N8602F

Part: FLAP SYSTEM — LOCKED · airframe 45,446 hrs · 21,483 cycles

FLAP GAUGE DID NOT MATCH COMMANDED POSITION. FLAPS WOULD NOT RETRACT PAST FLAPS 2. PERFORMED FSEU BITE PER FIM 27-51 TASK 801; NO FAULTS NOTED. PERFORMED TRAILING EDGE FLAP SYSTEM OPS TEST PER AMM 27-51-00. ALL OPS NORMAL. A/C OK FOR SERVICE.

Part: COVER — MISSING (ZONE 200) · airframe 44,447 hrs · 20,963 cycles

MID CABIN OVERHEAD EXIT SIGN MISSING COVER. REPLACED EMERGENCY EXIT SIGN IAW AMM 33-51-01.

Part: HANDLE — LOOSE (ZONE 800) · airframe 44,241 hrs · 20,859 cycles

R2 DOOR ASSIST HANDLE IS LOOSE. SECURED R2 DOOR ASSIST HANDLE IAW AMM 52-13-31. SECURED R2 DOOR ASSIST HANDLE IAW AMM 52-13-31

Part: HANDLE — LOOSE (ZONE 800) · airframe 44,241 hrs · 20,859 cycles

R1 DOOR ASSIST HANDLE ON G1 IS LOOSE. SECURED R1 DOOR ASSIST HANDLE IAW B737-800 AMM 52-41-31.

Part: HANDLE — LOOSE (ZONE 800) · airframe 44,241 hrs · 20,859 cycles

L1 DOOR ASSIST HANDLE VERY LOOSE<[01] SECURED L1 DOOR ASSIST HANDLE IAW B737-800 AMM 52-11-31;[02] SECURED L1 DOOR ASSIST HANDLE IAW B737-800 AMM 52-11-31.

Part: COVER — MISSING (ZONE 200) · airframe 42,072 hrs · 19,718 cycles

MID CABIN EMERGENCY EXIT SIGN COVER MISSING<[01] INSTALLED NEW COVER PER SIP

Part: ANGLE — CRACKED (ZONE 500) · airframe 41,579 hrs · 19,446 cycles

SIGNIFICANT DAMAGE TO PRIMARY STRUCTURE KRAS 150 (PN 116A4005) AND KRAS 166 (PN 116A4004). CRACK FOUND IN BULB SEAL Z ANGLE (NOSE BEAM PN 116A4610) AT THE BOTTOM OF THE LEADING EDGE. SEE ATTACHED PHOTOS OF DAMAGE<[01] ACCOMPLISHED EA 24-157-02319.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 41,576 hrs · 19,444 cycles

L/H EXTERIOR FWD OVERWING EMERGENCY LIGHT INOP<[01] RE-LAMPED L/H EXTERIOR FWD OVERWING EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.

Part: COVER — DETACHED (ZONE 200) · airframe 41,472 hrs · 19,386 cycles

EMERGENCY EXIT SIGN IN CEILING MID CABIN FELL OFF<[01] RESECURED EMER. EXIT SIGN COVER IAW AMM 33-51-03

Part: SIGN — DETACHED (ZN 200 FUS TOP) · airframe 40,595 hrs · 18,907 cycles

FWD ENTRY DOOR EXIT SIGN COVER DETACHED.<[01] REPLACED FWD ENTRY DOOR EXIT SIGN PER SIP.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 40,545 hrs · 18,882 cycles

BOTH OVERWING EXIT LIGHT COVERS CAME OFF DURING LANDING<[01] REINSTALLED BOTH OVERWING EXIT LIGHT COVER REF AMM 33-51-01. OPS CHK GOOD

Part: SIGN — BROKEN (AFT CABIN) · airframe 40,275 hrs · 18,725 cycles

AFT GALLEY EMERGENCY EXIT SIGN BROKEN<[01] REPLACED EXIT SIGN PER SIP

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,957 hrs · 18,565 cycles

SEVERAL EXTERIOR AND INTERIOR EMERGENCY LIGHTS INOPERATIVE.<[01] REPLACED EMERGENCY LIGHTS BATTERY PACKS I/A/W SWA AMM 33-51-06-960-805. OPERATIONAL TEST PASSED. <BR><BR>BATTERY; BATTERY PACK M1670 - P/N: AD-D717-01-100SWA. B/N: 454354<BR>BATTERY; BATTERY PACK M1694 - P/N: AD-D717-01-100SWA. B/N: 454842<BR>BATTERY; BATTERY PACK M1695 - P/N: AD-D717-01-100SWA. B/N: 447576;[02] PERFORMED TROUBLESHOOTING. FOUND 4 BATTERY PACKS DEFECTIVE. POSITIONS M1670; M1694; M1695; M1675<BR><BR>REPLACED EMERGENCY LIGHTS BATTERY PACKS AS PER AMM REF 33-51-06-960-805 AND WDM 33-51-13 AND WDM 33-51-14. (REPLACEMENT OF BATTERY PACK AT POSITION M1675 NOT REQUIRED) ALL LIGHTS ARE FUNCTIONING; INSTALLATION TEST PASSED.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 39,957 hrs · 18,565 cycles

CABIN FLOOR BOARD 231KF CRACKED<[01] REMOVED DAMAGE FLOOR PANEL; FABRICATED PANEL; AND INSTALLED FLOOR PANEL 231KF REF DWG 143A5810-522 AND AMM 53-21-00-400-801;[02] VERIFIED STEP 1

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

CAPTAIN FWD OB SEAT TRACK WITH SURFACE CORROSION AREAS.<[01] CAPTAIN FWD O/B SEAT TRACK WAS REPLACED ON TASKCARD TTG8Q00R8ZVB;[02] VERIFIED STEP 1.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

CAPTAIN AFT IB SEAT TRACK WITH SURFACE CORROSION AREAS.<[01] CAPTAIN AFT I/B SEAT TRACK WAS REPLACED ON TASKCARD TTG8Q00R90DL.;[02] VERIFIED STEP 1.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

FIRST OFFICER AFT IB SEAT TRACK WITH SURFACE CORROSION AREAS<[01] FIRST OFFICER AFT I/B SEAT TRACK WAS REPLACED ON TTG8Q00R8ZSQ.;[02] VERIFIED STEP 1.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

FIRST OFFICER FWD IB SEAT TRACK WITH SURFACE CORROSION AREAS.<[01] FIRST OFFICER FWD I/B SEAT TRACK WAS REPLACED ON TASKCARD TTG8Q00R90CA.;[02] VERIFIED STEP 1.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

FIRST OFFICER AFT OB SEAT TRACK WITH SURFACE CORROSION AREAS.<[01] FIRST OFFICER AFT O/B SEAT TRACK WAS REPLACED ON TASKCARD TTG8Q00R90CV.;[02] VERIFIED STEP 1.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

FIRST OFFICER FWD OB SEAT TRACK WITH SURFACE CORROSION AREAS.<[01] FIRST OFFICER FWD O/B SEAT TRACK WAS REPLACED ON TASKCARD TTG8Q00R8ZSX.;[02] VERIFIED STEP 1.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

CAPTAIN AFT OB SEAT TRACK WITH SURFACE CORROSION AREAS.<[01] CAPTAIN AFT O/B SEAT TRACK WAS REPLACED ON TASKCARD TTG8Q00R90CL.;[02] VERIFIED STEP 1.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

CAPTAIN FWD IB SEAT TRACK WITH SURFACE CORROSION AREAS.<[01] CAPTAIN FWD I/B SEAT TRACK WAS REPLACED ON TASKCARD TTG8Q00R90D6.;[02] VERIFIED STEP 1.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 39,957 hrs · 18,565 cycles

FLOOR PANEL 241AF UPPER SKIN DELAMINATED AT CENTER.<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA AS MARKED ON PANEL # 241AF AS PER B737 SRM 53-00-50-2R-1 PARAG 3-K-M; MATERIAL USED PO#2040692; PO#1690463.;[02] VERIFIED STEP 1

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

CAPTAIN AFT IB SEAT TRACK WITH SURFACE CORROSION AND GOUGED AREAS.<[01] NEW FAULT TTG8Q00R8ZVG / TTG8Q00R90DL

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

FIRST OFFICER FWD IB AND OB SEAT TRACK WITH SURFACE CORROSION.<[01] SEE NEW FAULTS TTG8Q00R7NEO / TTG8Q00R7NE9.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

FIRST OFFICER AFT OB SEAT TRACK WITH SURFACE CORROSION AND GOUGED AREAS.<[01] NEW FAULT TTG8Q00R8ZTV / TTG8Q00R90CV

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

CAPTAIN FWD OB SEAT TRACK WITH SURFACE CORROSION AND GOUGED AREAS.<[01] NEW FAULTS TTG8Q00R90DG / TTG8Q00R8ZVB

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

CAPTAIN AFT OB SEAT TRACK WITH SURFACE CORROSION AND GOUGED AREAS.<[01] NEW FAULT TTG8Q00R90CG / TTG8Q00R90CL

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

FIRST OFFICER AFT IB AND OB SEAT TRACK WITH SURFACE CORROSION AREAS.<[01] NEW FAULTS TTG8Q00R7NED / TTG8Q00R7P6D.

Part: SEAT TRACK — CORRODED (ZN 200 FUS TOP) · airframe 39,957 hrs · 18,565 cycles

FIRST OFFICER FWD IB SEAT TRACK WITH SURFACE CORROSION AND GOUGED AREAS.<[01] NEW FAULT TTG8Q00R90C9 / TTG8Q00R90CA

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

FIRST OFFICER AFT IB SEAT TRACK WITH SURFACE CORROSION AND GOUGED AREAS.<[01] NEW FAULT TTG8Q00R8ZSN / TTG8Q00R8ZSQ

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

CAPTAIN FWD IB SEAT TRACK WITH SURFACE CORROSION AND GOUGED AREAS.<[01] NEW FAULTS TTG8Q00R90D0 / TTG8Q00R90D6.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 39,957 hrs · 18,565 cycles

FIRST OFFICER FWD OB SEAT TRACK WITH SURFACE CORROSION AND GOUGED AREAS.<[01] NEW FAULT TTG8Q00R8ZSW / TTG8Q00R8ZSX

Part: PANEL — DAMAGED (RT WING) · airframe 39,957 hrs · 18,565 cycles

R/W T/E REAR SPAR LOWER PANEL 651GB INB SUPPORT RODS UPPER SUPPORT FITTING EXCESSIVE PLAY AND ELONGATATED HOLES MKD DOT<[01] REMOVED AND REPLACED SUPPORT FITTING AT R/W T/E REAR SPAR LOWER PANEL 651GB REF. SRM 51-40-02-0G-0;[02] VERIFIED STEP 1

Part: SUPPORT ANGLE — CRACKED (BS 500G S26L) · airframe 39,957 hrs · 18,565 cycles

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

Part: ACCESS PANEL — CRACKED (HINGE BOX) · airframe 39,957 hrs · 18,565 cycles

AFT GALLEY SERVICE DOOR R-2 LOWER HINGE ACCESS PANEL 844DZ CRACKED<[01] AFT GALLEY SERVICE DOOR R-2 LOWER HINGE ACCESS PANEL 844DZ WAS REPLACED ON TASKCARD TTG8Q00R215M.;[02] VERIFIED STEP 1.

Part: SUPPORT ANGLE — CRACKED (BS 500H S26R) · airframe 39,957 hrs · 18,565 cycles

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

Part: SUPPORT FRAME — CRACKED (NR 2 NACELLE) · airframe 39,957 hrs · 18,565 cycles

#2 ENGINE PNL#423 I/B FAN COWL SUPPORT FRAME NEXT TO OIL SERVICES DOOR IS CRACK<[01] REMOVED AND REPLACED #2 ENGINE PNL#423 I/B FAN COWL SUPPORT FRAME NEXT TO OIL SERVICES DOOR AS-PER SRM 51-40-02-0G-0;[02] VERIFIED STEP 1

Part: SUPPORT ANGLE — CRACKED (BS 500H S26L) · airframe 39,957 hrs · 18,565 cycles

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

Part: SUPPORT FRAME — CRACKED (NR 1 NACELLE) · airframe 39,957 hrs · 18,565 cycles

#1 ENGINE O/B FAN COWL FRAME SUPPORT NEXT TO OIL SERVICES DOOR IS CRACK<[01] REMOVED AND REPLACED #1 ENGINE O/B FAN COWL FRAME SUPPORT NEXT TO OIL SERVICES DOOR AS-PER SRM51-40-02-0G-0;[02] VERIFIED STEP 1

Part: BRACKET — DAMAGED (DOOR SENSOR) · airframe 39,957 hrs · 18,565 cycles

FWD CARGO DOOR WARNING SENSOR COVER ASSY AND BRACKET ENLONGATED HOLES AND COMUN POSITION<[01] REMOVED AND REPLACED COVER AND BRACKET AT FWD CARGO DOOR WARNING SENSOR ASSY;[02] VERIFIED STEP 1

Part: SHIELD — CORRODED (BS 500-500A) · airframe 39,957 hrs · 18,565 cycles

FWD CARGO FLOOR SUPPORT IS CORRODED 24 INCHES RIGHT OF CENTER LINE AT 500 TO 500A<[01] REMOVED AND REPLACED SHIELD AT FWD CARGO COMPT STA 492 TO STA 500A; RBL 21; PER REF SRM 51-40-02-0G-0 AND DWG #143A0080;[02] VERIFIED STEP # 1

Part: FLOOR SUPPORT — CORRODED (BS 767-793 RBL21) · airframe 39,957 hrs · 18,565 cycles

AFT CARGO FLOOR SUPPORT 22 INCHES RIGHT OF CENTER ONE AT 767-787 IS CORRODED.<[01] REMOVED AND REPLACED SHIELD AT AFT CARGO COMPT STA 767 TO STA 793; RBL 21; PER REF SRM 51-40-02-0G-0 AND DWG #146A0081.;[02] RII VERIFIED STEP 1;[03] ALL STEPS ARE COMPLIED WITH

Part: FLOORBEAM — CORRODED (BS 987 RBL 44) · airframe 39,957 hrs · 18,565 cycles

AFT WET AREA FLOOR STRUCTURE FASTENER HOLE WITH CORROSION AT STA 986.5 RBL 44<[01] ACCOMPLISHED REPAIR AT AFT WET AREA FLOOR STRUCTURE AT STA 986.5 RBL 44. REFERENCES: SRM 53-70-51-2R-6; ADDITIONALLY RESTORED AREA OF REPAIR AS PER SRM 51-20-01; SOPM 20-43-03.;[02] VERIFIED STEP 1

Part: SEAL — BROKEN (HORIZONTAL STAB) · airframe 39,957 hrs · 18,565 cycles

RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL IS BROKEN.<[01] REMOVED AND INSTALLED SERVICEABLE LINK ASSEMBLY AT NEW SLIDING SEAL R/H HORIZONTAL STAB FWD UPPER AS PER AMM 53-31-31-000-803 AND SRM 51-40-02-0G-0. INSTALLED R/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL AS PER AMM-53-31-31-400-803.;[02] VERIFIED STEP 1.

Part: FLOORBEAM — CORRODED (BS 987 LBL 38) · airframe 39,957 hrs · 18,565 cycles

AFT WET AREA FLOOR STRUCTURE WITH CORROSION AT STA 986.5+6 LBL 38<[01] REMOVED AND REPLACED ANGLE (PN: 147A5710U1) AT AFT WET AREA FLOOR STRUCTURE STA 986.5+6 LBL 38 REF SRM 51-40-02-0G-0 DWG:147A5700;[02] VERIFIED STEP 1

Part: FLOOR SUPPORT — CORRODED (BS 967-987) · airframe 39,957 hrs · 18,565 cycles

AFT WET AREA FLOOR STRUCTURE WITH CORROSION AT R/H INNER CHORD FROM STA 967 TO STA 986.5+6<[01] REMOVED AND REPLACED R/H INNER CHORD FROM STA. 937 TO 1006 REF. SRM 51-40-02-0G-0 DWG NO. 147A8501;[02] VERIFIED STEP 1

Part: FLOORBEAM — CORRODED (BS 987 RBL 42) · airframe 39,957 hrs · 18,565 cycles

AFT WET AREA FLOOR STRUCTURE WITH CORROSION AT STA 986.5+6 RBL 42.<[01] REMOVED AND REPLACED SUPPORT BRACKET AT AFT WET AREA FLOOR STRUCTURE AT STA 986.5+6 RBL 42 AS-PER SRM 51-40-02-02-0G;[02] VERIFIED STEP 1

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 39,957 hrs · 18,565 cycles

CABIN FLOOR PANEL 242D WITH CORRODED / CRACKED INSERTS AT FWD AND AFT IB CORNERS.<[01] THIS ITEM COMPLETE ON TTG8Q00QXJ94

Part: FLOOR SUPPORT — CRACKED (BS 277-294 BL0) · airframe 39,957 hrs · 18,565 cycles

CABIN FLOOR INTERCOSTAL CRACKED AT BL0 BETWEEN STA 277 & STA 294.5.<[01] REMOVED AND REPLACED NEW INTERCOSTAL AT CABIN FLOOR BL0 STA 277 AS-PER SRM51-40-02-0G-0;[02] VERIFIED FINAL STEP

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 39,957 hrs · 18,565 cycles

CABIN FLOOR PANEL 241XF WITH CORRODED INSERTS AT RH AFT CORNER.<[01] THIS ITEM COMPLETE ON TTG8QOOXHLS;[02] REJECT.... FOR PANEL 241XF LISTED RESOLUTION FAULT TTG8QOOXHLS NOT FOUND. SEE TTG8Q00R9P8E;[03] CORRECTION TO STEP 1: CABIN FLOOR PANEL 241XF WAS REPLACED ON TASKCARD TTG8Q00QXHLS.;[04] VERIFIED STEP 3.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 39,957 hrs · 18,565 cycles

CABIN FLOOR PANEL 241ABF WITH MULTIPLE INSERTS CORRODED / MISSING AT FWD EDGE.<[01] CABIN FLOOR PANEL 241 ABF TO BE REPLACED ON TASKCARD TTG8Q00QXHL9.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,957 hrs · 18,565 cycles

CABIN FLOOR PANEL 231DF UPPER SKIN DELAMINATED.<[01] CABIN FLOOR PANEL 231DF TO BE REPLACED ON TASKCARD TTG8Q00QXJ8J.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,957 hrs · 18,565 cycles

CABIN FLOOR PANEL 241GF UPPER SKIN DELAMINATED WITH FIRST PLY TORN / MISSING IN MULTIPLE AREAS.<[01] RECIVED FLOOR PANEL 241GF;[02] INSTALLATION TO BE ACCOMPLISHED IN CLOSING CARD

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 39,957 hrs · 18,565 cycles

CABIN FLOOR PANEL 241AAF WITH CORRODED INSERTS AT LE.<[01] CABIN FLOOR PANEL 241AAF WAS REPLACED ON TASKCARD TTG8Q00QXHKV.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,957 hrs · 18,565 cycles

CABIN FLOOR PANEL 241RF UPPER SKIN DELAMINATED WITH FIRST PLY TORN / MISSING IN MULTIPLE AREAS.<[01] RECEIVED NEW PANEL INSTALLATION TO BE ACCOMPLISHED ON TASKCARD #TTG8Q00QDJXW;[02] CORRECTION TO STEP #1<BR>RECEIVED NEW PANEL 241RF P/N:146A5810-466<BR>INSTALLATION TO BE ACCOMPLISHED ON TASKCARD #TTG8Q00QDJXW

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 39,957 hrs · 18,565 cycles

CABIN FLOOR PANEL 241E WITH CORRODED INSERTS AT IB LE CORNER.<[01] CABIN FLOOR PANEL 241E TO BE REPLACED ON TASKCARD TTG8Q00QXHKP.

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 39,957 hrs · 18,565 cycles

FWD CABIN FLOOR PANEL 221CF HAS CORRODED INSERTS<[01] RECEIVED CABIN FLOOR PANEL 221CF

Part: SUPPORT ANGLE — BROKEN (RT WG ACCESS PNL) · airframe 39,957 hrs · 18,565 cycles

RIGHT WING FIXED T/E ACCESS PANEL 661AB MOUNT BRACKET; I/B ANGLE SUPPORT BROKEN. 221-01<[01] REMOVED AND REPLACED FITTING AT R/W FIXED T/E ACCESS PANEL 661AB REF. SRM 51-40-02-0G-0;[02] REJECT....BRACKET REPLACED AT ANGLE SUPPORT PANEL 661AB WITH SAFETY WIRE INCORRECTLY INSTALLED AT ATTACH FASTENERS. SEE TTG8Q00R91S5;[03] SAFETY WIRING OF FASTENERS WAS RESOLVED ON TTG8Q00R91S5 REF. AMM 20-10-44-400-801.;[04] VERIFIED STEP 1 AND 3. COMPLETE

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 39,957 hrs · 18,565 cycles

REPAIR L/H MLG STA 663 VAPOR BARRIER<[01] APPLIED REPAIRED AND CURE REPAIRED AT L\H VAPOR BARRIER ON STA 663 BOTH SIDES PER B737 SRM51-70-04-2R-10 PARAGRAPH (4.D); B737 SRM 51-70-04-2R-0 PARAGRAPH (4.L.7) AND PARAGRAPH (4.N.2) MATERIAL USED RESIN EY 3804 PO#2040614; FIBERGLASS PO#1690463 AND USED TEMPERATURE CONTROLLER ID160354 DUE DATE 02\16\24 AND VACUUM GAGE ID 173239 DUE DATE 02\23\24.;[02] VERIFIED STEP 1

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 39,957 hrs · 18,565 cycles

LT MLG WHEEL WELL STA 663 VAPOR BARRIER CRACKED 3' LONG BEHIND HYD SYSTEM B RETURN FILTER.<[01] REMOVED VAPOR BARRIER WEB FOR ACCESS TO REPAIR AT L/H SIDE STA 663 PER REF SRM 51-40-02-0G-0 AND RE-INSTALLED L/H SIDE VAPOR BARRIER STA 663 ONCE REPAIR WAS ACCOMPLISHED PER REF SRM 51-40-02-0G-0 AND DWG#111A1000 AND DWG#111A1001..;[02] RII- VERIFIED STEP 1. COMPLETE

Part: ATTACH FITTING — CRACKED (LT WING TE FLAP) · airframe 39,957 hrs · 18,565 cycles

LT WING IB FLAP OB ATTACH FITTING WITH CRACKED AFT IB RUB PLATE.<[01] REMOVED AND REPLACED TRANSMISSION #3 INBOARD FLAP AFT RUB PLATE REF SRM 51-40-02-0G-0 AND AMM 27-51-13-400-803. TORQUE 175289; DUE DATE 31/07/24.<BR>OPERATED TRAILING EDGE FLAP SYSTEM WITH PRIMARY CONTROL REF AMM 27-51-00-860-801.<BR>OPC IS OK;[02] VERIFIED STEP 1

Part: ACCESS PANEL — BULGED (RT WING) · airframe 39,957 hrs · 18,565 cycles

R/W LOWER MID T/E ACCESS PANEL # 661AB HAS BULGING/CRACKED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGED AREA OF R/W LOWER MID T/E ACCESS PNL #661AB AS PER B737 SRM 51-70-04-2R-9 PARA 4/D-M; 51-70-04-2R-0 PARA 4/M-N. MATERIALS USED #1791128; #1690463; #1775890. TOOLS USED: TEMP CONTROLLER ID#160354 DUE 02/16/24; VAC GAUGE ID#173238 DUE 02/24/24.;[02] VERIFIED STEP 1.

Part: MEGAPHONE — LOOSE (ZN 200 FUS TOP) · airframe 39,865 hrs · 18,517 cycles

FORWARD GALLEY MEGAPHONE WONT STAY IN BRACKET.<[01] INSTALLED FWD. GALLEY MEGAPHONE PER SIP.

Part: LENS — LOOSE (ZN 200 FUS TOP) · airframe 39,572 hrs · 18,350 cycles

CENTER OVERHEAD EMERGENCY SIGNS NOT SECURE<[01] RESECURED OVERHEAD EMERGENCY LENS REF AMM 33-51-01. OK FOR SERVICE

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 38,790 hrs · 17,899 cycles

RT WING ESCAPE SLIDE EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED BATTERY PACK M1671 PER AMM 33-51-06

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 38,134 hrs · 17,521 cycles

LH AFT OVERWING EXIT DOOR EMERGENCY LIGHT INOP.<[01] REMOVED & REPLACED AFT LH OVERWING EXIT DOOR LIGHT REF. AMM 33-51-04. OPS CHECK OK.

Part: CARPET — BURNED (ZN 200 FUS TOP) · airframe 38,010 hrs · 17,447 cycles

LITHIUM BATTERY PACK EXPLODED IN ROW 28 & 29 CAPTAIN SIDE FIRE DAMAGE TO SIDEWALL & CARPET<[01] R&R CENTER ISLE R&H OUTBOARD CARPET REF AMM 25-27-15;[02] REMOVED LH VERY O.B. AFT TWO CARPET SECTIONS AND AIR RETURN GRILLS 2 EACH AT POSITION 29 ABC PER AMM 25-27-15-401-NG.;[03] INSTALLED NEW FLOOR CARPET L/H OUTBOARD STARTING AT ROW 23A AND ENDING AT ROW 30A PER AMM 25-27-15. INSPECTED SIDE WALL FOR CONTRABAND AND INSTALLED NEW SIDE AIR RETURN GRILLS @ 2 EACH AT POSITION 29ABC PER AMM 21-23-03.

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 37,804 hrs · 17,321 cycles

EMERGENCY LIGHT POS 8 ABC LENS COVER MISSING LIGHT OPERATING NORMAL<[01] INSTALLED NEW LENS ON EMERGENCY AISLE EMERGENCY LIGHT 8 ABC PER AMM 33-51-03 OP CHECK OK.

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 37,351 hrs · 17,058 cycles

LEFT FWD OVERWING LOWER EMERGENCY EXIT LIGHT LENS MISSING<[01] INSTALLED LENS IAW AMM 33-51-01

Part: HEATER — FAILED (ZN 200 FUS TOP) · airframe 37,351 hrs · 17,058 cycles

F/A REPORTED BURNING PLASTIC ODOR FROM F/O SIDE REAR LAV. SMOKE ALARM MOMENTARILY ACTIVATED. NO VISIBLE SMOKE OBSERVED.<[01] ACCOMPLISHED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION PER AMM 05-51-56; FOUND WATER HEATER FAILED. OK TO CONTINUE PER MEL 25-10-01; C/W SP # 1B. AUTH # 128777.;[02] R+R AFT RH LAV HEATER REF AM 38-13-01 OPS CHECK GOOD. THIS CLEARS MEL 25-10-01

Part: SLIDE — OUT OF ADJUST (ZN 900 LAV/GALLE) · airframe 36,864 hrs · 16,788 cycles

PLASTIC COVER FOR SLIDE BOTTLE LOOSE ON L1 DOOR. SECURED SIGHT GLASS ON L1 DOOR SLIDE PER AMM 25-66-01;THIS CLEARS MEL 25-10-01

Part: LENS — LOOSE (ZN 200 FUS TOP) · airframe 35,983 hrs · 16,266 cycles

ROW 15 CENTER AISLE CEILING EMERGENCY EXIT SIGN LENS IS NOT SECURE. / [01] SECURED ROW 15 CEILING CENTER AISLE EMERGENCY EXIT LENS PER AMM 33-51-01.

Part: COVER — DISLODGED (ZN 900) · airframe 35,908 hrs · 16,226 cycles

WING EMERGENCY EXIT ASILE SIGN OPENED / [01] SECURED WING ASILE EMERGENCY SIGN COVER IAW AMM 33-51-00.

Part: NONE — MISSING (PAX CABIN) · airframe 35,388 hrs · 15,932 cycles

CEILING EMERGENCY EXIT SIGN AT OVER WING HAS LENS COVER MISSING / [01] RE-SECURED LENS COVER PER SIP

Part: LIGHT — MISSING · airframe 34,010 hrs · 15,161 cycles

LEFT HAND EXIT ROW COVER MISSING / [01] REPLACED LEFT HAND EXIT ROW COVER PER SIP

Part: LIGHT — INOPERATIVE · airframe 33,429 hrs · 14,846 cycles

EMERGENCY LIGHT BATTERY PACK BEHIND KICK PANEL AT ROW 7 DEF IS DEAD / [01] REMOVED REPLACED AND OPS CHECKED EMERGENCY LIGHT BATTERY AT ROW 7DEF PER 33-5106;[02] VERIFIED

Part: RETAINER — MISSING (FWD CARGO BAY) · airframe 33,429 hrs · 14,846 cycles

FWD CARGO PANEL 122EW FWD RETAINER CAP STRIP MISSING. / [01] INSTALLED MISSING CAP STRIP RETAINER PER AMM 25-52-06.

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 33,429 hrs · 14,846 cycles

GUSSET CRACKED IN FWD CARGO BS500I STR19R. / [01] REMOVED; LOCATED AND DRILLED NEW GUSSET IAW SRM 51-40-02. INSTALLATION STILL REQUIRED.;[02] INSTALLED GUSSET IAW SRM 51-40-02.;[03] INSPECTION COMPLETE ON CORRECTIVE ACTION #2 FOR GUSSET REPLACEMENT.

Part: WEB — CRACKED (RH WING) · airframe 33,429 hrs · 14,846 cycles

RIGHT WING DEFLECTION CONTROL RIB WEB CRACKED / [01] REMOVED DAMAGED WEB; LOCATED; DRILLED NEW WEB PER SRM 51-40-02. OK TO INSTALL;[02] REMOVED AND REPLACED PER SRM 51-40-02.

Part: BRACKET — CRACKED (RH WING) · airframe 33,429 hrs · 14,846 cycles

RIGHT WING WEB ANGLE ATTACH BRACKET @ DEFLECTION CONTROL RIB CRACKED / [01] REMOVED DAMAGED BRACKET; LOCATED; DRILLED NEW BRACKET PER SRM 51-40-02. OK TO INSTALL;[02] REMOVED AND REPLACED PER SRM 51-40-02

Part: COWL DOOR — CORRODED (#1 ENGINE) · airframe 33,429 hrs · 14,846 cycles

#1 ENGINE NOSE COWL HAS CORROSION AT 12 O'CLOCK POSITION APPROX. 10INCHES FROM LE (MARKED) / [01] REMOVED .011? MATERIAL FROM ORIGINAL THICKNESS OF .071? FOUND TO BE OUT OF LIMITS IAW SRM 54-10-01?1A.;[02] C/W INSPECTION.;[03] REMOVED AND REPLACED NOSE COWL PER AMM 71-11-01.;[04] C/W INSPECTION.;[05] REMOVED AND REPLACED #1 ENGINE INLET COWL PER AMM 71-11-01.;[06] C/W INSPECTION.

Part: SLIDE — OUT OF POSITION (FWD ENTRY DOOR) · airframe 33,429 hrs · 14,846 cycles

FWD ENTRY DOOR ESCAPE SLIDE FWD GIRTH BAR HOOK LOOSE AT COVER ATTACH POINT. / [01] SECURED RIVETS SECURING GIRT BAR HANGER TO SLIDE CONTAINER PER SRM 51-40-02.

Part: LIGHT — FAULTY (OVERWING EXIT) · airframe 33,056 hrs · 14,646 cycles

INTERIOR OVERWING EXIT SIGNS ABOVE DOORS WILL NOT ILLUMINATE ; / [01] R&R?D BATTERY CHARGER AT STATION 565 RBL 68; NO FIX. REFERENCE AMM 33-51-06. TROUBLE SHOT DOWN TO BATTERY PACKS AT STA 565 RBL 68 AND STA 565 LBL 68. BOTH BATTERY PACKS ON EACH SIDE OF OVERWING EXITS ARE DEAD; CONFIRMED WITH A SLAVED IN BATTERY PACK FROM ANOTHER STATION. RESECURED SLAVED IN BATTERY PACK TO ORIGINAL POSITION.; [02] REPLACED BATTERY PACKS AT STA 565 RBL 68 AND LBL 68. OPS CHECK GOOD. REFERENCE AMM 33-51-06

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 33,018 hrs · 14,626 cycles

L/H O/B AFT FLAP HAS DELAM I/B LOWER SURFACE ; / [01] REMOVED AND REPLACED LH OB AFT FLAP REF AMM 27-51-22.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 14,070 hrs · 31,952 cycles

RT FWD OVERWING EXIT LIGHT COVER BROKEN / REPLACED LIGHT ASSY AND COVER IAW AMM 33-51-01

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 14,070 hrs · 31,952 cycles

RT FWD OVERWING EXIT LIGHT COVER BROKEN / REPLACED LIGHT ASSY AND COVER IAW AMM 33-51-01

Part: LIGHT — LOOSE (CABIN) · airframe 13,963 hrs · 31,772 cycles

FWD SERVICE DOOR EXIT EIGN COVER LOOSE / R&R'D LIGHT ASSY IN REF TO AMM 33-51-04

Part: BULKHEAD WEB — CRACKED (BS 663)

RT MLG WHEEL WELL VAPOR WEB CRACKED 5' LONG. REPAIRED BAPOR WEB CRACK IN RT MLG WHEEL WELL BEHIND HYD SYSTEM 'B' RETURN FILTER PER APB SRM 57-10-10 2.C.(4)(B) ALLOWABLE DAMAGE 2. RE INSPECT EVERY 1200 CYCLES OR MORE FREQUENTLY. MAKE SURE CRACK HAS NOT GROWN PAST THE INTERIM SEAL. IF CRACKE HAS GROWN PAST INTERIM SEAL REFER TO APB SRM 57-10-10. PARAGRAPH H/ALLOWABLE DAMAGE 2 FOR ALLOWABLE LIMITS. REPETITIVE ACTION REQUIRED. / A) REPETITIVE ACTION REQUIRED COMPLIED WITH; NO ADDITIONAL DAMAGE OR DETERIORATION NOTED. OK TO CONTINUE SERVICE IN ACCORDANCE WITH REFERENCE SRM 57-10-10-2.C(4)(B)

Part: COVER — BROKEN (EMERGENCY SIGN) · airframe 13,801 hrs · 31,464 cycles

CENTER AISLE OVERWING EMERGENCY EXIT SIGN COVER BROKEN / R&R CENTER AISLE OVERWING EMERGENCY EXIT SIGN COVER LENS IAW B737 AMM 33-51-01

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 29,247 hrs · 12,610 cycles

RT MLG WHEEL WELL VAPOR WEB CRACKED 5' LONG. REPAIRED VAPOR WEB CRACK IN RT MLG WHEEL WELL BEHIND HYD SYSTEM 'B' RETURN FILTER, PER APB SRM 57-10-10 2.C.(4)(B) ALLOWABLE DAMAGE 2. REINSPECT EVERY 1200 CYCLES OR MORE FREQUENTLY. MAKE SURE CRACK HAS NOT GROWN PAST THE INTERIM SEAL, IF CRACK HAS GROWN PAST INTERIM SEAL REFER TO APB SRM 57-10-10 PARAGRAPH H ALLOWABLE DAMAGE 2 FOR ALLOWABLE LIMITS. REPETITIVE ACTION REQUIRED. RESOLVED ON W/O: 466857 TASKCARD: N/R-00002. RESOLVED ON W/O: 588081 TASKCARD: N/R-00001.

Part: ACOUSTIC LINER — CRACKED (NR 1 ENGINE) · airframe 28,174 hrs · 12,070 cycles

ACCOMPLISH A DYE PENETRANT INSPECTION OF THE CRACK LOCATED ON THE #1 ENGINE EXHAUST ACOUSTIC LINER AT THE 6 O'CLOCK POSITION PER SOPM 20-20-02 WITHIN 10 CYCLES ( MX NOTE ) / CLEARING DMA:0157323ACCOMPLISHED DYE RENETRANT NO FURTHER DEFECTS AT THIS TIME PER AMM 70-40-01 CLEARING#75804

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,174 hrs · 12,070 cycles

EMERGENCY LTS. IN AREA OF L-1 DOOR INOP. / R/R EMRGCY LT. BATTERY PACK M1675 PER AMM 33-51-06. OPS-OK. P/N OFF/ON D717-01-100 S/N OFF 211755 S/N ON 40336

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,034 hrs · 11,570 cycles

EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE AT R1 DOOR. / R&R BULB PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,034 hrs · 11,570 cycles

EMERGENCY LIGHT INOP AT UPPER R/H AFT SERVICE DOOR. / R&R POWER SUPPLY M1672 BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,034 hrs · 11,570 cycles

EMERGENCY LIGHT INOPERATIVE AT UPPER R/H FORWARD SERVICE DOOR. / R&R POWER SUPPLY M2816 BATTERY PACK IAW AMM.

Part: STRIP — DAMAGED (AFT CARGO) · airframe 27,663 hrs · 11,844 cycles

AFT CARGO FWD FLOOR PANEL 140AF FWD SUPPORT CAPSTRIP DAMAGED / RECEIVED SERVICEABLE PART # 725317 WILL BE INSTALLED ON 801593 Q/C 859 (COPY ATTACHED) SA-M 565S

Part: INTERCOSTAL — CORRODED (BS 951 LBL50) · airframe 27,663 hrs · 11,844 cycles

***CORROSION*** AFT CABIN INTERCOSTAL BS 951 LBL 50 WL 208 AT LAV TIEDOWN FITTING / REMOVED CORROSION ON INTERCOSTAL BS 951 LBL 50 WL 208 IN AN AREA OF L.75' X W.0500' X D.080 IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS I.A.W SRM 53-70-51-1A-1. REMOVED INTERCOSTAL I.A.W. SRM 51-40-02-0G-0. INSTALLED NEW INTERCOSTAL I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 147A5650 REV. A P/O# 77921911.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,034 hrs · 11,570 cycles

AFT CABIN INTERCOSTAL CORRODED AT BS 951, LBL 50, AT LAV TIE DOWN FITTING. R&R INTERCOSTAL IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (BS 951) · airframe 27,663 hrs · 11,844 cycles

***CORROSION***ON UPPER FLANGE OF I/B CREASE BEAM CORD AT STA 951+12-986; RBL56; WL207 / REMOVED AND REPLACED NEW REPLACEMENT INNER CHORD ON STA 890 TO STA 1006 RBL 56; WL 207; PART # 147A8540U8; LOT # PO 765207; IAW SRM-51-40-02-0G-0; DWG. 142A8501 CORROSION DAMAGE ON THE ORIGINAL PART FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 27,663 hrs · 11,844 cycles

CABIN FLOOR PANEL 242D HAS UPPER SKIN DAMAGE / REPAIRED UPPER SKIN DAMAGE ON CABIN FLOOR PANEL 242D IAW 737 SRM 53-00-50-2R-0 TABLE 201 AND SRM 53-00-50-2R-1. DETERMINED DAMAGE WAS BEYOND ALLOWABLE LIMITS IAW 737 SRM 53-00-50-1A-1 PARA 4F. REINSTALLED INSERT IAW 737 SRM 53-00-50-2R-0 PARA 5S AND BOEING DWG: 147A5810 ID: 0345 REV:-. 59606U 27JAN20.

Part: CHANNEL — CORRODED (BS 737-847) · airframe 27,663 hrs · 11,844 cycles

***CORROSION*** AFT CARGO LH ZEE CHANNEL STA 737 - 847; LBL 20; WL 156 / CORROSION DAMAGE ON THE AFT CARGO L/H ZEE CHANNEL STA 737-847 LBL 20 WL 156 FOUND TO BE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2 FIG. 103 REMOVED DAMAGED ZEE CHANNEL STA 737-847 AND INSTALLED NEW ZEE CHANNEL WITH REPAIR SPLICES AT LOCATIONS 727J+10 AND 727F+10 LBL 21 IAW SRM 51-40-02-0G-0; 53-00-53-2R-5 AND DWG 146A2500 REV. B

Part: SHIELD — CORRODED (BS 767-787) · airframe 27,034 hrs · 11,570 cycles

AFT CARGO R/H SHIELD CORRODED BETWEEN BS. 767 TO BS. 787. R&R SHIELD IAW SRM & DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,663 hrs · 11,844 cycles

CABIN FLOOR PANEL 241AAF HAS UPPER SKIN DAMAGE / REPAIRED UPPER SKIN DAMAGE ON CABIN FLOOR PANEL 241AAF IAW 737 SRM 53-00-50-2R-0 TABLE 201 AND SRM 53-00-50-2R-1. DETERMINED DAMAGE WAS BEYOND ALLOWABLE LIMITS IAW 737 SRM 53-00-50-1A-1 PARA 4F. REINSTALLED INSERTS IAW 737 SRM 53-00-50-2R-0 PARA 5S AND BOEING DWG:147A5800 ID: 0023 REV:A 59606U 24JAN20.

Part: SUPPORT ANGLE — CORRODED (BS 294-312) · airframe 27,663 hrs · 11,844 cycles

***CORROSION*** ON UPPER FLANGE OF I/B CREASE CORD AT FWD SERVICE DOOR STA294+8-312+1 0; RBL56; WL207 / REMOVED AND REPLACED THRESHOLD SUPPORT ANGLE @ FWD SERVICE DOOR INNER CHORD MOPSILL STA 294+8-312+10 RBL56 WL207 DUE TO OUT OF LIMITS CORROSION 100% MATERIAL LOSS AROUND FASTENER HOLES IAW SRM 51-10-02-0G-0; SRM 51-10-02-0G-0 AND DWG 141A8310

Part: CREASE BEAM — CORRODED (BS 951) · airframe 27,663 hrs · 11,844 cycles

***CORROSION*** ON UPPER FLANGE OF I/B CREASE BEAM CORD AT STA 951+12-986; LBL56; WL207 / REMOVED AND REPLACED INNER CHORD BETWEEN BSTA. 893 AND BSTA 1006; IAW. DWG. 147A8501; SRM. 51-40-02-0G-0 LIMIT STATEMENT L3.0' X W0.75' X D.030' INNER CHORD FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1

Part: SHIELD — CORRODED (BS 767-787) · airframe 27,663 hrs · 11,844 cycles

***CORROSION*** AFT CARGO RH SHIELD STA 767 - 787 / REMOVED & REPLACED AFT CARGO FWD OF DOOR SHIELD STA 767-787 IAW SRM 51-40-02-0G-0; 51-40-05-0G-0 & BOEING DWG 146A0081

Part: WEB — CORRODED (THRESHOLD) · airframe 27,034 hrs · 11,570 cycles

AFT CARGO DOOR THRESHOLD CORRODED BETWEEN BS 787 TO 847, RBL 26. R&R THE WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (BS 890-1006) · airframe 27,034 hrs · 11,570 cycles

UPPER FLANGE OF INBOARD CREASE BEAM CHORD CORRODED AT BS. 890 TO BS. 1006, RBL 56. R&R INNER CHORD IAW SRM & DWG.

Part: CHANNEL — CORRODED (BS 737-847) · airframe 27,034 hrs · 11,570 cycles

AFT CARGO L/H ZEE CHANNEL CORRODED BETWEEN BS. 737 TO BS. 847, LBL 20. / R&R ZEE CHANNEL PER SRM AND DWG.

Part: CHANNEL — CORRODED (BS 727-767) · airframe 27,034 hrs · 11,570 cycles

AFT CARGO RH ZEE CHANNEL CORRODED BETWEEN BS. 727 TO BS. 767, RBL 20. R&R Z CHANNEL IAW SRM AND DWG.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 27,663 hrs · 11,844 cycles

CABIN FLOOR PANEL 242UF HAS UPPER SKIN DAMAGE / CABIN FLOOR PLANEL 242UF UPPER SKIN DAMAGE REPAIRED IAW SRM 53-00-50-2R-1. DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F. NO DELAMINATION ALLOWED.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 27,663 hrs · 11,844 cycles

***CORROSION*** AFT CARGO LH ZEE CHANNEL STA 727F - 737 LBL 20; WL 156 / REPAIR OF AFT CARGO L/H Z CHANNEL STA 727F-737 IS TRANSFERRED TO CUST CARD N245412.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 27,663 hrs · 11,844 cycles

CABIN FLOOR PANEL 241ABF HAS UPPER SKIN DAMAGE / CABIN FLOOR PANEL 241ABF UPPER SKIN DAMAGE REPAIRED IAW SRM 53-00-50-2R-1. DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F. NO DELAMINATION ALLOWED.

Part: WEB — CORRODED (BS 787-847 RBL26) · airframe 27,663 hrs · 11,844 cycles

***CORROSION*** AFT CARGO DOOR THRESHOLD FROM STA 787-847 RBL 26 WL 153 / CORROSION AT AFT CARGO DOOR THRESHOLD FROM STA 787-847 FOUND TO BE OUT OF LIMITS IAW SRM 523-60-15-1A-1 FIG 103 DETAIL D. REMOVED OLD WEB IAW SRM 51-40-02-0G-0 PAR 6C FIG 11. LOCATE; DRILLED; COUNTERSANK AND INSTALLED NEW WEB ITEM 7531818 P.O. 775352 IAW SRM 51-40-05-0G-0. SRM 51-40-08-0G-0. SRM 51-40-02-0G-0 PAR 6 AND DWG 146A8340 REV -. 92058U 01/24/20

Part: CHANNEL — CORRODED (BS 727H-767) · airframe 27,663 hrs · 11,844 cycles

***CORROSION*** AFT CARGO RH ZEE CHANNEL STA 727H - 767 RBL 25 WL 156. / REMOVED AND REPLACED AFT CARGO RH Z CHANNEL STA 727-767 RBL 25 IAW SRM 53-00-53-2R-5 AND DWG 146A7500 SHEET 213 REV -. SPLICE LOCATION AT STA 727G+10. 52901U 24JAN20 WL 156 DUE TO CORROSION DAMAGE ON THE AFT CARGO R/H ZEE CHANNEL BEING OUT OF LIMITS IAW SRM 53-00-53-1A-2

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 27,034 hrs · 11,570 cycles

FORWARD WET AREA INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, LBL 46. / R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 340-360) · airframe 27,663 hrs · 11,844 cycles

FWD WET AREA INTERCOSTAL CRACKED BS340 TO BS360; LBL12 / REMOVED CRACKED INTERCOSTAL BS 340 TO 360 LBL12 I.A.W SRM 51-40-02-0G-0. REMOVED INTERCOSTAL BS 340 TO 360 BL 'O' TO F.O.M. IAW SRM 51-40-02-0G-0. INSTALLED NEW INTERCOSTAL P/O #763090/1 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 REV:- . INSTALLED INTERCOSTAL BS 340 TO 360 BL'O' I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 REV:-.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 27,663 hrs · 11,844 cycles

AFT CARGO FWD CORNER SCUFF PLATE CRACKED / RECEIVED NEW AFT CARGO FWD CORNER SCUFF PLATE PN # 146A8342-8 PO # 768955. LOCATED AND DRILL FWD CORNER SCUFF PLATE IAW SRM 51-40-05-0G-0. PART TO BE INSTALLED ON CUSTOMER CARD 753-140-00-02Y COPY ATTACHED

Part: FLOOR SUPPORT — CRACKED (BS 312-328 RBL30) · airframe 27,663 hrs · 11,844 cycles

FWD WET AREA INTERCOSTAL CRACKED BS312 TO BS328; RBL30.5 / REMOVED CRACKED INTERCOSTAL BS 312 TO 328 RBL 30.5 I.A.W. SRM 51-40-02-0G-0. INSTALLED NEW INTERCOSTAL P/O# 734974/2 I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 REV:-.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 27,663 hrs · 11,844 cycles

AFT CARGO AFT CORNER SCUFF PLATE CRACKED / REPAIRED AFT CARGO AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1 REPAIR 1; AND APB SRM SUPPLEMENT AP37.8-0615 57304C 1/31/20 + SA-M 925 TRACKING# 20200010285.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 27,663 hrs · 11,844 cycles

FWD CARGO AFT CORNER SCUFF PLATE CRACKED / RECEIVED NEW CORNER SCUFF PLATE PO # 5091308. LOCATED AND DRILLED NEW CORNER SCUFF PLATE IAW SRM 51-40-05-0G-0. INSTALLATION TO BE ACCOMPLISHED ON ROUTINE CARD 801593 FUSELAGE 17. 57828U 1/28/2020 REF (753-140-00-01Y) 99749R 28JAN20

Part: CHANNEL — CORRODED (BS 312-328) · airframe 27,663 hrs · 11,844 cycles

***CORROSION*** FSD MOPSILL BS312 TO BS328 RBL56.5 / REMOVED CORROSION ON FWD MOPSILL BS 312 TO 328 RBL 56.5 I.A.W. SRM 51-10-22-0G-0. FOUND TO BE OUT OF LIMITS I.A.W. SRM 53-10-15-1A-2 FIG 103 DETAIL G. REMOVED MOP SILL I.A.W. SRM 51-40-02-0G-0. INSTALLED NEW MOP SILL P/O #766393/1 IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8310 REV:B.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 27,034 hrs · 11,570 cycles

FORWARD WET AREA INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, RBL 30.5. R & R THE INTERCOSTAL IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 312-328 LBL46) · airframe 27,663 hrs · 11,844 cycles

FWD WET AREA INTERCOSTAL CRACKED BS312 TO BS328; LBL46 / REMOVED CRACKED INTERCOSTAL BS 312 TO 328 LBL 46 I.A.W SRM 51-40-02-0G-0. INSTALLED NEW INTERCOSTAL P/O# 734974/R I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 REV:-.

Part: FLOOR SUPPORT — CORRODED (BS 767) · airframe 27,663 hrs · 11,844 cycles

ACB FLOOR PANEL SUPPORT STRAP BS767+5' HAS CORROSION. WL 153; LBL 25 TO RBL 25 / AFTER EVALUATION; FOUND OUT TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. REMOVED AND REPLACED FLOOR PANEL SUPPORT BS 767+5; WL 153; LBL 25-RBL 25 IAW SOPM 20-50-01 57751U 1/27/20

Part: FLOOR SUPPORT — CORRODED (BS 727I) · airframe 27,663 hrs · 11,844 cycles

ACB FLOOR PANEL SUPPORT STRAP BS727I+5' HAS CORROSION. WL 153; LBL 25 TO RBL 25. / AFTER EVALUATION; FOUND OUT TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. REMOVED AND REPLACED FLOOR PANEL SUPPORT BS 727I+5; WL 153; LBL 25-RBL 25 IAW SOPM 20-50-01 57751U 1/27/20

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 27,663 hrs · 11,844 cycles

FWD CARGO FWD CORNER SCUFF PLATE CRACKED / RECIEVED NEW CORNER SCUFF PLATE PO # 777241. LOCATED AND DRILLED NEW CORNER SCUFF PLATE IAW SRM 51-40-05-0G-0. INSTALLATION TO BE ACCOMPLISHED ON ROUTINE CARD # 753-140-00-01Y. 57828U 1/28/2020

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 27,663 hrs · 11,844 cycles

***CORROSION*** FWD CARGO FLOOR PANEL 120DF HAS CORROSION / REPLACED FWD CARGO PANEL 120DF WITH ATSHFAB-200-305 PO# 702228 IAW AMM 25-52-01-201-801 57901U 22JAN20 CORROSION DAMAGE ON THE ORIGINAL PART FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 27,663 hrs · 11,844 cycles

***CORROSION*** FLOOR PANEL 120AF HAS CORROSION / REPLACED FWD CARGO FLOOR PANEL 120AF WITH ATSHFAB-200-301 PO# 702228 IAW AMM 25-52-01-201-801 57901U 22JAN20 CORROSION DAMAGE ON THE ORIGINAL PART FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 27,663 hrs · 11,844 cycles

***CORROSION*** FWD CARGO FLOOR PANEL 120BF HAS CORROSION / REPLACED FWD CARGO FLOOR PANEL 120BF WITH ATSHFAB-200-303 PO# 702228 IAW AMM 25-52-01-201-801 57901U 22JAN20 CORROSION DAMAGE ON THE ORIGINAL PART FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1

Part: CREASE BEAM — CORRODED (BS 893-1006) · airframe 27,034 hrs · 11,570 cycles

UPPER FLANGE OF INBOARD CREASE BEAM CHORD CORRODED BETWEEN BS. 893 TO BS. 1006, LBL 56. / R&R INNER CHORD IAW DWG & SRM.

Part: SUPPORT ANGLE — CORRODED (BS 294-312) · airframe 27,034 hrs · 11,570 cycles

CORROSION FOUND ON UPPER FLANGE OF INBOARD CREASE BEAM AT FORWARD SERVICE DOOR BS 294+8 - 312+1 0, RBL 56, WL 207. REMOVED AND REPLACED THE THRESHOLD SUPPORT ANGLE AT FORWARD SERVICE DOOR INNER CHORD MOPSILL STA 294+8-312+10 RBL56 WL207 DUE TO OUT OF LIMITS CORROSION 100% MATERIAL LOSS AROUND FASTENER HOLES IAW SRM 51-10-02-0G-0, SRM 51-10-02-0G-0 AND DRAWING 141A8310.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,534 hrs · 11,786 cycles

L2 DOOR EXTERNAL EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 26,776 hrs · 11,460 cycles

R/H MAIN LANDING GEAR WHEEL WELL AFT PRESSURE BULKHEAD VAPOR WEB CRACKED. / REPAIRED VAPOR WEB PER SRM.

Part: NONE — CRACKED (CABIN) · airframe 26,395 hrs · 11,376 cycles

PASSENGER CABIN FLOOR BOARD BREAK ASSY CRACKED AT STA 540 LT OF CENTER / REMOVED AND REPLACED CABIN FLOOR BOARD BREAK ASSY AT STA 540 LT OF CENTER IAW SRM 51-40-02

Part: NONE — CRACKED (CABIN) · airframe 26,395 hrs · 11,376 cycles

PASSENGER CABIN FLOOR BOARD BREAK ASSY CRACKED AT STA 540 LT OF CENTER / REMOVED AND REPLACED CABIN FLOOR BOARD BREAK ASSY AT STA 540 LT OF CENTER IAW SRM 51-40-02.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 26,558 hrs · 11,357 cycles

CENTER SECTION OF THE AFT CARGO SCUFF PLATE IS CRACKED AT THE FWD STOP PIN CONTACT POINT. / REMOVED AND REPLACED PER MM 53-11-01. (INSP 39215)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,877 hrs · 10,608 cycles

L/H AFT EMERGENCY EXIT OFF WING LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 24,877 hrs · 10,608 cycles

AFT L/H EMERGENCY EXIT ROW EMERGENCY LIGHT DAMAGED. R&R SIGN PER AMM.

Part: DOUBLER — CRACKED (FWD FUSELAGE) · airframe 24,294 hrs · 10,354 cycles

WHILE CONNECTING GROUND POWER NOTICED A CRACK AROUND THE FWD RIVET AT THE BOTTOM INITIAL RUBBING BLOCK ON THE EGPR DOUBLER AT THE EXTERNAL POWER RECEPTACLE. THERE IS ALSO A GAP BETWEEN THE EGPR SURROUND DOUBLER AND EGPR STIFFENER / REPAIRED EXTERNAL GROUND POWER RECEPTACLE SURROUND. THIS IS A CATEGORY 'A' REPAIR AND IS CONSIDERED PERMANENT REQUIRING NO ADDITIONAL INSPECTIONS REF SRM 53-10-15-2R-4. SA-M 326: A948155

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 24,127 hrs · 10,283 cycles

RT MAIN LANDING GEAR WHEEL WELL VAPOR WEB CRACKED. REPAIRED WEB PER SRM/

Part: BATTERY — FAILED (CABIN) · airframe 22,889 hrs · 9,731 cycles

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

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 20,500 hrs · 8,708 cycles

AFT CARGO BAY BETWEEN STA 727C AND STA 827 L/H Z ANGLE IS CORRODED IN SEVERAL AREAS TOP AND BOTTOM SIDES AS MARKED / REMOVED + REPLACED Z ANGLE L/H STA 727 TO 827 IAW SRM 51-40-02 + DWG 146A7500 REV: - MATERIAL LOSS IS 100% OUT OF LIMITS IAW SRM 53-00-053

Part: PLATE — CRACKED (LT WING) · airframe 20,500 hrs · 8,708 cycles

LH WING AT #3 FLAP TRACK WIGGLE PLATE FOR PANEL 551 EB CRACKED. / L/H WING #3 FLAPTRACK WIGGLE PLATE FOR PNL 551EB CRACKED DRILLED & REMOVED CRACKED WIGGLE PLATE I/A/W SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW L/H WING WIGGLE PLATE IAW SRM 51-40-05-0G-0 ALSO AIPC 57-50-00-224. INSTALLED NEW L/H WING WIGGLE PLATE; I/A/W SRM 51-40-02-0G-0 ALSO AIPC 57-50-00-22A SHEET 003 PG 21. PRIMED AND TOP COAT I/A/W AMM 51-21-72-370-802; AMM 51-21-73-370-801.

Part: PLATE — CRACKED (LT WING) · airframe 19,650 hrs · 8,327 cycles

LEFT WING NR 3 FLAP TRACK WIGGLE PLATE FOR PANEL 551EB CRACKED. R & R THE PLATE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (BS 867) · airframe 19,650 hrs · 8,327 cycles

AFT CARGO BAY SUPPORT ANGLE CRACKED AT BS 867, BETWEEN STRINGERS 26L TO 27L. R & R THE SUPPORT ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 20,500 hrs · 8,708 cycles

FORWARD CARGO PIT; STA 500I; BULK HEAD PANEL AREA; LOWER 'L' ANGLE IS CORRODED IN MULTIPLE AREAS [MARKED] / REMOVED AND REPLACED LOWER L ANGLE FWD CARGO PIT STA 500I IAW SRM 51-40-02 + DWG 143A7902 REV: E

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 20,500 hrs · 8,708 cycles

AFT CARGO BAY AT STA 867 BETWEEN STR 26L AND 27L SUPPORT ANGLE FOR WASTE TANK REMOVABLE BULKHEAD FRAME WORK IS CRACKED AS MARKED / REMOVED AFT CARGO BAY SUPPORT ANGLE @ STA 867 BETWEEN STR 26L-27L IAW SRM 51-40-02-0G-0; VERFIED NEW BRACKET AS PART NO. 149A8109414 A-TAG A53652 IAW BOEING OWG 149A8109 REV:B; LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-05-0G-0 AND BOEING DWG 149A8109 REV:B INSTALLED AFT CARGO BAY SUPPORT BRACKET @ STA 867 BETWEEN STR 26L-27L IAW BOEING DWG 149A8109 REV'B AND SRM 51-40-02-0G-0

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 20,500 hrs · 8,708 cycles

AFT CARGO BAY BETWEEN STA 767 AND STA 793 FWD DOOR SHIELD IS CORRODED ON TOP AND BOTTOM SIDES AS MARKED / REMOVED CORROSION/ VERIFIED LIMITS AT AFT CARGO FWD DOOR SHIELD FROM STA 767 TO 793R (ORIGINAL T: .050') (LOSS: .008') (REMAINING: .042') OUT OF LIMITS IAW SRM 53-60-15-1A-1. REMOVED AND REPLACED AFT CARGO R/H SHIELD FROM STA 767 TO 793R IAW BOEING DWG #145A0081 REV A. TOOL ID #36649 DUE: 07/05/2018 TAG# WN6441

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,650 hrs · 8,327 cycles

AFT CARGO BAY Z ANGLE CORRODED BETWEEN BS 727C TO BS 827, LT. R&R Z ANGLE IAW SRM & DWG.

Part: BULKHEAD — DELAMINATED (RT MLG WW) · airframe 19,650 hrs · 8,327 cycles

RT MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER BULKHEAD REPAIR DELAMINATED AT BS 663. REPAIRED BULKHEAD IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 19,942 hrs · 8,449 cycles

CENTER AISLE OVERWING EXIT SIGN BROKEN. R&R SIGN ASSEMBLY PER MM.

Part: SEAL — CRACKED (RH HOR STAB) · airframe 19,745 hrs · 8,368 cycles

RIGHT HORIZONTAL UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED RH SIDE HORIZONTAL ZIPPER SLIDING SEAL PER AMM 53-31-31

Part: SEAL — CRACKED (LH HOR STAB) · airframe 19,745 hrs · 8,368 cycles

LEFT HORIZONTAL UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED LH SIDE HORIZONTAL UPPER SLIDING SEAL PER AMM 53-31-31

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 19,738 hrs · 8,351 cycles

FWD CARGO GUSSET CRACKED STR19RH STA 500I / REMOVED CRACKED GUSSET AT STR 19R BS 500I IAW SRM 51-40-02. LOCATED AND DRILLED NEW GUSSET AND INSTALLED IAW SRM 51-40-05; SRM 51-40-02 AND BOEING DRAWING 143A7902

Part: LENS — CRACKED (CABIN) · airframe 17,823 hrs · 7,543 cycles

EMERGENCY LIGHT LENS CRACKED AT SEAT ROW 8C. R&R LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 17,823 hrs · 7,543 cycles

EMERGENCY LIGHT LENS MISSING AT SEAT ROW 10D. INSTALLED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 17,823 hrs · 7,543 cycles

EMERGENCY LIGHT LENS CRACKED AT SEAT ROW 10D. R&R LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 17,823 hrs · 7,543 cycles

EMERGENCY LIGHT LENS CRACKED AT SEAT ROW 5C. R&R LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 17,823 hrs · 7,543 cycles

EMERGENCY LIGHT LENS CRACKED AT SEAT ROW 21D.

Part: LENS — CRACKED (CABIN) · airframe 17,823 hrs · 7,543 cycles

EMERGENCY LIGHT LENS CRACKED AT SEAT ROW 12C. R&R LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 17,823 hrs · 7,543 cycles

EMERGENCY LIGHT LENS CRACKED AT SEAT ROW 15C. R&R LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 17,823 hrs · 7,543 cycles

EMERGENCY LIGHT LENS CRACKED AT SEAT ROW 7D. R&R LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 17,823 hrs · 7,543 cycles

EMERGENCY LIGHT LENS CRACKED AT SEAT ROW 23C. R&R LENS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 17,429 hrs · 7,366 cycles

EMERGENCY EXIT LIGHT LENS MISSING AT 27C. REPLACED THE LENS IAW MM.

Part: COVER — MISSING (CABIN) · airframe 14,706 hrs · 6,164 cycles

AFT EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER IAW MM.

Part: LENS — MISSING (CABIN) · airframe 14,044 hrs · 5,910 cycles

RIGHT AISLE EMER LIGHT LENS MISSING, BETWEEN ROW 22 - 25. INSTALLED LENS IAW AMM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 13,564 hrs · 5,712 cycles

R1 DOOR GIRT BAR HOOK LOOSE. R & R HOOK IAW SIP.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 13,365 hrs · 5,614 cycles

RIGHT MLG WW VAPOR WEB CRACKED. REPAIRED WEB IAW SRM.

Part: LENS — CRACKED (CABIN) · airframe 13,322 hrs · 5,594 cycles

ENTRYWAY EMER EXIT LIGHT LENS CRACKED. R & R LIGHT ASSEMBLY IAW AMM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 10,567 hrs · 4,439 cycles

RIGHT MLG WW VAPOR WEB CRACKED. REPAIRED WEB IAW SRM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 10,565 hrs · 4,438 cycles

R1 DOOR EXIT SIGN COVER LOOSE. SECURED COVER IAW AMM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 10,567 hrs · 4,439 cycles

R1 DOOR EXIT SIGN COVER LOOSE. SECURED COVER IAW SIP.

Part: LIGHT — BROKEN (CABIN) · airframe 5,001 hrs · 1,952 cycles

R1 EMERGENCY EXIT LIGHT BASE BROKEN. R & R LIGHT IAW SIP.

Part: LENS — DAMAGED (CABIN) · airframe 4,776 hrs · 1,861 cycles

LT OVERHEAD EMERGENCY LIGHT BEZEL DAMAGED AT ROW 23. R & R LENS IAW AMM.

Part: LATCH — LOOSE (R2 DOOR) · airframe 4,776 hrs · 1,861 cycles

R2 DOOR EMERGENCY EVAC SLIDE LATCH LOOSE. SECURED LATCH IAW CMM.

Part: LENS — CRACKED (CABIN) · airframe 4,776 hrs · 1,861 cycles

LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS CRACKED AT ROW 8. R & R LENS IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 3,796 hrs · 1,470 cycles

FOUND FWD ENTRY EMERGENCY EXIT FLOOR LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: LIGHT — DAMAGED (OVERWING EXIT) · airframe 1,013 hrs · 341 cycles

OVERWING EMERGENCY EXIT LIGHT DAMAGED. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 1,013 hrs · 341 cycles

RIGHT FWD EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LENS — BROKEN (CABIN) · airframe 395 hrs · 121 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.