,136 cycles

HORIZONTAL LOWER BEAM STA 1088 HAS THE -1 REPAIR REPLACEMENT WEB WITH MULTIPLES RIVET HOLES ELONGATED. (FABRICATE NEW PART AS PER WIP)<[01] REMOVED -1 REPLACEMENT WEB AND FABRICATED NEW PER EA 24-153-01328; INSTALLATION WILL BE ACCOMPLISHED ON EA 24-153-01328 WIP 6 STEP 13.;[02] VERIFIED STEP 1

Part: DOUBLER — DAMAGED (HORIZONTAL STAB) · airframe 38,855 hrs · 18,136 cycles

HORIZONTAL LOWER BEAM STA 1088 HAS THE -2 REPAIR DOUBLER WITH FEW RIVET HOLES ELONGATED. CORRECTION TO DESCRIPTION....HORIZONTAL LOWER BEAM STA 1088 HAS THE [1] REPAIR DOUBLER WITH FEW RIVET HOLES ELONGATED.<[01] COMPLETED FABRICATION OF NEW REPAIR DOUBLER; COMPLETED FABRICATION OF NEW REPAIR DOUBLER IAW EA24-153-01328 WIP 2 STEP 3. TREATED AND PRIMED REPAIR PARTS PER REF AMM 51-21-41-370-803; AMM 51-21-72-370-804.

Part: SHIM — DAMAGED (HORIZONTAL STAB) · airframe 38,855 hrs · 18,136 cycles

HORIZONTAL LOWER BEAM STA 1088 HAS THE -3 SHIM WITH FEW RIVET HOLES ELONGATED.<[01] COMPLETED FABRICATION OF REPAIR SHIM; MATERIAL: 0.010-INCH 2024-T3 CLAD SHEET PO#1685376 PER EA24-153-01328 WIP 2 STEP 5.<BR>SURFACE ROUGHNESS GUAGE B/C 171854 NO CAL DUE AND TREATED AND PRIMED SHIM PER REF AMM 51-21-41-370-803; AMM 51-21-72-370-804 LOWER BEAM STA 1088.;[02] VERIFIED STEP 1.

Part: BATTERY PACK — INOPERATIVE (EXTERIOR LIGHT) · airframe 38,855 hrs · 18,136 cycles

SEVERAL EXTERIOR AND INTERIOR EMERGENCY LIGHTS INOPERATIVE.<[01] PERFORMED TROUBLESHOOTING EMERGENCY LIGHT AS PER REF AMM 33-50 TASK 801 FOUND BATTERY PACK M2335 AND M1673 DEFECTIVE; REPLACE BATTERY PACK M2335 AND M1673 AS PER REF AMM 33-51-06-960-805; TEST PASS;[02] CORRECTION STEP 1 PERFORMED TROUBLESHOOTING EMERGENCY LIGHT AS PER REF AMM 33-50 TASK 801 FOUND BATTERY PACK M2335 AND M1673 DEFECTIVE; REPLACED BATTERY PACK M2335 AND M1673 AS PER REF AMM 33-51-06-960-805; TEST PASS;[03] VERIFIED STEP 1 AND 2;[04] VERIFIED STEP 1; 2; 3

Part: ANGLE — CRACKED (HORIZONTAL STAB) · airframe 38,855 hrs · 18,136 cycles

TAIL COMPT AT LOWER HORIZONTAL BEAM WEB HAS FWD END OF LWR WEB ANGLE CRACKED STA 1090 RBL 31. 8-5<[01] ACCOMPLISHED EA 24-153-01328. REF FAULT TTG8Q00TCRJG.;[02] ACCOMPLISHED EA 24-153-01328. REF FAULT TTG8Q00TCRJG.

Part: BRACKET — CRACKED (COCKPIT SEAT) · airframe 38,855 hrs · 18,136 cycles

SECOND OBSERVER'S SEAT ASSEMBLY STOPPER BRACKET FOR FIRST OBSERVER'S SEAT MOUNTING BRACKET IS CRACKED.<[01] REMOVED AND REPLACED SECOND OBSERVER'S SEAT ASSEMBLY STOPPER BRACKET FOR FIRST OBSERVER'S SEAT MOUNTING BRACKET AS PER B737;<BR>SRM 51-40-02-0G-0;[02] REMOVED AND REPLACED SECOND OBSERVER'S SEAT ASSEMBLY STOPPER BRACKET FOR FIRST OBSERVER'S SEAT MOUNTING BRACKET AS PER B737;SRM 51-40-02-0G-0;[03] VERIFIED CORRECTIVE ACTION.

Part: BEAM — CRACKED (BS 1088 RBL 20) · airframe 38,855 hrs · 18,136 cycles

LOWER HORIZONTAL BEAM WEB AT STA 1088+1' RBL 20 CRACKED<[01] SUMMARY EA 24-153-01328 HAS BEEN ISSUED.

Part: WEB — CRACKED (HORIZONTAL STAB) · airframe 38,855 hrs · 18,136 cycles

ACCOMPLISH HIDDEN DAMAGE INSPECTION IN TAIL COMPARTMENT AT LWR HORIZ BEAM IN AREA AFFECTED BY BENT AND CRACKED HORIZONTAL WEB BS 1088 TO 1112 BL 0 TO RIGHT SIDE FUSELAGE SKIN INCLUDING 1088 BULKHEAD. ACCOMPLISHED A PRELIMINARY DETAIL VISUAL INSPECTION OF EXPOSED AREAS AT LWR HORIZ BEAM IN AREA AFFECTED BY BENT AND CRACKED HORIZONTAL WEB BS 1088 TO 1112 BL 0 TO RIGHT SIDE FUSELAGE SKIN INCLUDING 1088 BULKHEAD SRM 51-10-04-0G-0. AFTER INITIAL 10' X 12' WEB CUTOUT; ACCOMPLISHED DVI OF EXPLOSED AREA AND GENERATED NRC 737 SRM 51-10-04-00G-0. AFTER FINAL WEB CUTOUT OF 12' X 27' ACCOMPLISHED DVI OF EXPOSED AREA NO OTHER DEFECTS NOTED 373 SRM 51-10-04-00G-0.

Part: PLATE — CRACKED (NR 1 NACELLE) · airframe 38,855 hrs · 18,136 cycles

#1 ENGINE IB FAN COWL WITH SIDE PLATE (BETWEEN ENGINE OIL ACCESS DOOR AND AFT HOLD OPEN ROD) CRACKED. REMOVED AND REPLACED SHIELD PLATE AT #1 ENGINE IB FAN COWL AS PER SRM 51-40-02-0G.;[02] VERIFIED STEP #1

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 38,855 hrs · 18,136 cycles

FWD CARGO COMPT SCUFF PLATE FWD CORNER IS CRACKED. RECEIVED AND INSTALLED SERVICEABLE FWD CORNER SCUFF PLATE IN REF WITH AMM 53-11-02/401.

Part: WINGLET — CORRODED (RT WING) · airframe 38,855 hrs · 18,136 cycles

CORROSION AT RIGHT WINGLET UPPER TIP AFT EDGE.<[01] CUT OUT DAMAGED AREA WITH CORROSSION AT RIGHT WINGLET UPPER TIP AFT EDGE AS-PER SRM 57-30-01 REPAIR 6 FIG 201 DETAIL 2.TREATED PRIMED AND TOP COATED WORKED AREAS AT RIGHT WINGLET UPPER TIP AFT EDGE. AS-PER SOPM 20-44-04 AND AMM 57-21-21-300-801;[02] VERIFIED STEP 1

Part: DOOR — CORRODED (LAV SERVICE DOOR) · airframe 38,855 hrs · 18,136 cycles

CORROSION AT TOILET SERVICE DOOR 145AL BONDING FASTENER ATTACH AREA SURFACE.<[01] CORROSION FOUND OUT OF LIMITS PER SRM 52-40-01-1A-4; REPLACED AND INSTALLED NEW TOILET SERVICE DOOR PER AMM 52-49-07-000-801 AND SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.

Part: HINGE FITTING — CORRODED (LAV SERVICE DOOR) · airframe 38,855 hrs · 18,136 cycles

TOILET SERVICE DOOR 145AL WITH CORRODED FWD AND AFT HINGE FITTINGS.<[01] ACQUIRED NEW TOILET SERVICE DOOR 145AL ON CUSTOMER TASK CARD TTG8Q00SWM0Z; FWD AND AFT HINGE FITTINGS ATTACHED ON NEW ASSEMBLY OF TOILET SERVICE DOOR. THIS TASK WILL BE ACCOMPLISHED ON TTG8Q00SWM0Z STEP 2 INSTALLATION OF TOILET SERVICE DOOR.;[02] VERIFIED STEP 1

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 38,855 hrs · 18,136 cycles

CABIN FLOOR PANEL241XF UPPER SKIN FIRST PLY TORN MISSING MATERIALIN SEVERAL AREA<[01] ACQUIRED FLOOR PANEL 241XF (PN#147A5810-18) AS PER DWG #147A5810; INSTALLATION OF FLOORBOARD 241XF WILL BE ACCOMPLISHED ON CUSTOMER TASK CARD (TTG8Q00SBRC7);[02] VERIFIED STEP 1

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 38,855 hrs · 18,136 cycles

CABIN FLOOR PANEL 221DF WITH MULTIPLE LE INSERTS CORRODED.<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00STT09;[02] VERIFIED STEP 1

Part: CAM — OUT OF ADJUST (R1 DOOR HANDLE) · airframe 38,855 hrs · 18,136 cycles

R1 DOOR HANDLE BOX CAM RUBBING AGAINST INNER SKIN BOTTOM RIVET HEADS. REMOVED AND REPLACED BLIND RIVETS AT R-1 DOOR INNER SKIN IN REF B737-800 SRM 51-40-02-0G-0; BOEING DWG# 141A6516.;[02] VERIFIED STEP 1

Part: ATTACH BRACKET — CRACKED (BS 500Y) · airframe 38,855 hrs · 18,136 cycles

FWD CARGO COMPT STA 500H ATTACHMENT BRACKET FROM SR25 TO FRAME IS CRACKED.<[01] REMOVED AND REPLACED FWD CARGO COMPT STA 500H ATTACHMENT BRACKET FROM SR25 TO FRAME IN REF WITH SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.

Part: ATTACH BRACKET — CRACKED (BS 500G) · airframe 38,855 hrs · 18,136 cycles

FWD CARGO COMPT STA 500G ATTACHMENT BRACKET FROM SR25 TO FRAME IS CRACKED.<[01] REMOVE AND REPLACED FWD CARGO COMPT STA 500G ATTACHMENT BRACKET FROM SR25 TO FRAME REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.

Part: CAM — CHAFED (R1 DOOR) · airframe 38,855 hrs · 18,136 cycles

R1 DOOR HANDLE BOX CAM HAS CHAFFING MARKS AT BOTTOM FACE.<[01] REMOVED AND REPLACED HANDLE BOX CAM R1 DOOR AS PER B737 AMM 52-41-11-400-801;[02] VERIFIED STEP 1

Part: ATTACH BRACKET — CRACKED (BS 500G) · airframe 38,855 hrs · 18,136 cycles

FWD CARGO COMPT STA 500G ATTACHMENT BRACKET FROM SL25 TO FRAME IS CRACKED.<[01] REMOVE AND REPLACE FWD CARGO COMPT STA 500G ATTACHMENT BRACKET FROM SL25 TO FRAME IN REF TO SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.;[03] CORRECTION: UPDATED MEASUREMENT TABLE.;[04] VERIFIED STEEP 3

Part: FLOOR SUPPORT — CRACKED (BS 380-400 LBL 1) · airframe 38,855 hrs · 18,136 cycles

CABIN FLOOR STRUCTURE INTERCOASTAL CRACKED AT FASTENER HOLES BETWEEN STA 380-400 LBL 13.<[01] REMOVED AND REPLACED CRACKED INTERCOSTAL AT CABIN FLOOR STRUCTURE BETWEEN STA 380-400 LBL 13 AS PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1

Part: ATTACH BRACKET — CRACKED (BS 500H) · airframe 38,855 hrs · 18,136 cycles

FWD CARGO COMPT STA 500H ATTACHMENT BRACKET FROM SL 25 TO FRAME IS CRACKED.<[01] REMOVED AND REPLACED FWD CARGO COMPT STA 500H ATTACHMENT BRACKET FROM SL 25 TO FRAME IN REF WITH SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.

Part: FLOOR SUPPORT — CRACKED (BS 344-360 BL0) · airframe 38,855 hrs · 18,136 cycles

FWD WET AREA FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 344-360 BL 0 CRACKED AT FASTENER HOLE.<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA BETWEEN STA 344-360 BL 0 AS-PER SRM 51-40-02-0G-0;[02] VERIFIED STEP 2

Part: FLOOR SUPPORT — CRACKED (BS 312-328 RBL30) · airframe 38,855 hrs · 18,136 cycles

FWD WET AREA FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 312-328 RBL 30 CRACKED.<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA FLOOR STRUCTURE BETWEEN STA 312-328 RBL 30 AS PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1

Part: FRAME — CRACKED (BS 312 LBL 33) · airframe 38,855 hrs · 18,136 cycles

PASSENGER CABIN STA 312 WL282 LBL 33 CRACKED (ABOVE L-1 DOOR CUTOUT).<[01] ACCOMPLISHED EA M-22-153-01244(737-NG-SWA-BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33BETWEEN S-5L AND S-6L;[02] VERIFIED STEP 1

Part: FLOOR SUPPORT — CRACKED (BS 312-328 LBL46) · airframe 38,855 hrs · 18,136 cycles

FWD WET AREA FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 312-328 LBL 46 CRACKED AT FASTENER HOLE.<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA FLOOR STRUCTURE BETWEEN STA 312-328 LBL 46 AS PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1

Part: FLOORBEAM — CORRODED (BS 947) · airframe 38,855 hrs · 18,136 cycles

CABIN FLOORBEAM IS CORRODED AT BS 947.15 NEXT TO LEFT AFT LAVATORY, INBOARD MOUNT. DAMAGE EVALUATION AND REPAIR OF FLOORBEAM CORROSION AT BS 947, LEFT AFT LAVATORY I/B MOUNT WILL BE ACCOMPLISHED ON CUSTOMER TASK CARD TTG8Q00SRRMT STEP 4 AND STEP 6.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · airframe 38,855 hrs · 18,136 cycles

AFT CABIN FLOOR SUPPORT BETWEEN 947.15-967 LEFT OF CENTER LINE 24 INCHES IS CORRODED. CORROSION EVALUATION AND REPLACEMENT OF FLOOR SUPPORT AT STA 947.5-967 LBL 24 WILL BE ACCOMPLISHED ON CURRENT CUSTOMER CARD TTG8Q00SRQT9; REMOVED INTERCOSTAL AT AFT CABIN BS 947.5-967 LBL 24 PER SRM 51-40-02-0G-0 AND ACQUIRED NEW INTERCOSTAL PER AIPC 53-42-51-25B. INSTALLATION OF INTERCOASTAL WILL BE ACCOMPLISHED ON CUSTOMER CARD TTG8Q00SRRMT STEP 13.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 38,855 hrs · 18,136 cycles

CABIN FLOORBEAM IS CORRODED AT 947.15 NEXT TO RIGHT AFT LAVATORY, INBOARD MOUNT. DAMAGE EVALUATION AND REPAIR OF FLOOR BEAM CORROSION AT STA 947; RIGHT AFT LAVATORY I/B MOUNT WILL BE ACCOMPLISHED ON CUSTOMER TASK CARD TTG8Q00SRRMT STEP 4 AND STEP 6.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 38,855 hrs · 18,136 cycles

CABIN FLOOR BEAM IS CORRODED AT 947.15 NEXT TO RIGHT AFT LAVATORY; OUTBOARD MOUNT.<[01] AFTER FURTHER INSPECTION NO CORROSION WAS FOUND AT CABIN FLOOR BEAM STA 947.5 AT RIGHT AFT LAVATORY O/B MOUNT. CORROSION WAS ONLY FOUND ON ADJACENT ATTACHED INTERCOASTAL AT RBL 51 STA 947-967. REPLACEMENT OF INTERCOASTAL WILL BE ACCOMPLISHED ON CUSTOMER TASK CARD TTG8Q00SRRMT ON STEP 5. REFERENCE USED: SRM 51-10-02-0G-0;[02] AFTER FURTHER INSPECTION NO CORROSION WAS FOUND AT CABIN FLOOR BEAM STA 947.5 AT RIGHT AFT LAVATORY O/B MOUNT. CORROSION WAS ONLY FOUND ON ADJACENT ATTACHED INTERCOASTAL AT RBL 51 STA 947-967; REFERENCE: SRM 51-10-01-0G;[03] CORRECTION TO STEP 2 REFERENCE: AFTER FURTHER INSPECTION NO CORROSION WAS FOUND AT CABIN FLOOR BEAM STA 947.5 AT RIGHT AFT LAVATORY O/B MOUNT. CORROSION WAS ONLY FOUND ON ADJACENT ATTACHED INTERCOASTAL AT RBL 51 STA 947-967; REFERENCE: SRM 51-10-02-0G;[04] VERIFIED STEP 3;[05] REMOVED CORRODED INTERCOASTAL AND REPLACED WITH NEW INTERCOASTAL PN147A5660-22 AT CABIN FLOOR BEAM 947.5- 967 RBL 51; PER SRM 51-40-02-0G-0; AND DWG# 147A5760;[06] VERIFIED STEP 5

Part: FLOOR SUPPORT — CRACKED (BS 276-295) · airframe 38,855 hrs · 18,136 cycles

FWD CABIN FLOOR SUPPORT IS CRACKED BETWEEN 276-294.5; 1 INCH RIGHT OF CENTER LINE. REMOVED AND REPLACED NEW FLOOR SUPPORT AT FWD CABIN BETWEEN STA 276-294.5 1 INCH RIGHT OF CENTER LINE AS-PER SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (BS 948) · airframe 38,855 hrs · 18,136 cycles

AFT PASSENGER CABIN FLOOR BEAM 947.5 CORRODED IN MULTIPLE AREAS ALONG THE FULL LENGTH OF THE BEAM<[01] ACCOMPLISHED REPAIR AT AFT PASSENGER CABIN CENTER OF FLOOR BEAM 947.5 REF SRM 53-70-51-2R-5.

Part: SKIN — DELAMINATED (LT NR 2 SLAT) · airframe 38,855 hrs · 18,136 cycles

LEFT WING SLAT # 2 UPPER SURFACE O/B T/E COMPOSITE MAY BE DELAMINATED.MARKED DOT 251-002<[01] REMOVED AND INSTALLED SERVICEABLE LEFT WING SLAT #2 AS PER AMM 27-81-21-000-801 AND AMM 27-81-21-400-801.;[02] CORRECTION TO STEP 1: REMOVED AND INSTALLED SERVICEABLE LEFT-WING SLAT #2 AS PER AMM 27-81-21-000-801 AND AMM 27-81-21-400-801.;[03] LATE ENTRY: CORRECTION TO STEP 1 AND 2 REMOVED AND INSTALLED SERVICEABLE LEFT-WING SLAT #2 AS PER AMM 27-81-21-000-801 AND AMM 27-81-21-400-801.;[04] LATE ENTRY : RII / VERIFIED ENTRY#3 FOR WORK ACCOMPLISHED.

Part: PANEL — CORRODED (RT REFUEL PANEL) · airframe 38,855 hrs · 18,136 cycles

REFUEL PANEL (P15) FACE PLATE HAS SIGN OF CORROSION AROUND FUEL QTY GAUGES.<[01] REMOVED REFUEL PANEL (P15) AS PER B737 AMM TASK 28-21-00-000-801. REMOVED REFUEL QUANTITY INDICATOR AS PER B737 AMM TASK 28-41-61-000-801<BR>REINSTALLED REFUEL QUANTITY INDICATOR AS PER B737 AMM TASK 28-41-61-400-801. INSTALLED REFUELING PANEL P15 AS PER B737 AMM TASK 28-21-00-400-801. <BR>PERFORMED P15 REFUEL PANEL INSTALLATION TEST AS PER B737 AMM TASK 28-21-00-400-801.;[02] REMOVED REFUEL PANEL (P15) AS PER B737 AMM TASK 28-21-00-000-801. REMOVED REFUEL QUANTITY INDICATOR AS PER B737 AMM TASK 28-41-61-000-801<BR>REINSTALLED REFUEL QUANTITY INDICATOR AS PER B737 AMM TASK 28-41-61-400-801. INSTALLED REFUELING PANEL P15 AS PER B737 AMM TASK 28-21-00-400-801.<BR>PERFORMED P15 REFUEL PANEL INSTALLATION TEST AS PER B737 AMM TASK 28-21-00-400-801. TEST PASS.;[03] VERIFIED STEP 2<BR>PASSED

Part: UNKNOWN — ODOR (FWD CABIN) · airframe 38,243 hrs · 17,829 cycles

CREW REPORTS BURNING PLASTIC SMELL FROM FORWARD CABIN AREA. ALL ENGINE INDICATIONS NORMAL. RETURNED TO DAL- NORMAL LANDING<[01] ACCOMPLISHED TASK 05-51-56 AND FIM 21-00 TASK 806. NO UNUSUAL ODORS NOTED. OPS AND CKS OK.

Part: MOUNT — CRACKED (DOOR LINER) · airframe 38,133 hrs · 17,770 cycles

AFT GALLEY SERVICE DOOR LOWER LINING SUPPORT 2 EA. ISOLATOR MOUNTS DOORSIDE CRACKED.<[01] R&R AS DOOR LOWER LINING SUPPORT ISOLATOR MOUNTS PER SRM 51-40-02

Part: LIGHT — CRACKED (ZN 200 FUS TOP) · airframe 38,133 hrs · 17,770 cycles

PAX CABIN AISLE O/H CENTER EMERGENCY EXIT LIGHT ASSY CRACKED.<[01] R&R'D PAX CABIN AISLE O/H CENTER EMERGENCY EXIT LIGHT ASSY PER CMM 33-24-03

Part: LENS — LOOSE (ZN 100 FUS LOWER) · airframe 36,762 hrs · 17,006 cycles

L-1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF.<[01] INSTALLED EXIT LENS IAW AMM 33-51-01. OPS CK GOOD

Part: LAMP — INOPERATIVE (ZN 800 DOOR) · airframe 35,056 hrs · 16,061 cycles

EMERGENCY SLIDE LIGHT AFT OF L2 DOOR INOP<[01] PERFORMED LAMP REPLACEMENT FOR EMERGENCY SLIDE LIGHT AFT OF L2 DOOR IAW AMM 33-51-04

Part: BATTERY PACK — INOPERATIVE (OVERWING EXIT) · airframe 32,602 hrs · 14,759 cycles

SEVERAL EMERGENCY EXIT LIGHTS NEAR THE LH AND RH OVER-WING EXITS INOP / [01] REMOVED AND REPLACED BATTERY PACK M1695. OPS CHECK GOOD. IAW AMM 33-51-06;[02] REMOVED AND REPLACED BATTERY PACK ON M1694. OPS CHECK GOOD. IAW AMM 33-51-06;[03] REMOVED AND REPLACED BATTERY PACK ON M1671. OPS CHECK GOOD. IAW AMM 33-51-06

Part: BATTERY PACK — INOPERATIVE (R/H OVERWING) · airframe 32,602 hrs · 14,759 cycles

SEVERAL EMERGENCY EXIT LIGHTS NEAR THE LH AND RH OVER-WING EXITS INOP / [01] REMOVED AND REPLACED BATTERY PACK M1695. OPS CHECK GOOD. IAW AMM 33-51-06;[02] REMOVED AND REPLACED BATTERY PACK ON M1694. OPS CHECK GOOD. IAW AMM 33-51-06;[03] REMOVED AND REPLACED BATTERY PACK ON M1671. OPS CHECK GOOD. IAW AMM 33-51-06

Part: BATTERY PACK — INOPERATIVE (L/H OVERWING) · airframe 32,602 hrs · 14,759 cycles

SEVERAL EMERGENCY EXIT LIGHTS NEAR THE LH AND RH OVER-WING EXITS INOP / [01] REMOVED AND REPLACED BATTERY PACK M1695. OPS CHECK GOOD. IAW AMM 33-51-06;[02] REMOVED AND REPLACED BATTERY PACK ON M1694. OPS CHECK GOOD. IAW AMM 33-51-06;[03] REMOVED AND REPLACED BATTERY PACK ON M1671. OPS CHECK GOOD. IAW AMM 33-51-06

Part: PLATE — CRACKED (L/H WING) · airframe 32,602 hrs · 14,759 cycles

LOWER AFT WING SPAR TRAILING EDGE PANEL 551EB IB ATTACH WAFFLE PLATE IS CRACKED AT OB FASTENER. APPROXIMATELY IRSS 199+20. / [01] REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02;[02] INSPECTED AS REQUIRED

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 32,602 hrs · 14,759 cycles

FOOR SUPPORT ANGLE AT STA 540 FROM BL 0 TO RBL 24 AND BL 0 TO LBL24 CRACK AT FASTNER HOLE. / [01] PARTS DATA UPDATE ONLY;[02] REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER SRM 51-40-02.;[03] C/W INSPECTION

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,602 hrs · 14,759 cycles

CORNER ATTACH FITTING FOR RH WING PANEL 661AB IS CRACKED. (MARKED) / [01] REMOVED AND REPLACED FITTING PER SRM 51-40-02.;[02] VERIFIED REMOVED AND REPLACED FITTING PER SRM 51-40-02.;[03] ADJUSTMENT CK GOOD PER AMM 27-51-11;[04] SAFETIED PER AMM 27-51-11;[05] SAFETIED PER AMM 27-51-11

Part: FLASHLIGHT — DIRTY (FWD CABIN) · airframe 32,602 hrs · 14,759 cycles

FWD LAV OUTSIDE WALL 2 EACH EMERGENCY FLASH LIGHTS DIRTY. / [01] CLEANED FWD LAV OUTSIDE WALL 2 EACH EMERGENCY FLASH LIGHTS AS REQUIRED PER SOPM 20-30-03

Part: ANGLE — CRACKED (R/H WING) · airframe 32,602 hrs · 14,759 cycles

RH WING UPPER PANEL ANGLE JUST INBOARD OF DEFLECTION CONTROL RIB IS CRACKED AT OUTBOARD FASTENER HOLE. (MPN 115A2156-8) / [01] REMOVED RH WING UPPER PANEL ANGLE JUST INBOARD OF DEFLECTION RIB.;[02] LOCATED AND DRILLED UP NEW ANGLE P/N 115A2156U8 PER SRM 51-40-05.;[03] VERIFIED 2. DANIEL ANDERSON (TECHNICIAN); 26-MAY-2022 05:52 UTC<BR>LOCATED AND DRILLED UP NEW ANGLE P/N 115A2156U8 PER SRM 51-40-05.;[04] REMOVED AND INSTALLED NEW ANGLE P/N 115A2156U8 WITH FASTENERS PER SRM 51-40-02.;[05] REMOVED AND INSTALLED NEW ANGLE P/N 115A2156U8 WITH FASTENERS PER SRM 51-40-02. INSPECTION C/W

Part: BATTERY — INOPERATIVE (FWD CABIN) · airframe 31,981 hrs · 14,475 cycles

FWD. GALLEY F/A FLASHLIGHT RED LIGHT NOT BLINKING / [01] R$R FWD. GALLEY F/A FLASHLIGHT BATTERY I.A.W. A.M.M. 25-64-00

Part: LIGHT — INOPERATIVE · airframe 31,736 hrs · 14,355 cycles

LEFT OVERWING EMERGENCY EXIT LIGHTS INOP ON THE AFT OUTSIDE AND INSIDE LIGHTS ; LEFT OVERWING EMERGENCY EXIT LIGHTS INOP ON THE AFT OTSIDE AND INSIDE LIGHTS / [01] REMOVED AND REPLACED POWER SUPPLY BATTERY PACK ON CHARGER ASSY M1670. OP?S CHECKS GOOD. REF AMM 33-51-06.

Part: LIGHT — LOOSE (CABIN) · airframe 13,835 hrs · 30,601 cycles

EMERGENCY ILLUMINATION STRIP LOOSE NEAR ROW 1Z FO SIDE / REAPPLIED DBL STICK TAPE ON EMERGENCY ILLUMINATION STRIP PER SIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,694 hrs · 30,243 cycles

FWD SERVICE DOOR SLIDE LIGHT INOP / RELAMPED PER AMM 33-51-04

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,497 hrs · 12,367 cycles

SEVERAL FWD CABIN RT SIDE EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK M1676, PER AMM 33-51-06.

Part: POWER SUPPLY — INOPERATIVE (COCKPIT) · airframe 26,697 hrs · 11,892 cycles

FLIGHT DECK EMERGENCY LIGHT IS NOT WORKING / REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION TEST OF M1675 EMERGENCY EXIT LIGHT BATTERY PACK POWER SUPPLY IAW AMM 33-51-06-960-806. FLIGHT DECK EMERGENCY LIGHT CHECKS GOOD ATAG: WN0141

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 26,697 hrs · 11,892 cycles

PASSENGER CABIN FLOOR PANEL 221 EF HAS FIBERS PULLING AWAY ON UPPER SURFACE. / REPAIRED PASSENGER CABIN FLOOR PANEL 221 EF IAW SRM 53-00-50-2R-0 GENERAL REPAIR AND SRM 53-00-50-2R-1 REPAIR 1

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 26,697 hrs · 11,892 cycles

CABIN FLOOR PANEL 221GF IS PUNCTURED ON LOWER SIDE; MARKED. REPAIRED CABIN FLOOR PANEL 221GF IAW SRM 53-00-50-2R-2 AND 53-00-50-2R-0. TOOLS USED THERMOMETER AAR 30347 DUE 4/30/21 AAR 39626 DUE 3/21/21 VACUUM GOUGE AAR 5801; DUE 11/21/20 FLOOR PANEL DAMAGE EVALUATED IAW SRM 53-00-50-1A-1 ATAGTS A33993 A24484 A87131 A22696 A05073.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 26,697 hrs · 11,892 cycles

FWD CARGO COMPT FLOOR PANEL 120DF UPPER SURFACE EDGES HAVE CORROSION / EVALUATED CORROSION DAMAGE ON FWD CARGO COMPT FLOOR PANEL 120DF UPPER SURFACE EDGES-FOUND DAMAGE IS OVER THE 20' MAXIMUM ALLOWABLE DAMAGE-REPLACED WITH NEW FLOOR PANEL 120DF P/N 453A1610-20 IAW BOEING P/L 453A1610 REV T AND IPC 25-52-10-17; TO BE INSTALLED ON SA-M 565S PANEL CLOSE CARD WN0688 ATAG

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 26,697 hrs · 11,892 cycles

FWD CARGO COMPT FLOOR PANEL 120CF UPPER SURFACE EDGES HAVE CORROSION / EVALUATED CORROSIN ON FWD CARGO COMPT FLOOR PANEL 120CF UPPER SURFACE EDGES; FOUND TO BE OVER THE 20' TOTAL ACCUMULATED DAMAGE MAXIMUM- OUT OF LIMITS; IAW SRM 53-00-53-1A-1; REPLACED WITH NEW FLOOR PANEL 120CF P/N 453A1610-103 IAW BOEING P/L 453A1610-103 REV A AND IPC 25-52-10-17; TO BE INSTALLED ON SA-M 565S PANEL INSTALL CARD ATAG WN0959

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,697 hrs · 11,892 cycles

FORWARD CARGO COMPARTMENT Z-ANGLE CORROSION AT BS500A-500D+10'; RBL24; WL156 MULTIPLE LOCATIONS MARKED / REMOVED CORROSION IN FWD CARGO COMPARTMENT R/H Z-ANGLE BS 500A-500D+10' IAW SRM 51-10-02-0G-0 SECTION 15. VERIFIED LIMITS ORIGINAL THICKNESS .040' LOSS OF .008'; REMAINING .032' OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIGURE 103; DETAIL D. ACCOMPLISHED Z-ANGLE REPAIR AT BS500A - 500I IAW SRM 53-00-53-2R-5 BOEING P/N 143A7501-188

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 26,697 hrs · 11,892 cycles

CABIN FLOOR PANEL 221BF HAS FIBERS PULLING LOOSE ON UPPER SURFACE. / REPAIRED AREA OF FRAYED FIBERS ON PANEL 221BF UPPER SURFACE IAW B737-800 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,697 hrs · 11,892 cycles

AFT PASSENGER CABIN FLOOR BOARD 242E; UPPER SURFACE FACE SHEET HAS MISSING FIBERS. / REPAIRED UPPER SURFACE FACE SHEET ON FLOOR BOARD 242E IAW 737-800 SRM 53-00-50-2R-1 REPAIR 1 REV 69; SRM 53-00-50-2R-0 REPAIR GENERAL REV 69.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 26,697 hrs · 11,892 cycles

CABIN FLOOR PANEL #221CF; UPPER SIDE; LAMINANT FIBERS PULLED FROM PANEL; MARKED IN BLUE / REPAIRED CABIN FLOOR PANEL #221CF UPPER SURFACE IAW SRM 53-00-50-2R-1 REV 69 AND SRM 53-00-50-2R-0 REV 69

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,697 hrs · 11,892 cycles

AFT PASSENGER CABIN FLOOR BOARD 242UF; UPPER SURFACE FACE SHEET HAS MISSING FIBERS. / REPAIRED AFT PASSENGER CABIN FLOORBOARD 242VF UPPER FACESHEET MISSING FIBERS AS MARKED IAW B737 SRM 53-00-58-2R-1 REV 69 AND B737 SRM 53-00-50-2R-0 REV 69 A94414 A35703

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,697 hrs · 11,892 cycles

AFT PASSENGER CABIN FLOOR BOARD 241D; UPPER SURFACE FACE SHEET HAS MISSING FIBERS. / REPAIRED 2EA AREA'S OF FRAYED FIBERS ON PANEL 241D UPPER SURFACE IAW B737-800 SRM 53-00-50-2R-1 SRM 53-00-50-2R-0

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 26,697 hrs · 11,892 cycles

CABIN FLOOR PANEL 221AF IS PUNCTURED. REPAIRED FLOOR PANEL 221AF PUNCTURES IAW SRM 53-00-50-2R-2 AND SRM 53-00-50-1A-1 AND SRM 53-00-50-2R-0.

Part: DOOR SILL — CORRODED (BS 447-485) · airframe 26,697 hrs · 11,892 cycles

FORWARD CARGO COMPARTMENT DOOR SILL CORROSION AT BS4447-485; RBL30-32; WL156 LOCATIONS MARKED / REMOVED CORROSION ON FWD CARGO SILL WEB AT BS 447-485; RBL 30-32 IAW SRM 53-30-15-1A-1; ORIGINAL THICKNESS ;040'; LOSS .017' OUT OF LIMITS. REMOVED AND REPLACED SILL WEB IAW SRM 51-40-02-0G-0 AND BOEING DWG# 143A8120 REV - P/N 143A8122-10

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,697 hrs · 11,892 cycles

FORWARD CARGO COMPARTMENT Z-ANGLE CORROSION AT BS500E+10' - 500I; RBL24; WL156 MULTIPLE LOCATIONS MARKED / REMOVED CORROSION IN FWD CARGO COMPARTMENT R/H Z-ANGLE BS 500E+10' - 500I IAW SRM 51-10-02-0G-0 SCTION 15. VERIFIED LIMITS; ORIGINAL THICKNESS .040'; LOSS .008' REMAINING .032' OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIGURE 103 DETAIL D; Z-ANGLE REPAIR BS 500A-500I ACCOMPLISHED ON W/O# 40930-1400-0021 DEFECT# Y221079 BOEING P/N 143A7501-188

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 26,697 hrs · 11,892 cycles

AFT CARGO COMPT STA 794+3 - 827+17 RBL27 WL156 DOOR CUT-OUT WEB HAS CORROSION UPPER SURFACE. REMOVED CORROSION ON AFT CARGO DOOR CUTOUT LOWER THRESHOLD WEB ORIGINAL THICKNESS .045' REMOVED .030' REMAINING .015' OUT OF LIMITS IAW SRM 53-60-15-1A-1 REMOVED AND REPLACED WEB P/N 146A8123-25 IAW SRM 51-40-02-0G-0 AND DRAWINGS 146A8123 REV -; 146A8340 REV B.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,697 hrs · 11,892 cycles

AFT CARGO COMPT STA 727G - 787+14 LBL22 WL156 Z-ANGLE HAS CORROSION UPPER SURFACE / BLENDED CORROSION ON AFT CARGO L/H Z-ANGLE STA 727G-787+14 VERIFIED MATERIAL LOSS ORIG 'T' .040 REM T.030 LOSS OF .010 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED AFT CARGO L/H Z-ANGLE STA 727F+10 - 849 IAW B737-800 SRM 53-00-53-1A-2; 53-00-53-2R-5 P/N BAC 1496-377 7075-T6 ATAG A49856 TOOL# 36644 CAL DUE 29SEP20 BOEING DWG 146A7500 REV - P/N BAC1496-377 7075-T6 ATAG A49856

Part: FLOORBOARD — DAMAGED (CABIIN) · airframe 26,697 hrs · 11,892 cycles

AFT PASSENGER CABIN FLOOR BOARD 242D; UPPER SURFACE FACE SHEET HAS MISSING FIBERS. / REPAIRED AFT PASSENGER CABIN FLOORBOARD 242D UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 AND 53-00-50-2R-0 A33703 A94414

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 26,697 hrs · 11,892 cycles

CABIN FLOOR PANEL #221BF; LOWER SIDE; AREAS OF PEELING LAMINANT FIBERS; MARKED IN BLUE / REPAIRED AREA OF FRAYED FIBERS ON PANEL 221BF LOWER SURFACE IAW B737-800 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0

Part: SHIELD — CORRODED (FUSELAGE) · airframe 26,697 hrs · 11,892 cycles

FORWARD CARGO COMPARTMENT Z-ANGLE SEGMENT CORROSION AT BS492.4-500A; RBL24; WL156 MULTIPLE LOCATIONS MARKED / EVALUATED CORROSION ORIGINAL THICKNESS .032' 100% MATERIAL LOSS OUT OF LIMITS IAW SRM 53-30-15-1A-1. REMOVED AND REPLACED SHIELD STA 492.4 TO 500A P/N 143A8126Y38 IAW SRM 51-40-02-0G-0 AND BOEING DRAWING 143A0080 REV- RESTORED CORROSION INHIBITING COMPOUND IAW AMM 51-21-91-620-802 ATAG HY0525 PN143A8126Y38.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 26,697 hrs · 11,892 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140EF; TOP SURFACE; HAS CORROSION ALONG RIGHT SIDE. / EVALUATED CORROSION FOUND MORE THAN 20 INCHES OF DAMAGE OUT OF LIMITS I/A/W SRM 52-00-53-1A-1 FIGURE 102 RECIEVED NEW PANEL AND PLACED PANEL ON RACK I/A/W AIPC 25-52-10-19

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 26,697 hrs · 11,892 cycles

L/H HORIZONTAL STABILIZER SLIDING SEAL UPPER SEAL PLATE IS CRACKED. / REMOVED & REPLACED L/H HORIZONTAL STAB UPPER SLIDING SEAL IAW AMM 53-31-31-000-802+ 53-31-31-400-802

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 26,697 hrs · 11,892 cycles

CABIN FLOOR PANEL #222CF; UPPER SIDE; ATTACH SCREW INSERT MISSING / EVALUATED AND FOUND DAMAGED FIBERS AT INSERT LOCATION ON FLOOR BOARD 222CF. PEFORMED DAMAGED FIBERS AND INSTALLED NEW INSERTS IAW B737-800 SRM 53-0-50-2R-1 REPAIR 1 REV 69; SRM 53-00-50-2R-0 REPAIR GENERAL REV 69 AND (A94414)(A03261)(A29079)(A67412)(A74475)

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 26,697 hrs · 11,892 cycles

CABIN FLOOR PANEL 222AF HAS FIBERS PULLING LOOSE ON UPPER SURFACE. / REPAIRED PASSENGER CABIN FLOOR PANEL 222AF IAW SRM 53-00-50-2R-0 GENERAL REPAIR AND SRM 53-00-50-2R-1 REPAIR 1

Part: SHIELD — CORRODED (BS 767-794) · airframe 26,697 hrs · 11,892 cycles

AFT CARGO COMPT STA 767 - 794 RBL22 WL156 SHIELD HAS CORROSION UPPER AND LOWER SURFACE / REMOVED CORROSION ON AFT CARGO FLOOR SUPPORT SHIELD AT STA 767-794 RBL 22 WL156 IAW SRM 51-10-02. VERIFIED OUT OF ALLOWABLE LIMITS AS ORIGINAL =.050' WITH REMAINING THICKNESS AS .042' IAW SRM 53-60-15-1A-1 REMOVED DAMAGED SHIELD IAW SRM 51-40-02. VERIFIED PART EFFECTIVITY FOR P/N 146A8127-12 ON TAG# WN9192 IAW SRM 53-00-15-01-1 AND BOEING DRW #146A0081 SHT 46 REV -. INSTALLED SHIELD IAW SRM 51-40-02 AND DRW # 146A0081 SHT 46 REV -.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 26,697 hrs · 11,892 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140DF; TOP SURFACE; HAS CORROSION AT ATTACHMENT HOLES AND EDGE. / EVALUATED CORROSION FOUND MORE THAN 20 INCHES OF DAMAGE OUT OF LIMITS I/A/W SRM 52-00-53-1A-1 FIGURE 102 RECIEVED NEW PANEL AND PLACED PANEL ON SHELF I/A/W AIPC 25-52-10-19

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,697 hrs · 11,892 cycles

AFT PASSENGER CABIN FLOOR BOARD 241AAF; UPPER SURFACE FACE SHEET HAS MISSING FIBERS. / REPAIRED AREAS ON FRAYED FIBERS ON PANEL 241AAF UPPER SURFACE IOAW B737-800 SRM 53-00-50-2R-1 SRM 53-00-50-50-2R-0

Part: BAFFLE — CRACKED (BS 727A-727B) · airframe 26,697 hrs · 11,892 cycles

AFT CARGO COMPT STA 727A - 727B RBL22 BAFFLE IS CRACKED / REMOVED AND REPLACED CRACKED BAFFLE AT BS727A-727B; RBL22IN AFT CARGO COMPARTMENT IAW SRM 51-40-02-0G-0 AND BOEING DWG #5 146A7505 ID: 0001 REV A AND 146A7500 ID: 0213 REV-

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,697 hrs · 11,892 cycles

AFT PASSENGER CABIN FLOOR BOARD 241ABF; UPPER SURFACE FACE SHEET HAS MISSING FIBERS. / REAPAIRED AFT PASSENGER CABIN FLOOR BOARD 241ABF UPPER FACE SHEET AT I/B FWD EDGE IAW B737 SRM 53-00-50-2R-1 REV 69 AND SRM 53-00-50-2R-0 REV 69 A94414 A33703

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,697 hrs · 11,892 cycles

AFT PASSENGER CABIN FLOOR BOARD 241E; UPPER SURFACE FACE SHEET HAS MISSING FIBERS. / REPAIRED UPPER SURFACE FACE SHEET ON FLOOR BOARD 241E IAW 737-800 SRM 53-00-50-2R-1 REPAIR 1 REV 69 SRM 53-00-50-2R-0 REPAIR GENERAL REV 69

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 26,697 hrs · 11,892 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140CF; TOP SURFACE; HAS CORROSION AT FORWARD AND AFT THRESHOLD CUTOUT AREAS. / EVALUATED CORROSION FOUND MORE THAN 20 INCHES OF DAMAGE OUT OF LIMITS I/A/W SRM 52-00-53-1A-1 FIGURE 102 RECIEVED NEW PANEL AND PLACED PANEL ON SHELF I/A/W AIPC 25-52-10-19

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,697 hrs · 11,892 cycles

AFT PASSENGER CABIN FLOOR BOARD 241XF; UPPER SURFACE FACE SHEET HAS MISSING FIBERS. / REPAIRED DAMAGE TO UPPER SURFACE FACE SHEET ON FLOOR BOARD 241XF IAW 737-800 SRM 53-00-50-2R-1 REPAIR 1 REV 69 AND SRM 53-00-50-2R-0 REPAIR GENERAL REV 69 (A94414)(A94774)

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 26,697 hrs · 11,892 cycles

R/H HORIZONTAL STABILIZER SLIDING SEAL UPPER SEAL PLATE IS CRACKED. / REMOVED + REPLACED R/H HORIZONTAL STAB UPPER SLIDING SEAL IAW AMM 53-31-31-000-802; + 53-31-31-400-802

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 26,697 hrs · 11,892 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140BF; TOP SURFACE; HAS CORROSION ALONG EDGES. / EVALUATED CORROSION FOUND MORE THAN 20 INCHES OF DAMAGE OUT OF LIMITS I/A/W SRM 52-00-53-1A-1 FIGURE 102 RECIEVED NEW PANEL AND PLACED PANEL ON SHELF I/A/W AIPC 25-52-10-19

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,697 hrs · 11,892 cycles

FORWARD CARGO COMPARTMENT Z-ANGLE CORROSION AT BS500A-500G; LBL24; WL156 MULTIPLE LOCATIONS MARKED / REMOVED CORROSION IN FWD CARGO COMPARTMENT L/H Z-ANGLE BS 500A-500G IAW SRM 51-10-02-0G-0 SECTION 15. VERIFIED LIMITS ORIGINAL THICKNESS .040'; LOSS OF .006'; REMAINING .034' OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIGURE 103; DETAIL D. ACCOMPLISHED Z-ANGLE REPAIR AT BS 500F-500I IAW SRM 53-00-53-2R-5 BOEING P/N 143A7501-188

Part: ANCHOR FITTING — CORRODED (AFT CARGO) · airframe 26,697 hrs · 11,892 cycles

AFT PIT; FWD AFT TIE DOWN ANCHOR PLATE; HAS CORROSION. / RECIEVED NEW TIE DOWN ANCHOR PLATE MPN 453A2611-1 ISSUE TAG E02051 AND PLACED ITEM ON SHELF IAW AIPC 25-52-10-04

Part: STRIP — CORRODED (FWD CARGO) · airframe 26,697 hrs · 11,892 cycles

FWD CARGO COMPT R/H AFT FLOOR TO SIDEWALL CAP STRIP HAS CORROSION / FWD CARGO COMPT RH AFT FLOOR TO SIDEWALL CAP STRIP REPLACED DUE TO NO ALLOWABLE LIMITS WITH PN 453A1611-17 TAG# HY0516 IAW AIPC 25-52-10-03 AND BOEING DWG #453A1600 ID 20 REV -

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 26,697 hrs · 11,892 cycles

FWD PIT AFT CORNER SCUFF PLATE CRACKED / FWD CARGO; AFT CORNER SCUFF PLATE REPAIRED ON BACK SHOP WORK ORDER 40932-1000-0001 IAW SRM 53-30-15-2R. SCUFF PLATE WILL BE INSTALLED ON W/O 40931-1400-0008

Part: STRIP — CORRODED (FWD CARGO) · airframe 26,697 hrs · 11,892 cycles

FWD CARGO COMPT R/H MIDDLE FLOOR TO SIDEWALL CAP STRIP HAS CORROSION / REMOVED CORROSION; NO PUBLISHED LIMITS FOR FWD CARGO COMPT R/H MIDDLE FLOOR TO SIDEWALL CAP STRIP; REPLACED WITH NEW CAPSTRIP P/N 453A1611-31 IAW IPC 25-52-10-03; TO BE INSTALLED ON SA-M 565S PANEL CARD WHEN PANEL 122EW AND 120CF ARE INSTALLED ATAG WN1585

Part: COVER — CRACKED (CABIN) · airframe 26,697 hrs · 11,892 cycles

PASSENGER COMPARTMENT SIDEWALL 231ZKW EXIT LIGHT COVER CRACKED. / REPLACED PASSENGER COMPARTMENT SIDEWALL 2312KW EXIT LIGHT COVER IAW B737-800 AMM 33-51-01-960-801. WN9219.

Part: BATTERY — FAILED (CABIN) · airframe 26,554 hrs · 11,818 cycles

FWD LEFT EMERGENCY BATTERY FAILED CAPASITY TEST. / R AND R FWD LEFT EMERGENCY BATTERY; TEST GOOD PER AMM 33-51-06 INSP P50

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 26,554 hrs · 11,818 cycles

RT STAB; UPPER FWD SPAR SLIDING SEAL CRACKED / R&R R/H HORIZONTAL STAB; UPPER FWD SLIDING SEAL REF AMM 53-31-31INSP 38977

Part: SEAT TRACK — WORN (COCKPIT) · airframe 26,554 hrs · 11,818 cycles

FIRST OFFICER I/B SEAT TRACK WORN / R AND R FIRST OFFICER I/B SEAT TRACK PER AMM 25-11-11 INSP 22640

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 26,554 hrs · 11,818 cycles

EXTERNAL GROUND POWER RECEPTACLE SURROUND DOUBLER CRACKED .350 IN LOWER ZONE 2 AREA / REPAIRED PER SRM 53-10-15-2R-4 INSP P44

Part: SEAT TRACK — WORN (COCKPIT) · airframe 26,554 hrs · 11,818 cycles

CAPTAIN I/B SEAT TRACK WORN / R AND R CAPTAIN I/B SEAT TRACK PER AMM 25-11-11 INSP 22640

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,880 hrs · 10,966 cycles

EMERGENCY LIGHTS ARE OUT AT LEFT AFT INTERIOR & EXTERIOR. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK FOR LEFT AFT INTERIOR AND EXTERIOR IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,632 hrs · 10,850 cycles

R/H AFT SECTION EMERGENCY LIGHTS INOP. R&R BATTERY PACK IAW AMM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,521 hrs · 10,810 cycles

AFT L/H ENTRY DOOR EMERGENCY LIGHT INOP. R & R THE BATTERY PACK CHARGER ASSEMBLY IAW AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 24,163 hrs · 10,608 cycles

AFT RIGHT EMERGENCY FLASHLIGHT STRAP BROKEN. R&R STRAP PER AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 24,117 hrs · 10,588 cycles

R/H EXIT ROW LIGHT COVER MISSING AT ROW 14. INSTALLED LENS PER SIP.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 23,228 hrs · 10,160 cycles

L/H PASSENGER CABIN EMERGENCY LIGHT LENS BROKEN AT ROW 15. R&R LENS PER MM.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 23,544 hrs · 10,292 cycles

RT HOVIZ STAB UPPER FWD SLIDING SEAL CRACKED / REMOVED AND REPLACED RT HORIZONTAL STAB UPPER FWD SLIDING SEAL PER AMM 53-31-31 INSP 43511

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 23,544 hrs · 10,292 cycles

LT HARIZ STAB UPPER FWD SLIDING SEAL CRACKED / R&R LT HARIZ STAB UPPER FWD SLIDING SEAL IAW AMM 53-31-31 INSP 43511

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 22,291 hrs · 9,733 cycles

R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,211 hrs · 9,699 cycles

L2 DOOR EXTERNAL SLIDE LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: PRESSURE SWITCH — FAILED (NR 1 ENGINE) · airframe 22,180 hrs · 9,684 cycles

DIVERSION, NR 1 ENGINE COWL ANTI ICE VALVE FAILED IN FLIGHT. R&R NR 1 ENGINE ANTI-ICE PRESSURE SWITCH PER MM.

Part: LENS — MISSING (CABIN) · airframe 21,649 hrs · 9,432 cycles

CENTER AISLE OVERWING EXIT SIGN MISSING LENS. R&R LENS PER SIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,012 hrs · 8,706 cycles

R1 DOOR EMERGENCY LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,012 hrs · 8,706 cycles

R1 SLIDE LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: BRACKET — BROKEN (LEFT WING) · airframe 20,798 hrs · 9,064 cycles

LEFT WING TRAILING EDGE PANEL 551FB HAS A BROKEN BRACKET ON FWD SIDE / REMOVED & REPLACED LEFT WING TRAILING EDGE PANEL 551FB BRACKET IAW SRM 51-40-02-0G-0

Part: SKIN — DAMAGED (AFT FUSELAGE) · airframe 20,798 hrs · 9,064 cycles

FOUND DAMAGE TO SKIN BS 747+1.5 AND 1.75' ABOVE STR 22R / REPAIRED DAMAGED SKIN AT STA. 747+1.5 AND 1.75' ABOVE STR. 22R IAW ATS ER 18-02801 REV. IR AND SOUTHWEST EA REPAIR 53EA-05228 REV. 1

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 20,798 hrs · 9,064 cycles

SUPPLEMENTAL INFORMATION: L/H SIDE VAPOR BARRIER AT 663.75 HAS A CRACK BETWEEN LBL 0.19 AND 15.45 / REPAIRED L/H SIDE VAPOR BARRIER AT 663.75 IAW W/O OTHER-57EA-03738; SRM 57-10-10-1A-2 CH 1C AND SRM 57-10-10-2R-2 CH1 WITH SRM 51-70-04-2R-10

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 20,012 hrs · 8,706 cycles

PRESSURE BULKHEAD WEB CRACKED AT BS 663.75. REPAIRED THE BULKHEAD SRM AND EA.

Part: NONE — CRACKED (FWD CARGO BAY) · airframe 20,798 hrs · 9,064 cycles

SUPPLEMENTAL INFORMATION: FORWARD CARGO. FRAME SUPPORT GUSSET CRACKED AT BS 500I SRT21L / AFTER EVALUATION OF GUSSET FOUND NO ALLOWABLE LIMITS AND IN REPAIRABLE BY REPLACEMENT. IAW SRM 51-10-02-0G-0. FABRICATED GUSSET FROM 7025-0 .040' LOT #5013125 IAW BOEING DWG 1439483; HEAT TREATED PART TO T6 IAW DWG 143A9483 AND BAC 5602. LOCATED; DRILLED; DEBURRED; AND INSTALLED FABRICATED GUSSET TO THE FWD CARGO STR 21L STA 500I. IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7402. 57575U 05/10/18

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 20,012 hrs · 8,706 cycles

LT VAPOR BARRIER CRACKED AT BS 663.75, BETWEEN LBL 0.19 TO LBL 15.45. REPAIRED BARRIER IAW SRM.

Part: GUSSET — CRACKED (BS 500I) · airframe 20,012 hrs · 8,706 cycles

FORWARD CARGO FRAME SUPPORT GUSSET CRACKED AT BS 500I, STRINGER 21L. R & R THE GUSSET IAW SRM & DWG.

Part: NONE — CRACKED (AFT CARGO BAY) · airframe 20,798 hrs · 9,064 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO FWD BULKHEAD PANEL 142NW LOWER CAP STRIP CRACKED / RECEIVED NEW AFT CARGO BULKHEAD PANEL 152NW LWR CAP STRIP SI #7253171; PO #687608. STEP TO BE INSTALLED ON SA-M 55S 57305U 5/12/18

Part: WEB — CRACKED (LT WING) · airframe 20,798 hrs · 9,064 cycles

SUPPLEMENTAL INFORMATION: CRACKED WEB INBOARD OF LH WING AFT FLAP DEFLECTION ARM. MARKED WITH TAPE. APPROXIMA TE WS 281. / REMOVED CRACKED WEB; INBOARD OF L/H WING AFT. FLAP DEFLECTION ARM I.A.W. S.R.M. 51-40-02-0G-0. LOCATED AND DRILLED HOLES ON NEW WEB. PART #115A2156Y. AND SRM 51-40-05-0G-0; DRAWING #115A2156. INSTALLED WEB; I.A.W. S.R.M. 51-40-02-0G-0 AND DRAWING #115A2156.

Part: SIDEWALL SUPPORT — CORRODED (BS 727-767) · airframe 20,012 hrs · 8,706 cycles

AFT CARGO BAY, RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO 767. R&R THE SIDEWALL SUPPORT IAW DWG & SRM.

Part: GUSSET — CRACKED (BS 500I) · airframe 20,012 hrs · 8,706 cycles

FORWARD CARGO FRAME SUPPORT GUSSET CRACKED AT BS 500I, STRINGER 19R. R & R THE GUSSET IAW SRM AND DWG.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 20,798 hrs · 9,064 cycles

***CORROSION*** AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT HAS CORROSION STA. 727 TO STA. 767 / SIDEWALL SUPPORT AT 727 STA TO 767 STA FOUND TO BE OUT OF LIMITS PER SRM-53-00-53-1A-2. REMOVED AND REPLACED SIDEWALL SUPPORT REPLACEMENT PER DWG. 146A7500; SRM 53-00-53-2R-5; SRM 51-40-02-0G-0

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 20,798 hrs · 9,064 cycles

FORWARD CARGO. FRAME SUPPORT GUSSET CRACKED AT BS 500I SRT19R / REMOVED FWD CARGO GUSSET AT BS 500I SRT 19R PARE #143A9481-5 IAW SRM 51-40-02-0G-0 AND INSTALLED NEW GUSSET PART #143A9481-5 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7902 REV.A.

Part: CAP SEAL — CORRODED (AFT CARGO BAY) · airframe 20,798 hrs · 9,064 cycles

***CORROSION*** AFT CARGO COMPARTMENT L/H FLOOR TO SIDEWALL SUPPORT HAS CORROSION STA. 727 TO STA. 847 / SIDEWALL SUPPORT STA 727 TO 847 STA FOUND TO BE OUT LIMITS PER SRM 53-00-53-1A-2; REMOVED AND REPLACED SIDEWALL SUPPORT REPLACEMENT PER DWG. 146A7500; SRM 53-00-53-2R-5; SRM-51-40-02-0G-0. SPLICE LOCATIONS AT BS 77F +10 AND BS 794 L/H SIDE.

Part: SHIELD — CORRODED (BS 774) · airframe 20,012 hrs · 8,706 cycles

AFT CARGO FLOOR TO SIDEWALL SHIELD CORRODED AT BS 774. R & R THE SHIELD IAW SRM & DWG.

Part: CAP SEAL — CORRODED (AFT CARGO BAY) · airframe 20,798 hrs · 9,064 cycles

***CORROSION*** ON AFT CARGO FLOOR TO SIDEWALL SHIELD BS 774 R/H / REMOVED CORROSION ON AFT CARGO FLOOR TO SIDEWALL SHIELD @ BS. 774 R/H; IAW SRM 51-10-02-0G-0; AREA L=1.0 X W= 1.0 D= .020 OUT OF LIMITS IAW SRM 53-00-53-1A-1; REMOVED SHIELD IAW SRM 51-40-02-0G-0. LOCATED & DRILLED NEW SHIELD P//N 7531132 PO #679929 IAW SRM 51-40-05-0G-0 & DWG 146A0081. INSTALLED SHIELD IAW SRM 51-40-02-0G-0 & DWG 146A0081

Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 20,798 hrs · 9,064 cycles

***CORROSION*** R/H Z CHANNEL FROM STATION 500A TO 500D HAS MULTIPLE AREAS OF CORROSION AROUND FASTENER HOLES / CORROSION AROUND FASTENER HOLES ON RH Z CHANNEL STATION 500A TO 500D FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 FIG 103 DETIAL D. REMOVED Z CHANNEL FROM STATION 500A TO 500D+10' AND LOCATED REPAIR SPLICE AT STA 500D+10'. FABRICATED AND INSTALLED REPLACEMENT Z CHANNEL AND SPLICE IAW B737-800 SRM 53-00-53-2R-5 AND SRM 51-40-02-0G-0 AND DWG #143A7500 SHEET 75

Part: CHANNEL — CORRODED (BS 500I) · airframe 20,012 hrs · 8,706 cycles

FORWARD CARGO LOWER BULKHEAD SUPPORT CHANNEL CORRODED AT BS 500I, BETWEEN RBL 24 TO LBL 24. R & R THE CHANNEL IAW SRM AND DWG.

Part: FAIRING — CRACKED (LWR FUSELAGE) · airframe 20,798 hrs · 9,064 cycles

PANEL 194BR CRACKED / REPAIRED CRACKED PANEL 194BR I.A.W 737 SRM 53-60-70-2R-1 PARA 1; 4D TABLE 203 250 DEG CURE; PER 737 SRM 51-70-05 REPAIR 10

Part: SUPPORT CHANNEL — CORRODED (FWD CARGO BAY) · airframe 20,798 hrs · 9,064 cycles

***CORROSION*** ON FWD CARGO LOWER BULKHEAD SUPPORT CHANNEL BS 500I RBL 24 TO LBL 24 / REMOVED CORROSION FROM FWD CARGO LOWER BULKHEAD SUPPORT CHANNEL BS 500I RBO 24 I.A.W. SRM 51-10-02-0G-0 DAMAGE MEASURES L=4.0' X W=1.5'XD=.090' FOUND TO BE OUT OF LIMITS IAW SRM 53-30-30-1A-1 FIG 103 SHT 3G LOCATED AND DRILLED NEW CHANNEL P/N 7530142 P.O. #675637 IAW SRM 51-40-05-0G-0 INSTALLED NEW CHANNEL IAW SRM 51-40-02-0G-0 AND DRAWING #143A9481 80644U 05/08/18

Part: FAIRING — CRACKED (LWR FUSELAGE) · airframe 20,798 hrs · 9,064 cycles

PANEL 194CR CRACKED/DELAMINATED 3 EACH AREAS. (MARKED) / REPAIRED 3EA CRACK/DELAMINATION AREAS ON PANEL 194CR PER SRM 53-60-70-2R-1 TABLE 201 AND SRM 51-70-05-2R-2

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 20,012 hrs · 8,706 cycles

RT Z CHANNEL CORRODED BETWEEN BS 500A TO BS 500D. R&R Z CHANNEL IAW SRM AND DWG.

Part: PANEL — DELAMINATED (RT WING) · airframe 20,798 hrs · 9,064 cycles

R/H WING L/E PANEL 621JB HAS FWD CORNER DELAMINATION (MARKED) / REPAIRED DELAMINATION ON FWD CORNER OF R/H WING L/E PANEL 621JB IAW SRM 57-41-01-2R-1; TABLE 202& SRM 51-70-05-2R-6 80733U 20MAY18

Part: WEB — CRACKED (TE FLAP) · airframe 20,012 hrs · 8,706 cycles

LT WING AFT FLAP INBOARD WEB CRACKED. R&R WEB IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,012 hrs · 8,706 cycles

AFT CARGO COMPARTMENT LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847. R&R SUPPORT PER DWG & SRM.

Part: PANEL — CRACKED (RIGHT WING) · airframe 20,652 hrs · 8,997 cycles

RIGHT WING DEFLECTION CONTROL RIB INBOARD CLOSURE PANEL CRACKED / REMOVED AND REPLACED PANEL REF SRM 51-40-02 (INSPECTOR 71231)

Part: VAPOR BARRIER — CRACKED (RT WHEEL WELL)

RT SIDE VAPOR BARRIER HAS A 6' CRACK FWD OF B SYS HYD FILTER. STOP DRILLED CRACK IN ZONE 1 LAMINATE AND SEALED WITH SPEED TAPE PER 57-10-10-1A-2 PAR 2C(4) REINSPECT EVERY 1200 FLT CYCLES NO PERMINANT REPAIR LIMIT GIVEN. MAKE SURE THAT CRACK HAS NOT GROWN PAST INTERIM SEAL (SPEED TAPE)REPETITIVE ACTION REQUIRED / C) REPETITIVE ACTION REQUIRED COMPLIED WITH. ADDITIONAL DAMAGE OR DETERIORATION WAS FOUND. CONDITION HAS BEEN CORRECTED AS NOTED ON N141337

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 18,658 hrs · 8,059 cycles

FORWARD CABIN RT PHOTOLUMINESCENT LIGHTING BROKEN AT ROW 1. R&R STRIP PER AMM.

Part: BRACKET — SHEARED (R1 DOOR) · airframe 18,932 hrs · 8,198 cycles

R1 DOOR EMERGENCY EVAC SLIDE CONTAINER AFT BRACKET SHEARED. R&R BRACKET ASSEMBLY PER SRM & MT.

Part: LENS — LOOSE (CABIN) · airframe 16,590 hrs · 7,146 cycles

L1 DOOR EMERGENCY LIGHT LENS COVER LOOSE. SECURED LENS ASSEMBLY PER SIP.

Part: LENS — CRACKED (CABIN) · airframe 13,840 hrs · 5,910 cycles

LEFT EMERGENCY EXIT LIGHT LENS CRACKED BETWEEN ROW 8 TO ROW 23. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 13,840 hrs · 5,910 cycles

RIGHT EMERGENCY EXIT LIGHT LENS CRACKED BETWEEN ROW 10 TO ROW 27. R & R LENS IAW AMM.

Part: LIGHT — FAULTY (CABIN) · airframe 12,724 hrs · 5,426 cycles

LEFT EMER EXIT CEILING LIGHT AT FAULTY. REPAIRED LIGHT IAW MM.