N8327A

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 41,413 hrs · 19,826 cycles

EMERGENCY LIGHT LENSE MISSING AT 10DEF. REPLACED EMERGENCY LIGHT LENS IAW AMM 33-51-00.

Part: COVER — MISSING (ZONE 200) · airframe 40,998 hrs · 19,620 cycles

EMERGENCY EXIT LIGHT SIGN COVER MISSING. INSTALLED ROW 14A EMERGENCY EXIT SIN COVER REF AMM 33-51-02

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 40,231 hrs · 19,221 cycles

VARIOUS EMERGENCY LIGHTS INOP<[01] FOUND BATTERY PACK AT LOCATION M1676 TO BE AT FAULT REPLACED BATTERY WITH NEW. OPS CHECK GOOD. WORK DONE PER AMM 33-51-06.

Part: LIGHT — DETACHED (ZONE 200) · airframe 40,226 hrs · 19,219 cycles

CTR AISLE EMER EXIT LIGHT ASSY FELL DOWN. RESECURED AISLE OVHD EMER EXIT LIGHT ASSY PER AMM 33-51-03.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 40,187 hrs · 19,199 cycles

AFT RIGHT HAND OVER WING EXIT SIGN AT STATION 639 IS HALF LIT. RELAMPED AFT RH OWE SIGN AT STA 639 (LOWER RECTANGULAR SIGN BEHIND OWE) AND OPS CHECK FOR THE LIGHT ASSEMBLY GOOD IAW B737-800 AMM 33-51-01-960-801.

Part: TAIL CONE — PULLED (ZONE 600) · airframe 39,081 hrs · 18,606 cycles

RT WING #6 FLAP CANOE FAIRING TAIL CONE HAS PULLED FASTENER ON O/B SIDE. <[01] REMOVED AND REPLACED PULLED FASTENER ON RT WING #6 FLAP CANOE FAIRING TAIL CONE ON O/B SIDE. REF SRM 51-40-02.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

EMER LIGHT AT SEAT ROW 15ABC INOP 2024-600631<[01] REPLACED EMER LIGHT AT SEAT ROW 15ABC AT PASSENGER CABIN I.A.W. B737-800 AMM 33-51-03-960-803 STEP 4. D.(1) AND (2).;[02] CORRECTED STEP 1<BR>REPLACED EMER LIGHT AT SEAT ROW 15ABC AT PASSENGER CABIN I.A.W. B737-800 AMM 33-51-03-960-805;[03] CERTIFIED CORRECTIVE ACTION STEP 2

Part: HANDLE — LOOSE (ZONE 800) · airframe 38,276 hrs · 18,139 cycles

PAX CABIN FWD SERVICE DOOR LINING AREA ASSISTANT HANDLE LOOSE 2024-600640<[01] TIGHTENED FWD SERVICE DOOR LINING ASSISTANT HANDLE I.A.W B737-800 AMM 52-41-31-400-802 STEP 3.F ITEM (2).(D);[02] TASK COMPLETED

Part: SLIDE — OUT OF POSITION (ZONE 800) · airframe 38,276 hrs · 18,139 cycles

PAX CABIN AFT LEFT DOOR LOWER SLIDE COVER IS RUBBING AGAINST TO DOOR SCUFF PLATE 2024-600628<[01] REPOSITIONED AFT LEFT DOOR LOWER SLIDE COVER IAW MT 725-61-06;[02] TASK COMPLETED

Part: RIB — CRACKED (ZONE 300) · airframe 38,276 hrs · 18,139 cycles

CRACK LEADING EDGE RIB LOCATED ACCCES PANEL 341B LE STA 105.26 AT RT HORIZONTAL STABILIZER 2024-600586<[01] REPLACED LEADING EDGE RIB LOCATED ACCCES PANEL 341B LE STA 105.26 AT RT HORIZONTAL STABILIZER IAW B737-800 SRM 51-10-02; ITEM 9 AND SRM 51-40-02 AND DWG 186A1001 SHEET: 19 REV. -:; SEE INDIVIDUAL SINGS OFF BELOW;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: RIB — CRACKED (ZONE 300) · airframe 38,276 hrs · 18,139 cycles

CRACK ON RIB LOCATED LE STA 78.29 ON ACCESS PANEL 331B AT LT HORIZONTAL STABILIZER 2024-600579<[01] RE0LACED RIB LOCATED LE STA 78.29 ON ACCESS PANEL 331B AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02 AND DWG 186A1001 SHEET: 19 REV. -:; SEE INDIVIDUAL SINGS OFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED RIB LOCATED LE STA 78.29 ON ACCESS PANEL 331B AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 186A1001 SHEET: 19 REV. -:; SEE INDIVIDUAL SINGS OFF BELOW;[03] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: ACCESS PANEL — DELAMINATED (ZONE 600) · airframe 38,276 hrs · 18,139 cycles

DELAMINATED HOLE (2EA) IN ACCESS PANEL 661CB AT RT WING 2024-600552<[01] TOOL USED: CALIPER PN: 500-197-30; SN: B20189521; DUE DATE: 26-JAN-25;[02] TOOL USED: HOT BONDER PN: HCS9200B SN: 15102320; DUE DATE: 25-JAN-25;[03] TOOL USED: SCALE PN: SPX222; SN: C410738991; DUE DATE: 05-AUG-25;[04] TOOL USED: SCALE P/N: CR5200; S/N: 8343110814; DUE DATE: 20-JAN-25.;[05] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18196127; DUE DATE: 25-JAN-25.;[06] TOOL USED: ULTRASONIC FLAW DETECTOR P/N: USM GO+; S/N: USMGO11040089; CAL DUE DATE: 21-MAY-25;[07] TOOL USED: HUMIDITY/TEMPERATURE CHART RECORDER P/N: RH550; S/N: 240531238; DUE DATE: 10/SEP/25.;[08] TOOL USED: MULTIMETER P/N: FLUKE 87; S/N: 90160155; DUE DATE: 26-JAN-25.;[09] REPAIRED ACCESS PANEL 661CB AT RT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[10] REPAIRED ACCESS PANEL 661CB AT RT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: WEB — CORRODED (ZONE 600) · airframe 38,276 hrs · 18,139 cycles

CORROSION ON WEB FIXED LEADING EDGE AT LEVEL OFSS 308 AT RT WING 2024-600554<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3015GOES00000 S/N 142811019 DUE DATE 23 JAN 25.;[02] REPLACED WEB (NOSE BEAM) FIXED LEADING EDGE AT LEVEL OFSS 308 AT RT WIN I.A.W B737-800 SRM 51-40-02-0G-0; SRM 51-10-02 Ï¿½TEM 9 AND DWG# 116A5600; SHEET 35; REV.-; DWG: 116A5300; SHEET: 22 REV: -; SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED WEB (NOSE BEAM) FIXED LEADING EDGE AT LEVEL OFSS 308 AT RT WIN I.A.W B737-800 SRM 51-40-02-0G-0; SRM 51-10-02 Ï¿½TEM 9 AND DWG# 116A5600; SHEET 35; REV.-; DWG: 116A5300; SHEET: 22 REV: -; SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT ANGLE — CORRODED (ZONE 600) · airframe 38,276 hrs · 18,139 cycles

CORROSION ON BONDING JUMPER ANGLE SUPPORT OF AFT BOOST PUMP TANK 2 I/B TRAILING EDGE AT RT WING (2EA) 2024-600553<[01] REPLACED INBOARD TRAILING EDGE BONDING JUMPER SUPPORT ANGLE OF AFT BOOST PUMP TANK 2 AT RT WING (2 EA) IAW B737-800 AMM 28-22-41-400-801. STEP 3.H.(18);(20);(21);(22). AND PERFORMED RESISTANCE TEST IS OK. TOOL USED: BONDING METER PN:M1 MILLIOHM METER; S/N:DC007483; DUE DATE:29 JUL 25.;[02] REPLACED INBOARD TRAILING EDGE BONDING JUMPER SUPPORT ANGLE OF AFT BOOST PUMP TANK 2 AT RT WING (2 EA) IAW B737-800 AMM 28-22-41-400-801. STEP 3.H.(18);(20);(21);(22). AND PERFORMED RESISTANCE TEST IS OK. TOOL USED: BONDING METER PN:M1 MILLIOHM METER; S/N:DC007483; DUE DATE:29 JUL 25.

Part: ANGLE — DAMAGED (ZONE 600) · airframe 38,276 hrs · 18,139 cycles

ELONGATED HOLE ACCESS PANEL 651GB TRAILING EDGE T ANGLE AT RT WING 2024-600557<[01] REPLACED T ANGLE LOC. ACCESS PANEL 651GB TRAILING EDGE AT RT WING I.A.W B737-800 SRM: 51-40-02 AND DWG: 115A2714 SHEET 13; REV. A.;[02] REPLACED T ANGLE LOC. ACCESS PANEL 651GB TRAILING EDGE AT RT WING I.A.W B737-800 SRM: 51-40-02 AND DWG: 115A2714 SHEET 13; REV. A.

Part: WEB — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK ON WEB LOCATED UPPER AREA BTW BS 847 TO BS 867 LBL 20 AT AFT CARGO COMPARTMENT 2024-600531<[01] REPLACED WEB LOCATED UPPER AREA BTW BS 847 TO BS 867 LBL 20 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 149A8100; SHEET: 1 AND REV -: . TOOL USED: DIGITAL CALIPER PN: 500-196-300; SN: B21141522 AND DUE DATE: 07/NOV/24;[02] TASK COMPLETED

Part: WEB — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK ON WEB LOCATED BTW BS 927 TO BS 947.5 AT AFT CARGO COMPARTMENT 2024-600532<[01] REPLACED WEB LOCATED BTW BS 927 TO BS 947.5 AT AFT CARGO COMPARTMENT I.A.W B737-800 SRM 51-10-02-0G-0 AND DWG 147A7500 SHEET 36 REV ?-? MEASURE OF CRACK IS L: 0.889 IN TOOL USED DIGITAL CALIPER P/N: 500-196-300 S/N:B21141522 DUE DATE: 07 NOV 24;[02] CORRECTED STEP 1 <BR>REPLACED WEB LOCATED BTW BS 927 TO BS 947.5 STR26R AT AFT CARGO COMPARTMENT I.A.W B737-800 SRM 51-10-02-0G-0 AND DWG 147A7500 SHEET 36 REV ?-? MEASURE OF CRACK IS L: 0.889 IN TOOL USED DIGITAL CALIPER P/N: 500-196-300 S/N:B21141522 DUE DATE: 07 NOV 24;[03] TASK COMPLETED

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK ON CARGO TRACK LOCATED BS 727I RBL 13.84 AT AFT CARGO COMPARTMENT 2024-600537<[01] STEPS 5 AND 7 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 200048001;CAL DUE DATE: 28-MAY-25;[02] TOOL USED ON STEP 13 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[03] PERFORMED PERMANENT REPAIR ON CARGO TRACK LOCATED BETWEEN BS 727H TO BS 767 RBL 13.84 AT AFT CARGO COMPARTMENT I.A.W B737-800 SRM 53-00-53-2R-3; REPAIR 3. AND DWG# 146A7500; SHEET 113; REV.-. AND DWG# 146A7501; SHEET 27; REV.-. SEE INDIVIDUAL SIGN OF BELOW.;[04] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OF BELOW

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK ON SUPPORT ANGLE LOCATED CEILING AREA BS 727B LBL 52 AT AFT CARGO COMPARTMENT 2024-600530<[01] ON STEP 4; TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 210138003; DUE DATE: 11-JUN-25;[02] PERFORMED PERMANENT REPAIR ON SUPPORT ANGLE LOCATED CEILING AREA BS 727B LBL 52 AT AFT CARGO COMPARTMENT I.A.W. B737-800 SRM 51-70-11-2R-0.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] TASK CARD COMPLETED <BR>PERFORMED PERMANENT REPAIR ON SUPPORT ANGLE LOCATED CEILING AREA BS 727B LBL 52 AT AFT CARGO COMPARTMENT I.A.W. B737-800 SRM 51-70-11-2R-0.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: SUPPORT — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK SUPPORT ZEE LOCATED BS 747 LBL 22 AFT CARGO COMPARTMENT 2024-600538<[01] PERFORMED REPAIR LOCATED BETWEEN BS727I TO BS847 LBL 22 AFT CARGO COMPARTMENT IAW B737-800 SRM 53-00-53-2R-6 REPAIR 6. <BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] CERTIFIED RII MAJOR REPAIR WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK ON CARGO TRACK LOCATED BS 747 RBL 13.84 AT AFT CARGO COMPARTMENT 2024-600536<[01] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00W69Y6;[02] SEE INDIVIDUAL SIGN OF BELOW;[03] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00W69Y6 ; RII <BR>SEE INDIVIDUAL SIGN OF BELOW ;

Part: ANGLE — CRACKED (ZONE 500) · airframe 38,276 hrs · 18,139 cycles

CRACK ANGLE TRAILING EDGE ORSS 274 DEFLECTION CONTROL RIB BEAM AREA LT WING 2024-600533<[01] REPLACED ANGLE TRAILING EDGE ORSS 274 DEFLECTION CONTROL RIB BEAM AREA LT WING I.A.W. B737-800 SRM 51-40-02 AND DWG 115A6200 SHEET 17 REV. A <BR><BR>CRACK LENGTH: 1.700? <BR><BR>TOOL USED CALIPER P/N: 500-197-30 S/N: B23394221 DUE DATE: 04/FEB/25;[02] REPLACED ANGLE TRAILING EDGE ORSS 274 DEFLECTION CONTROL RIB BEAM AREA LT WING I.A.W. B737-800 SRM 51-40-02 AND DWG 115A6200 SHEET 17 REV. A

Part: PLATE — CRACKED (ZONE 600) · airframe 38,276 hrs · 18,139 cycles

CRACK OUTBOARD TRAILING EDGE CORRUGATED PLATE ORSS 297 AT RT WING 2024-600541<[01] REPLACED OUTBOARD TRAILING EDGE CORRUGATED PLATE ORSS 297 AT RT WING IAW B737-800 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9. AND DWG 115A3700 SHEET 72. REV:- TOOL USED CALIPER DIGITAL P/N:500-196-30 S/N:A23329415 DUE DATE:06-MAR-25.;[02] TASK CARD COMPLETED

Part: FITTING — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK ON FITTING LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-600534<[01] REPLACED FITTING LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 149A8103 SHEET 8 REV-. TOOL USED DIGITAL CALIPER P/N: 500-196-300 S/N:B21141522 DUE DATE: 07 NOV 24.;[02] REPLACED FITTING LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 149A8103 SHEET 8 REV-. TOOL USED DIGITAL CALIPER P/N: 500-196-300 S/N:B21141522 DUE DATE: 07 NOV 24.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 727 BTW STR 25L TO STR 25R AT AFT CARGO COMPARTMENT 2024-600549<[01] REPLACED SUPPORT ANGLE LOCATED BS 727 BTW STR 25L TO STR 25R AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9. TOOL USED: ELECTRONIC CALIPER P/N: 500-196-30; S/N: B23343124 AND DUE DATE: 09-MAR-25.;[02] CORRECTED STEP 1 <BR>REPLACED SUPPORT ANGLE LOCATED BS 727 BTW STR 25L TO STR 25R AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9. TOOL USED: ELECTRONIC CALIPER P/N: 500-196-30; S/N: B23343124 AND DUE DATE: 09-MAR-25.<BR><BR>ANGLE MUST BE INSTALLED WITHIN: TTG8Q00VMT3Y.;[03] TASK COMPLETED

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-600535<[01] REPLACED SUPPORT ANGLE LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40-02<BR><BR>CRACK LENGHT IS: 0.364 INCHES .TOOL USED IS: DIGITAL CALIPER P/N: 500-197-30 S/N: 23316868 DUE DATE: 04-FEB-25;[02] REPLACED SUPPORT ANGLE LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40-02<BR><BR>CRACK LENGHT IS: 0.364 INCHES .TOOL USED IS: DIGITAL CALIPER P/N: 500-197-30 S/N: 23316868 DUE DATE: 04-FEB-25

Part: ANGLE — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK ON GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 19R AT FWD CARGO COMPARTMENT 2024-600504<[01] REPLACED GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 19R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 143A7902 SHEET: 257 REV: B . SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 19R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 143A7902 SHEET: 257 REV: B . SEE INDIVIDUAL SIGNOFFS BELOW

Part: ANGLE — CRACKED (ZON E100) · airframe 38,276 hrs · 18,139 cycles

CRACK ON ANGLE LOCATED FWD FACE BS 500G AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-600515<[01] REPLACED ANGLE LOCATED FWD FACE BS 500G AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9. AND DRAWING # 143A7505 SHEET 109 REV. -.;[02] CORRECTED STEP 1.REPLACED ANGLE LOCATED FWD FACE BS 500G AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9. AND DRAWING # 143A7505 SHEET 108 REV. -.;[03] INSTALLED ANGLE AND FASTENERS LOCATED FWD FACE BS 500G AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DRAWING # 143A7505 SHEET 108 REV. -

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

CRACK SUPPORT ANGLE LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN 2024-600513<[01] REPLACED SUPPORT ANGLE LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN IAW B737-800 SRM 51-10-02-0G-0 ITEM 9 ; SRM 51-40-02-0G-0 AND DWG 146A7901 SHEET 66 REV: A ; MEASUREMENT OF CRACK IS: 0.466? TOOL USED: ELECTRONIC CALIPER P/N: 500-196-30 S/N:A23329415 DUE DATE: 06-MAR-25.;[02] REPLACED SUPPORT ANGLE LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN IAW B737-800 SRM 51-10-02-0G-0 ITEM 9 ; SRM 51-40-02-0G-0 AND DWG 146A7901 SHEET 66 REV: A ; MEASUREMENT OF CRACK IS: 0.466? TOOL USED: ELECTRONIC CALIPER P/N: 500-196-30 S/N:A23329415 DUE DATE: 06-MAR-25.

Part: ANGLE — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK ON ANGLE LOCATED FWD FACE BS 500G AT LEVEL STR 26R AT FWD CARGO COMPARTMENT 2024- 600512<[01] REPLACED ANGLE LOCATED FWD FACE BS 500G AT LEVEL STR 26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9. AND DRAWING # 143A7505 SHEET 109 REV. -.;[02] REPLACED ANGLE LOCATED FWD FACE BS 500G AT LEVEL STR 26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9. AND DRAWING # 143A7505 SHEET 108 REV. -.;[03] REPLACED ANGLE LOCATED FWD FACE BS 500G AT LEVEL STR 26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9. AND DRAWING # 143A7505 SHEET 108 REV. -.

Part: ANGLE — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK ON ANGLE LOCATED FWD FACE BS 500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-600517<[01] REPLACED ANGLE LOCATED FWD FACE BS 500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 143A7505 REV:-. LENGTH OF CRACK IS: 0.543? TOOL USED ELECTRONIC CALIPER P/N:500-196-30 S/N:A23048326 DUE DATE: 05-JUN-25;[02] REPLACED ANGLE LOCATED FWD FACE BS 500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 143A7505 REV:-. LENGTH OF CRACK IS: 0.543? TOOL USED ELECTRONIC CALIPER P/N:500-196-30 S/N:A23048326 DUE DATE: 05-JUN-25

Part: ANGLE — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK ON ANGLE LOCATED FWD FACE BS 500H AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-600516<[01] REPLACED ANGLE LOCATED FWD FACE BS 500H AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 143A7505 REV:-. LENGTH OF CRACK IS: 0.230? TOOL USED ELECTRONIC CALIPER P/N:500-196-30 S/N:A23048326 DUE DATE: 05-JUN-25;[02] REPLACED ANGLE LOCATED FWD FACE BS 500H AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 143A7505 REV:-. LENGTH OF CRACK IS: 0.230? TOOL USED ELECTRONIC CALIPER P/N:500-196-30 S/N:A23048326 DUE DATE: 05-JUN-25

Part: LIGHT — BROKEN (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

BROKEN PHOTOLUMINESCENT STRIP AT PASSENGER CABIN RH SIDE (6EA) 2024-600453<[01] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN RH SIDE (6EA) IAW B737-800 AMM 33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN RH SIDE (6EA) IAW B737-800 AMM 33-51-15-400-802

Part: LIGHT — BROKEN (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

BROKEN PHOTOLUMINESCENT STRIP AT PASSENGER CABIN LH SIDE (6EA) 2024-600452<[01] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN LH SIDE (6EA) IAW B737-800 AMM 33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN LH SIDE (6EA) IAW B737-800 AMM 33-51-15-400-802

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

CORROSION ON SUPPORT ANGLE LOCATED BS 500I BTW STR 26L TO STR 26R WL 156.1 AT FWD CARGO COMPARTMENT 2024-600468<[01] REPLACED SUPPORT ANGLE LOCATED BS 500I BTW STR 26L TO STR 26R WL 156.1 AT FWD CARGO COMPARTMENT I.A.W B737-800 SRM 51-40-02-0G-0 AND DWG# 143A7902; SHEET 257; REV.B.;[02] REPLACED SUPPORT ANGLE LOCATED BS 500I BTW STR 26L TO STR 26R WL 156.1 AT FWD CARGO COMPARTMENT I.A.W B737-800 SRM 51-40-02-0G-0 AND DWG# 143A7902; SHEET 257; REV.B.

Part: BRACKET — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK BODY STATION 540 BRACKET LBL 6 AT AIR CONDITIONING BAY 2024-600474<[01] REPLACED BRACKET ON BODY STATION 540 AT AIR CONDITIONING BAY IAW B737-800 SRM 51-40-02-0G.;[02] CORRECTED STEP 1. REPLACED BRACKET ON BODY STATION 540 AT AIR CONDITIONING BAY IAW B737-800 SRM 51-40-02-0G AND DWG 212A1101 SHEET 1. REV A.;[03] CERTIFIED ITEM 2

Part: ANGLE — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK INDICATION FOUND ON TWO HOLES OF ANGLE LOCATED ON BS294.5 RBL54 AND WL208.1 AT FWD GALLE AREA 2024-600445<[01] REPLACED ANGLE LOCATED ON BS294.5 RBL54 AND WL208.1 AT FWD GALLEY AREA I.A.W B737-800 SRM 51-40-02 AND DWG: 141A8310 REV: -. SHEET 33;[02] REPLACED ANGLE LOCATED ON BS294.5 RBL54 AND WL208.1 AT FWD GALLEY AREA I.A.W B737-800 SRM 51-40-02 AND DWG: 141A8310 REV: -. SHEET 33<BR>RII

Part: ANGLE — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CRACK INDICATION FOUND ON TWO HOLES OF INNER CHORD LOCATED ON BS294.5 RBL52 AND WL208.1 AT FWD GALLE AREA 2024-600444<[01] REPLACED INNER CHORD LOCATED BETWEEN BS 259 TO BS 360 AND RBL52 WL208.1 AT FWD GALLEY AREA. IAW B737-800 SRM 51-40-02 AND DWG: 141A8310 REV: -. SHEET 33<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED INNER CHORD LOCATED BETWEEN BS 259 TO BS 360 AND RBL52 WL208.1 AT FWD GALLEY AREA. IAW B737-800 SRM 51-40-02 AND DWG: 141A8310 REV: -. SHEET 33<BR>RII<BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 38,276 hrs · 18,139 cycles

CRACK ON BLADE OF ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER 2024-600434<[01] REPLACED BLADE OF ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02.;[02] REPLACED BLADE OF ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA380 TO STA400 AND LBL14 AT PASSENGER CABIN 2024-600422<[01] REPLACED ANGLE LOCATED ON FLOOR STRUCTURE BETWEEN STA 380 TO STA 400 AND LBL 14 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 143A5400 SHEETS: 138 AND 142; REV: -; SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: BALANCE WEIGHT — OUT OF BALANCE (ZONE 300) · airframe 38,276 hrs · 18,139 cycles

DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR LT PN:183A0103-25 SN:006176 FOUND BALANCE WEIGHTS PN:183A0210-15 (1 EA) ON BAY 4 PN:183A0210-14 (1 EA) ON BAY 3 PN:183A0210-14 (1 EA) ON BAY 2 2024-600394<[01] ACCOMPLISHED ELEVATOR BALANCING IAW EA M-22-155-03766.;[02] ACCOMPLISHED ELEVATOR BALANCING IAW EA M-22-155-03766.<BR>RII CERTIFIED

Part: SEAL PLATE — CRACKED (ZONE 400) · airframe 38,276 hrs · 18,139 cycles

CRACK ON SEAL PLATE ACCESS PANEL 431AL LOC. #1 ENGINE. 2024-600415<[01] REPLACED SEAL PLATE ACCESS PANEL 431AL LOC. #1 ENGINE. IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.;[02] REPLACED SEAL PLATE ACCESS PANEL 431AL LOC. #1 ENGINE. IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.

Part: SEAL PLATE — CRACKED (ZONE 400) · airframe 38,276 hrs · 18,139 cycles

CRACK ON SEAL PLATE ON ACCESS PANEL 431AR LOC. ON # 1 ENGINE. 2024-600412<[01] REPLACED SEAL PLATE ACCESS PANEL 431 AR LOCATED ON #1 ENGINE IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] COMPLETED JOB

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

CRACK WEB INTERCOSTAL LOCATED BETWEEN STA344 TO STA360 AND LBL11 FWD GALLEY AND LAV 2024-600315<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS344 TO BS360 LBL11 AT FWD GALLEY AREA I.A.W. B737-800 SRM 51-40-02 AND DWG 141A5400 SHEET 46 REV. A AND SHEET 16 REV. B<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: LENS — BROKEN (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

BROKEN GALLEY 1 EMERGENCY EXIT COVER LENS AT FWD GALLEY AREA 2024-600316<[01] REPLACED GALLEY 1 EMERGENCY EXIT COVER LENS AT FWD GALLEY AREA I.A.W. B737-800 AMM-33-51-01-960-801 STEP 2 C. (4);[02] CERTIFIED WORK PERFORMED

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

CRACK INNER CHORD LOCATED STA303.9 AND LBL55 FWD GALLEY AND LAV 2024-600307<[01] REPLACED INNER CHORD AND FASTENERS LOCATED STA259.5 TO STA360 AND LBL55 FWD GALLEY AND LAV IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A8110 SHEET 9; 10 AND 11; REV-.<BR>SEE INDIVIDUAL SIG-OFF BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIG-OFF BELOW.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

CRACK FLOOR BEAM LOCATED STA294.5 AND RBL52 AT FWD GALLEY AREA 2024-600354<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 7 AND STEP 8;[02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 23-JAN-25. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 23-JAN-25.;[03] ON STEP 12; TOOL USED P/N: XRP-3000; S/N: 1998072; CAL DUE: 23-JAN-25.;[04] PERFORMED PERMANENT REPAIR ON FLOOR BEAM STA294.5 BETWEEN RBL15 TO RBL60 AT FWD GALLEY AREA I.A.W B737-800 B737-800 SRM 53-10-51-2R-16 REPAIR 16. <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[05] PERFORMED PERMANENT REPAIR ON FLOOR BEAM STA294.5 BETWEEN RBL15 TO RBL60 AT FWD GALLEY AREA I.A.W B737-800 B737-800 SRM 53-10-51-2R-16 REPAIR 16.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW AS RII

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

CRACK WEB INTERCOSTAL LOCATED BETWEEN STA277 TO STA294.5 AND BL0 FWD GALLEY AND LAV 2024-600309<[01] REPLACED WEB INTERCOSTAL LOCATED BETWEEN STA277 TO STA294.5 AND BL0 FWD GALLEY AND LAV AND FASTENERS IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 20; REV-.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED WEB INTERCOSTAL LOCATED BETWEEN STA277 TO STA294.5 AND BL0 FWD GALLEY AND LAV AND FASTENERS IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 20; REV-.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.

Part: LENS — MISSING (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

MISSING EMERGENCY LIGHT LENS ROW 6RH AT PASSENGER CABIN 2024-600234<[01] INSTALLED EMERGENCY LIGHT LENS ROW 6RH AT PASSENGER CABIN I.A.W. B737-800 AMM 33-51-03-960-803 STEP 4. D.(2).;[02] INSTALLED EMERGENCY LIGHT LENS ROW 6RH AT PASSENGER CABIN I.A.W. B737-800 AMM 33-51-03-960-803 STEP 4. D.(2).

Part: LENS — CRACKED (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

CRACK EMERGENCY LIGHT LENS ON CEILING PANEL ROW 16 AT PASSENGER CABIN 2024-600238<[01] REPLACED EMERGENCY LIGHT LENS ON CEILING PANEL ROW 16 AT PASSENGER CABIN I.A.W. B737-800 AMM 33-51-03-960-803 STEP 4. D.(1) AND (2).;[02] COMPLETED

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

CRACK FLOOR STRUCTURE SUPPORT ANGLE LOCATED BS540 AND LBL 2 AT PASSENGER CABIN 2024-600249<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATED BS540<BR>AND LBL2 AT PASSENGER CABIN AND FASTENERS I.A.W B737-<BR>800 SRM 51-10-02 STEP 9 AND DWG: 143A0060 SHEET: 64 REV: - SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1: REPLACED ANGLE FLOOR STRUCTURE LOCATED BS540 AND BL0 TO LBL24.75 AT PASSENGER CABIN AND FASTENERS I.A.W B737-800 SRM 51-10-02 STEP 9 AND DWG: 143A0060 SHEET: 64 REV: - SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED ANGLE FLOOR STRUCTURE LOCATED BS540 AND BL0 TO LBL24.75 AT PASSENGER CABIN AND FASTENERS I.A.W B737-800 SRM 51-10-02 STEP 9 AND DWG: 143A0060 SHEET: 64 REV: - SEE INDIVIDUAL SIGN OFF BELOW

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

CRACK FLOOR STRUCTURE SUPPORT ANGLE LOCATED BS540 AND RBL 2 AT PASSENGER CABIN 2024-600250<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATED STA540<BR>AND RBL2 AT PASSENGER CABIN AND FASTENERS I.A.W B737-<BR>800 SRM 51-10-02 STEP 9 AND DWG: 143A0060 SHEET: 64 REV: - SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1: REPLACED ANGLE FLOOR STRUCTURE LOCATED STA540 AND RBL2 AT PASSENGER CABIN AND FASTENERS I.A.W B737-800 SRM 51-10-02 STEP 9 AND DWG: 143A0060 SHEET: 64 REV: - SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 2: REPLACED ANGLE FLOOR STRUCTURE LOCATED STA540 AND BL0 TO RBL24.75 AT PASSENGER CABIN AND FASTENERS I.A.W B737-800 SRM 51-10-02 STEP 9 AND DWG: 143A0060 SHEET: 64 REV: - SEE INDIVIDUAL SIGN OFF BELOW;[04] REPLACED ANGLE FLOOR STRUCTURE LOCATED STA540 AND BL0 TO RBL24.75 AT PASSENGER CABIN AND FASTENERS I.A.W B737-800 SRM 51-10-02 STEP 9 AND DWG: 143A0060 SHEET: 64 REV: - SEE INDIVIDUAL SIGN OFF BELOW

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 38,276 hrs · 18,139 cycles

CUSTOMER REQUEST-CRACK ON VAPOR VARRIER LOCATED LBL 27 AT BS663.75 AT MAIN WHEEL WELL COMPARTME 2024-600226<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: A18229508; DUE DATE: 14-JAN-25.;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18196126; DUE DATE: 03-APR-25.;[03] TOOL USED SPX222; S/N: C410738989; DUE DATE: 05-AUG-25.;[04] CORRECTIVE ACTION 3 ENTER BY ERROR THE CORRECT IS: TOOL USED SCALE P/N: SPX222; S/N: C410738989; DUE DATE: 05-AUG-25.;[05] TOOL USED: HOTBONDER: P/N:HCS9200B-AV S/N:18185733 DUE DATE:25-JAN-25.;[06] TOOL USED: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 650; S/N: 190859705; CAL DUE DATE: 23-OCT-24;[07] REPAIRED VAPOR BARRIER LOCATED LBL 27 AT BS663.75 AT MAIN WHEEL WELL COMPARTMENT IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW.;[08] REPAIRED VAPOR BARRIER LOCATED LBL 27 AT BS663.75 AT MAIN WHEEL WELL COMPARTMENT IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW. RII COMPLETED.

Part: ACCESS PANEL — DAMAGED (ZONE 500) · airframe 38,276 hrs · 18,139 cycles

ELONGATED HOLES ACCESS PANEL 561CB AT LT WING 2024-600149<[01] TOOL USED: CALIPER PN:500-196-30 SN:A22348594 DUE DATE:23-JUL-25.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N:18175478 DUE DATE: 25/JAN/25.;[03] TOOL USED SCALE P/N: CR5200 S/N: 8343110809 DUE DATE: 28 FEB 25.;[04] TOOL USED: MICROBONDER P/N: HCS8800 S/N: 01112546 DUE DATE: 25/JAN/25;[05] TOOL USED: SCALE P/N: CR5200 S/N: 8343110809 DUE DATE: 28/FEB/25.;[06] TOOL USED HOT BONDER PN: HCS9200B-AV SN: 18175478 DUE DATE: 25/JAN/25.;[07] TOOL USED: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 650; S/N: 190859705; CAL DUE DATE: 23-OCT-24;[08] TOOL USED: MULTIMETER P/N: FLUKE 87; S/N: 37640185; DUE DATE: 24-JAN-25. TOOL USED HUMIDITY/TEMPERATURE CHART RECORDER P/N: RH550; S/N: 240531238 ; DUE DATE: 10-SEP-25.;[09] REPAIRED ACCESS PANEL 561CB AT LT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW.;[10] REPAIRED ACCESS PANEL 561CB AT LT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10.

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 38,276 hrs · 18,139 cycles

INOP MEGAPHONE FWD GALLEY 7 AT FWD GALLEY AREA 2024-600163<[01] REPLACED MEGAPHONE FWD GALLEY 7 AT FWD GALLEY AREA I.A.W. SWA JOB CARD 725-031-00-05Y SEE TTG8R007MMZY STEP 2. A (1) ITEM (F).;[02] REPLACED MEGAPHONE FWD GALLEY 7 AT FWD GALLEY AREA I.A.W. SWA JOB CARD 725-031-00-05Y SEE TTG8R007MMZY STEP 2. A (1) ITEM (F).

Part: ACCESS PANEL — DELAMINATED (ZONE 500) · airframe 38,276 hrs · 18,139 cycles

DELAMINATED ACCESS PANEL 561AB LT WING 2024-600147<[01] TOOL USED: CALIPER PN:500-196-30 SN:A22348594 DUE DATE:23-JUL-25;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N:18175478 DUE DATE: 25/JAN/25.;[03] TOOL USED SCALE P/N: CR5200 S/N: 8343110809 DUE DATE: 28 FEB 25.;[04] TOOL USED: MICROBONDER P/N: HCS8800 S/N: 01112546 DUE DATE: 25/JAN/25.;[05] TOOL USED: SCALE P/N: CR5200 S/N: 8343110809 DUE DATE: 28/FEB/25.;[06] TOOL USED HOT BONDER PN: HCS9200B-AV SN: 18175478 DUE DATE: 25/JAN/25.;[07] TOOL USED: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 650; S/N: 190859705; CAL DUE DATE: 23-OCT-24;[08] TOOL USED: MULTIMETER P/N: FLUKE 87; S/N: 37640185; DUE DATE: 24-JAN-25. TOOL USED HUMIDITY/TEMPERATURE CHART RECORDER P/N: RH550; S/N: 240531238 ; DUE DATE: 10-SEP-25.;[09] REPAIRED ACCESS PANEL 561AB LT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW.;[10] REPAIRED ACCESS PANEL 561AB LT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10.

Part: DOUBLER — CRACKED (EXTER POWER BOX) · airframe 37,138 hrs · 17,543 cycles

EXTERNAL POWER DOOR FRAME DOUBLER LOOSE/BROKEN<[01] PERFORMED EA 24-153-01378

Part: ENGINE — LEAKING (NR 2) · airframe 35,774 hrs · 16,827 cycles

DURING CRUISE FLIGHT @ FL390 THE WHITE BOX APPEARED ON THE ENGINE DISPLAY AND #2 OIL QTY INDICATED 18%. OIL PRESS AND OIL TEMP NORMAL. OIL QUANTITY CONTINUED TO DECREASE TO 0%. WITHIN ABOUT 5 MINUTES OIL PRESSURE BEGAN TO FALL AND BEGAN INDICATING YELLOW AND RED. WE PERFORMED AN ENGINE SHUTDOWN AND DIVERTED TO ATL. NORMAL UNDERWEIGHT LANDING AND NO BRAKE TEMPERATURE ISSUES NOTED IN PWB BRAKE COOLING MODULE. NORMAL TAXI TO GATE. (REF DFDR DOWNLOAD TTG8Q00QGYTH - THE ENGINE WAS COMMANDED TO SHUTDOWN AT AN OIL PRESSURE OF 16PSI WHICH IS WITHIN LIMITS OF AMM 71-00-00-210-037-F00)<[01] INSPECTED #2 ENGINE FOUND STARTER CLAMP BROKEN AND OIL QTY LOW; ACCOMPLISHED FDR DOWNLOAD ENGINEERING WAS SATISFIED WITH FINDINGS; REPLACED STARTER AND CLAMP REF AMM 80-11-01AND ACCOMPLISHED POWER ASSURANCE REF AMM 71-00-00 ALL OPS AND LEAK CHECK WERE GOOD; REF TTG8Q00NS8CS; TTG8Q00QGZGM; TTG8Q00QH190 CHIP DETECTORS ALSO GOOD ATTACHED PICTURES AND ACCOMPLISHED MCD TASK 779-00-00

Part: GIRT BAR — LOOSE (ZN 200 FUS TOP) · airframe 34,467 hrs · 16,113 cycles

FWD SERVICE DOOR RIGHT GIRT BAR BRACKET LOOSE<[01] INSTALLED RIVET ON FWD SERVICE DOOR RIGHT GIRT BAR PER SRM 51-40-02;[02] INSTALLED RIVET ON FWD SERVICE DOOR RIGHT GIRT BAR BRACKET PER SRM 51-40-02

Part: SIGN — DETACHED (ZN 200 FUS TOP) · airframe 34,159 hrs · 15,938 cycles

CAS SIDE EXIT ROW SIGN DETACHED<[01] REINSTALLED CA?S SIDE FWD EMERGENCY EXIT OVERWING LIGHT LENS PER MM 33-51-01

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 32,471 hrs · 14,998 cycles

EXIT LIGHT COVER MISSING IN AFT GALLEY, LEFT SIDE ON AFT BULKHEAD. INSTALLED EXIT LIGHT LENS IAW AMM 33-51-01.

Part: NONE — DAMAGED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

FWD CABIN FLOOR PHOTOLUMINESCENT LIGHT END CAP WORN . / [01] R&R FWD CABIN FLOOR PHOTO LUMINESCENT END CAP PER AMM 33-51-15.

Part: NONE — DELAMINATED (RH HOR STAB) · airframe 31,667 hrs · 14,563 cycles

L/H HORIZONAL STAB TIP FAIRING HAS DELAMINATION ON UPPER SURFACE. / [01] REPLACED HORZ L/E TIP REF MM 27-41-21;[02] VERIFIED REPLACED HORZ L/E TIP REF MM 27-41-21;[03] CW

Part: NONE — CUT (RH HOR STAB) · airframe 31,667 hrs · 14,563 cycles

RIGHT HORIZONTAL UPPER FORWARD SLIDER SEAL IS CUT; SHEARED IN FORWARD TRACK. / [01] REMOVED AND REPLACED R/H UPPER FWD SLIDING SEAL PER AMM 53-31-31;[02] RII: INSPECTED THE WORK PERFORMED ON C/A #1; THE REMOVAL AND REPLACEMENT OF THE R/H UPPER FWD SLIDING SEAL PER AMM 53-31-31. NO DEFECTS NOTED.

Part: NONE — CUT (LH HOR STAB) · airframe 31,667 hrs · 14,563 cycles

LEFT HORIZONTAL UPPER FORWARD SLIDER SEAL IS CUT; SHEARED AT FORWARD TRACK. / [01] INSTALLED ATTACH BRACKET WITH FASTENERS PER SRM 51-40-02.;[02] 1. DANIEL ANDERSON (TECHNICIAN); 21-SEP-2022 08:02 UTC<BR>INSTALLED ATTACH BRACKET WITH FASTENERS PER SRM 51-40-02.<BR>C/W INSPECTION.;[03] PARTS DATA UPDATE ONLY;[04] PARTS DATA UPDATE ONLY;[05] INSTALLED CLOSEOUT PANEL 331AB PER SRM 51-40-02;[06] REMOVED AND REPLACED LEFT HORIZONTAL UPPER FORWARD SLIDER SEAL PER AMM 53-31-31;[07] C/W

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

CABIN FLOOR PANEL 232SF HAS DENTS AND DELAMINATION. / [01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.;[02] PARTS INFO

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

CABIN FLOOR PANEL 242CF HAS DENTS AND DELAMINATION. / [01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.;[02] PARTS INFO

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

CABIN FLOOR PANEL 231YF HAS DENTS AND DELAMINATION. / [01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

CABIN FLOOR PANEL 232RF HAS DENTS AND DELAMINATION. / [01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.;[02] PARTS INFO

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

CABIN FLOOR PANEL 242DF HAS DENTS AND DELAMINATION. / [01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.;[02] PARTS INFO

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

CABIN FLOOR PANEL 241FF HAS DENTS AND DELAMINATION. / [01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.;[02] PARTS INFO

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

CABIN FLOOR PANEL 241BF HAS DENTS AND DELAMINATION. / [01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.;[02] PARTS INFO

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

CABIN FLOOR PANEL 242AF HAS DENTS AND DELAMINATION. / [01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.;[02] PARTS INFO

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

CABIN FLOOR PANEL 241AF HAS DENTS AND DELAMINATION. / [01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.;[02] PARTS INFO

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

CABIN FLOOR PANEL 231ZF HAS DENTS AND DELAMINATION. / [01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.;[02] PARTS INFO

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

CABIN FLOOR PANEL 241DF HAS DENTS AND DELAMINATION. / [01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.;[02] PARTS INFO

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

CABIN FLOOR PANEL 242BF HAS DENTS AND DELAMINATION. / [01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

CABIN FLOOR PANEL 231XF HAS DENTS AND DELAMINATION. / [01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.;[02] PARTS INFO;[03] PARTS INFO

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 31,667 hrs · 14,563 cycles

CABIN FLOOR PANEL 241CF HAS DENTS AND DELAMINATION. / [01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.;[02] PARTS INFO

Part: NONE — CRACKED (LH WING) · airframe 31,667 hrs · 14,563 cycles

LT WING T/E WIGGLE PLATE CRACKED INBD OF #3 FLAP TRACK [MARKED]. / [01] REMOVED AND REPLACED DAMAGED WIGGLE PLATE PER SRM 51-40-02.;[02] PARTS DATA UPDATE ONLY;[03] RESTORED EXTERIOR PAINT FINISH PER AMM 51-21-99.;[04] C/W INSPECTION.

Part: BATTERY PACK — INOPERATIVE (R/H OVERWING) · airframe 30,988 hrs · 14,194 cycles

R/H OVERWING AFT EMERGENCY LIGHT INOP / [01] REMOVED AND REPLACED BATTERY PACK AND PACK CHARGER AT STA 727C RH IAW AMM 33-51-06 OPS CHECK GOOD

Part: COVER — MISSING (R/H CABIN) · airframe 30,988 hrs · 14,194 cycles

EMERGENCY LIGHT LENS COVER MISSING AT 10DEF / [01] REPLACED COVER PER AMM33-51-03.

Part: SWITCHPACK — FAULTY (#2 ENGINE) · airframe 30,293 hrs · 13,830 cycles

#2 ENG THRUST REVERSER SLOW TO DEPLOY. #2 THRUST REVERSER LIGHT ILLUMINATED. 09APR EMAIL SENT REQUESTING FIELD TECH SUPPORT F/C AT TIME OF DEFERRAL LH SLEVE STOW SENSOR S831***SCHD 04/10 MCO***3-21 OPS CK GOOD 3-29 R/R #2 ENG LH T/R SYNC LOCK 4-9 R&R T/RSLEEVE STOW SENSOR S831 AWLAYS BEEN SAME FAULT CODE4-9 OPS CK GOOD******4/10: ATL HAS A FIELD TECH AVAILABLE TONIGHT DO NOT CARRY OVER MEL WITHOUT RUSS HILLMAN OR TEAM LEAD APPROVAL ***********PRIOR TO R/R HARNESS PLEASE RING OUT AND VERIFY RECENTLY INSTALLED SENSOR ASSY FAULTY - MOC / [01] COMPLIED WITH EAU BITE; FOUND FAULT CODE LEFT SLEEVE STOW SENSOR FAULT S831. OK TO CONTINUE PER MEL 78-1-01. SP# 1 SP# 1A SP#78. AIRCRAFT DOWNGRADED TO CAT I STATUS.;[02] REMOVED AND REPLACED RIGHT AUTOTHROTTLE SWITCH PACK ASSY. IAW AMM 76-11-07. OP?S CHECK GOOD. EV.# E011214.<BR>AIRCRAFT RECERTIFIED TO CAT III STATUS PER MT 734-00-03. <BR>VERIFICATION # 28484. E71883.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 30,163 hrs · 13,753 cycles

EMERGENCY EXIT LIGHTS INOP OVER LH AND RH OVER WING EXIT DOORS. / [01] REMOVED AND REPLACED M1695(RH OVER WING EXIT) BATTERY PACK AND CHARGER. IAW AMM 33-51-06. REMOVED AND REPLACED M1694(LH OVER WING EXIT) BATTERY PACK. IAW AMM 33-51-06. EMERGENCY EXIT LIGHT SYSTEM OPS CHECK GOOD IAW AMM 33-51-00.

Part: NONE — STUCK (E&E BAY) · airframe 30,067 hrs · 13,712 cycles

ON APPROACH FLAPS STUCK SYMMETRICALLY AT 2 WITH FLAP HANDLE AT 5. USED ALT FLAP EXTENSION TO LAND AT FLAPS 15. / [01] PERFORMED FIM 27-51 TASK 836. BITE MSG 27-53279(L28VAC EXC INV). T/S FIM 27-51 TASK 822. VERIFIED 28VAC AT D728B PIN G11 TO D728A PIN F1. WITHIN LIMITS. R+R FSEU AMM 27-51-01. BITE CKS OK GOOD. CHECKED AND CLEANED CONNECTOR FOR D01012 FLAP MOTOR. VERIFIED FLAP TRANSMISSION FLUID NORMAL PER AMM 12-22-51 LEFT WING TRANSMISSIONS. VERIFIED PER FIM 27-51 TASK 849 TRAILING EDGE FLAPS TRANS TRIP INDICATION NOT EXTENDED. RAN FLAPS/SLATS 5 FULL CYCLES. CKS OK.

Part: LIGHT — INOPERATIVE · airframe 29,766 hrs · 13,587 cycles

FOUND MID CABIN EMER BATT M1670 INOP ; / [01] R&R EMER LIGHT BATTERY M1670 IAW AMM 33-51-06.

Part: LENS — BROKEN (CABIN) · airframe 29,169 hrs · 13,317 cycles

LH FWD OW EMERGENCY EXIT SIGN HAS LAMPS INOP AND LENS IS BROKEN ; / [01] RELAMPED AND REPLACE LENS IAW AMM 33-51-01

Part: SKIN — DENTED (BS 967) · airframe 25,873 hrs · 11,594 cycles

DENT ON FUSELAGE SKIN BS 967 +9', 0.5' ABOVE STR 28L DENT MEASURES L=2.55', W=1.95', Y=0.027' W/Y=72. DISCREPANCY TRANSFERRED FROM N/R D166337. DENT FUSELAGE SKIN STA 967 & 9 .5' ABOVE STR 25L. DAMAGE CUTOUT AND REPAIRED, IAW SRM 53-00-01-2R-1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,873 hrs · 11,594 cycles

FWD GALLEY RT EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED BATTERY PACK, PER MM 33-51-06. EMERGENCY LIGHTS OPERATIONS CHECKED GOOD, PER MM 33-51-00P/N OFF D717-01-100 S/N OFF 45832 P/N ON D717-01-100-SWA S/N ON 57388.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,873 hrs · 11,594 cycles

AFT OVERWING RT EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, PER MM 33-51-06. EMERGENCY LIGHTS OPERATIONS CHECKED GOOD, PER MM 33-51-00. P/N OFF D717-01-100 S/N OFF 216952 P/N ON D717-01-100SWA S/N ON 45642.

Part: STRAP — CORRODED (AFT CARGO) · airframe 25,873 hrs · 11,594 cycles

PER PRODUCTION REQUEST-AFT CARGO #4 FLOOR STRAP HAS CORROSION. AT THE FASTENER HOLE. / R&R FLOOR STRAP PART # 146A9401-4 PER SRM 51-40-02. TO BE INSTALLED ON SAM 565S

Part: BRACKET — CRACKED (BS 500H RBL 24) · airframe 25,873 hrs · 11,594 cycles

FORWARD CARGO; INTERCOSTAL ATTACH BRACKET/CLIP CRACKED AT FWD SIDE OF STA 500H; RBL 24' JUST ABOVE STR 26R AREA MARKED / REMOVED AND REPLACED FWD CARGO INTERCOSTAL ATTACH BRACKET/CLIP AT FWD SIDE OF STA. 500H; RBL 24' JUST ABOVE STR. 26R PER SRM 51-40-02.

Part: ATTACH BRACKET — CRACKED (BS 500H ROB 24) · airframe 25,873 hrs · 11,594 cycles

FORWARD CARGO; INTERCOSTAL ATTACH BRACKET/CLIP CRACKED AT STA 500H; RBL 24' KIST ABPVE STR 26R AREA MARKED / REMOVED AND REPLACED INTERCOSTAL ATTACH BRACKET AFT SIDE OF STA. 500H; RBL 24 (MARKED) PER SRM 51-40-02 (SA-M 326 ATTACHED: A1200820)

Part: ANGLE — DAMAGED (BS 420) · airframe 25,873 hrs · 11,594 cycles

FWD CARGO LT TRANS ANGLE DAMAGED AT STA 420 + 5'. REMOVED, FABRICATED, AND REPLACED FWD CARGO LT TRANSITION ANGLE AT STA 400+13 TO STA 440+9, IAW SRM 53-00-53-2R-5.

Part: SKIN — DENTED (BS 996.5) · airframe 25,873 hrs · 11,594 cycles

DENT ON RT FUSELAGE SKIN AT APPROXIMATELY STA 996.5, 3.5' BELOW STR 21R, L=2.7', W=2.3' AND .90' DEEP W/Y=25.5. REWRITTEN FROM DEFECT NR 8419. THIS N/R WRITTEN TO DOCUMENT PERMANENT REPAIR. REPAIRED DENT ON RT FUSE SKIN AT APPROXIMATELY STA 996.5; 3.5' BELOW STR 21R, PER SRM 53-00-01-2R-3. SEE SAM 326 FOR INDIVIDUAL WORK ACCOMPLISHED (SA-M 326 A1200782).

Part: GUSSET — CRACKED (BS 500I S19R) · airframe 25,873 hrs · 11,594 cycles

FWD CARGO GUSSET CRACKED BS 500 I STR 19R / REMOVED AND REPLACED FWD CARGO GUSSET AT BS .500I; STR 19R PER SRM 51-40-02. APPLIED CORROSION INHIBITING COMPOUND TO REPAIR AREA PER SOPM 20-41-05. SEE SA-M 326 FOR INDIVIDUAL WORK ACCOMPLISHED.SA-M 326 A1184510 INSP BY E49332

Part: SKIN — DAMAGED (BS 277) · airframe 25,873 hrs · 11,594 cycles

FUSELAGE SKIN AT STA 277+6 BETWEEN STR 1 AND 2 HAS DAMAGE FROM FWD LAV DOOR HINGE PIN MIGRATION, AS PER SA-M 735 ROY DENBOW E13421. FUSELAGE SKIN AT STA 277 + 6 BETWEEN STR 2L AND STR 3L HAS DAMAGE FROM LAV DOOR HINGE MIGRATION. REMOVED DAMAGE, ACCOMPLISHED HFEC HOLE PROBE, STEPPED HOLE TO .187'. INSTALLED REPAIR RIVET PROTRUDING HEAD, APPLIED CHEMICAL CONVERSION AND RESTORED EXTERIOR FINISH. ALL WORK COOMPLISHED IS A CATEGORY A REPAIR, PER SRM 53-00-01-2R-38.SA-M 326 S/N A1184506.

Part: FLOOR SUPPORT — CORRODED (BS 787-827) · airframe 25,873 hrs · 11,594 cycles

CORROSION ON FLOOR BEAM BS 787+10 - BS 827 RBL 14 AFT CARGO RBL-14. REMOVED AND REPLACED SECTION FLOOR TRACK FROM STA 757-887, PER SRM 53-00-53-2R-3 AND EA 20-153-01854 P/N 146A7501-41 (SA-M 326 A1200804).

Part: ANGLE — CORRODED (BS 500E-500F) · airframe 25,873 hrs · 11,594 cycles

FWD CARGO LH TRANS ANGLE HAS CORROSION STA 500 E TO 500 F / REMOVED CORR. L/H TRANSITION ANGLE PER SRM 51-10-02 MATERIAL FOUND OUT OF LIMITS PER SRM 53-00-53-1A-0 REPLACED SECTION TRANSITION ANGLE FROM STA 500D + 9 TO STA 500I PER SERM 51-10-02 ; 53-00-53-2R-5 TRANS ANGLE P/N 143A7501-188 (S/N A1200806)

Part: STRINGER CLIP — CRACKED (BS 500I) · airframe 25,873 hrs · 11,594 cycles

FWD CARGO STA 500I STRINGER 26R STRINGER CLIP CRACKED. REMOVED AND REPLACED DAMAGED STRINGER CLIP, PER EA 20-153-01929 PART 1. STR CLIP P/N 143A75020158 (SA-M 326 ATTACHED: A1200821).

Part: WEB — CORRODED (CARGO THRESHOLD) · airframe 25,873 hrs · 11,594 cycles

FWD CARGO DOOR THRESHOLD WEB AREA STA 440 THRU STA 493 HAS LIGHT CORROSION ACCESS MARKED / REMOVED AND REPLAED FWC CARGO DOOR THRESHOLD WAD AT STA 440 THRU STA 493 PER SRM 51-40-02. SEE SAM -326 ATTACHED: A1184504 INSTALLED PART NUMBER 143A8122Y10

Part: FLOOR PANEL — CORRODED (BS 947) · airframe 25,873 hrs · 11,594 cycles

CORROSION AROUND FLOOR PANLE ATTACH HOLE STA 947 LBL 53 MARKED. REPAIRED PER EA 20-153-01821 (S/N A1200784).

Part: TIE DOWN — CORRODED (BS 948) · airframe 25,873 hrs · 11,594 cycles

'D' LAV AFT OUTBOARD TIE DOWN FITTING HAS CORROSION AT BASE STA 948 LBL49 / DAMAGE LIMITED TO INTERCOSTAL STA LBL49. FOUND TO BE OUT OFF LIMITS PER 53-70-51. LOCATED AND DRILLED NEW INTERCOSTAL P/N 147A5660Y21; PER SRM 51-40-05. INSTALLED NEW INTERCOSTAL PER SRM 5140-02.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 25,873 hrs · 11,594 cycles

CORROSION BETWEEN STA 947 FLOOR BEAM AND INTERCOSTAL AT LBL 51. REPAIRED, PER EA 20-153-01821. SEE INDIVIDUAL SIGNOFFS ON SAM 326 947 FLOOR BEAM P/N 17A5504-7SEE SA-M 326 A1200769.

Part: SKATE ANGLE — DAMAGED (BS 1016) · airframe 25,873 hrs · 11,594 cycles

R/H SKATE ANGLE STARTING AT B.S 1016 HAS WEAR DAMAGE ON INBOARD AND OUTBOARD SURFACES ( FWD SKATE ANGLE ) / REMOVED AND REPLACED R/H FWD SKATE ANGLE PER SRM 51-40-02

Part: SKATE ANGLE — DAMAGED (BS 1016) · airframe 25,873 hrs · 11,594 cycles

L/H SKATE ANGLE AT STA. 1016 HAS WEAR DAMAGE ON INBOARD AND OUTBOARD SURFACES ( FWD SKATE ANGLE) / REMOVED AND REPLACED L/H FWD SKATE ANGLER PER ARM 51-40-02

Part: MOUNT — CORRODED (LAVATORY) · airframe 25,873 hrs · 11,594 cycles

'E' LAV AFT OUTBOARD TIE DOWN FITTING HAS CORROSION AT STA 950 RBL 50' MARKED / REMOVED AFT OUTBD LAV MOUNT FOR EVALUATION (NO CORROSION NOTED ON LAV MOUNT); CORROSION LIMITED TO INTERCOASTAL RBL 50 STA. 947 TO 967 P/N 147A5660-22 OUT OF LIMITS PER SRM 53-70-51-1A-1 REMOVED AND REPLACED DAMAGE INTERCOSTAL PER SRM 51-40-02 INSTALLED AFT OUTBD LAV MOUNT PER SRM 51-40-02SA-M 326 S/N A1200771

Part: MOUNT — CORRODED (R2 DOOR GIRT BAR) · airframe 25,873 hrs · 11,594 cycles

AFT SERVICE DOOR; AFT GIRT BAR MOUNT HOLE AT STA 986.5 AND RBL 43 HAS CORROSION / REPAIRED IAW SRM 53-70-51-2R-6 REPAIR 6 SEE ATTACHED SAM 326 FOR INDIVIDUAL WORK STEP ACCOMPLISHEMENTS (S/N A1200770)

Part: MOUNT — CORRODED (BS 947) · airframe 25,873 hrs · 11,594 cycles

CORROSION UNDER LAV MOUNT AT STA 947 AT RBL 51. REPAIRED PER EA 20-153-01838 AND SRM 53-70-51-2R-8 ALT 1. SEE INDIVIDUAL SIGNOFF'S ON SAM-326 ATTACHED (S/N A1200783).

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 25,873 hrs · 11,594 cycles

LEFT WING AFT FLAP INBOARD AND DELAMED. / REMOVED & REPLACED AFT FLAP PER M/M 27-51-22POS L/H TAG 714506 PN OFF 113A3700-25 SN OFF 113A3700-23 SN OFF 004300 SN ON 001845

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 25,859 hrs · 11,584 cycles

RH HORIZONTAL STAB UPPER FWD SLIDING SEAL CRACKED / R&R RH HORIZONTAL STAB UPPER FWD SLIDING SEAL PER AMM 53-31-31INSP 43450

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 25,324 hrs · 11,169 cycles

PHOTO LUMINESCENT TRACK LIGHTING AT ROWS 1 THRU 4 RIGHT SIDE NOT ILLUMINATE OR GLOW AND IS CRACK AT AFT END OF TRACK. REPLACED PHOTO LUMINESCENT STRIP AT ROWS 1-4 ON RIGHT SIDE DEF REF AMM 33-51-15 OK FOR SERVICE.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 25,323 hrs · 11,168 cycles

CABIN FLOOR PANEL PN 144A5810-127 HAS FIBERS TORN IN SEVERAL AREAS. DAMAGE ALONG CENTER STRIP MEASURES 84' IN LENGTH. DAMAGE 4' RIGHT OF CENTER HAS LAYER OF FIBERS MISSING 21' LONG. DAMAGE 7.5' RIGHT OF CENTER 15' FWD OF END OF PANEL HAS DAMAGE 9' LONG. OUT OF LIMITS SRM 53-00-50. APPLIED INTERIM SEAL BY APPLYING P280 TAPE IAW REPAIR-53EA-06061, PERMANENT ACTION REQUIRED. REMOVE AND REPLACE PANEL 144A5810-127 OR PERFORM A REPAIR, WITHIN 730 DAYS. REMOVED AND REPLACED FLOOR PANEL REF AMM 53-21-00.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 25,316 hrs · 11,164 cycles

DURING PFC SERVICE FOUND IN FWD CABIN SEVERAL EMERGENCY LIGHTS OUT. TROUBLESHOT PER WDM 33-51-12, FOUND EMERGENCY BATTERY PACK M2335 FAULTY. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW AMM 33-51-06. OPS CHECKS NORMAL, POS FWD PN OFF D717-01-100, SN OFF 215152, PN ON D717-01-100SWA AND SN ON 37287.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 25,228 hrs · 11,122 cycles

FWD EMERGENCY LIGHTS FOR L1 AND R1 DOOR INOP. / R/R BATTERY CHARGERS FOR L1 AND R1 EMERGENCY LIGHTS IAW MM 33-51-06. OPS CHECK; NO HELP. PLEASE SEE LOG PAGE 0200445E FOR CORRECTIVE ACTION

Part: CHARGER — INOPERATIVE (CABIN) · airframe 25,228 hrs · 11,122 cycles

FWD EMERGENCY LIGHTS FOR L1 AND R1 DOOR INOP. / R/R BATTERY CHARGERS FOR L1 AND R1 EMERGENCY LIGHTS IAW MM 33-51-06. OPS CHECK; NO HELP. PLEASE SEE LOG PAGE 0200445E FOR CORRECTIVE ACTION

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 25,142 hrs · 11,053 cycles

AFT ENTRY DOOR ESCAPE SLIDE GIRT REQUIRES ADJUSTMENT / ADJUSTED GIRT PER MT 725-61-06

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,044 hrs · 11,012 cycles

AFT RIGHT EMERGENCY LIGHTS INOP / REMOVED AND REPLACED AFT RIGHT EMERGENCY BATTERY PACK IN REF. TO AMM 33-51-06. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,954 hrs · 10,965 cycles

AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP / RELAMPED AFT ENTRY EXTERIOR EMERGENCY LIGHT REF AMM 33-51-00. OPS CHK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,949 hrs · 10,963 cycles

AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP RELAMPED AFT ENTRY EXTERIOR EMERGENCY LIGHT REF AMM 33-51-00. OPS CHK GOOD.

Part: HOOK — LOOSE (L1 DOOR) · airframe 21,391 hrs · 9,273 cycles

L1 DOOR GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM & MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,678 hrs · 8,960 cycles

L2 DOOR EMERGENCY LIGHTS INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,678 hrs · 8,960 cycles

RT FORWARD CABIN EMERGENCY LIGHTS INOP. R&R BATTERY PACK PER AMM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 20,538 hrs · 8,891 cycles

R1 DOOR GIRT BAR STORAGE HOOKS LOOSE. R&R HOOK PER SRM.

Part: STRIP — CORRODED (FWD CARGO RH) · airframe 20,525 hrs · 8,885 cycles

FWD CARGO COMPARTMENT RH BS 500D- 500I FLOOR CAP STRIP IS CORRODED / REMOVED CORROSION AT FWD CARGO CAP STRIP STA 500D TO 500I R/H IAW SRM 51-10-02-0G-0 STEP 15 100% MATERIAL LOSS. REPLACED FLOOR CAP STRIP IAW DWG# 453A1611 REV C./ SRM 51-40-02-0G-0. TAG# WN9784

Part: NONE — CORRODED (AFT CARGO COMPT) · airframe 20,525 hrs · 8,885 cycles

AFT CARGO COMPARTMENT FRAME FAIL SAFE CORD STA 827 RBL 2 TO RBL 6 HAS CORROSION AS MARKED. / REMOVED CORROSION FROM FAIL SAFE CHORD STA 827 RBL 2-RBL 6 IAW SRM 53-00-07-1A-1; VERIFIED WITH 10X GLASS ORIG T .090' WITH .020' LOSS .070' REMAINING OUT OF LIMITS IAW B737 SRM 53-00-07-1A-1. REPAIRED FAILSAFE CHORD IAW EA 180520 REV P1; P2; AND IR AND SWA W/O # REPAIR-53EA-05755

Part: BRACKET — BROKEN (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

PANEL 551FB HAS BROKEN FWD BRACKET PN#287A9152-23 / REPLACED BRACKET AT PANEL AT 551FB IAW SRM 51-40-02; STEP 4.ATAG #A25698 P/N 287A9152-23

Part: PANEL — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING FUEL TANK ACCESS PANEL 532CB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 532CB AND CLAMP RING FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED LEFT WING FUEL ACCESS PANEL 532CB AND CLAMP RING IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG 2A59 A25674

Part: PLATE — CRACKED (L/H WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING REAR SPAR WIGGLE PLATE PHENOLIC STRIP CRACKED NEAR WING STATION 370. (ABOUT 3 FEET OUTBOARD OF #2 FLAP TRACK) / REMOVED AND REPLACED L/H WING REAR SPAR WIGGLE PLATE NEAR WING STATION 370 IAW SRM 57-40-02-0G-0 STEP 4 AND DWG#115A33760 REV - TAG#Z40101

Part: PANEL — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING FUEL TANK ACCESS PANEL 532JB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON LEFT WING FUEL ACESS PANEL 532JB AND CLAMP RING FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED LEFT WING FUEL ACCESS PANEL 532JB AND CLAMP RING IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG ZA74 A25668

Part: PANEL — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING FUEL TANK ACCESS PANEL 532GB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 532GB AND CLAMP RING FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED LEFT WING FUEL ACCESS PANEL 532GB AND CLAMP RING IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG 2A79 A25670

Part: PANEL — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING FUEL TANK ACCESS PANEL 532DB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 532DB AND CLAMP RING FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED LEFT WING FUEL ACCESS PANEL 532DB AND CLAMP RING IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG 2A65 A25672

Part: PANEL — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING FUEL TANK ACCESS PANEL 532EB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON LEFT WING FUEL TANK 532EB AND CLAMP RING FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED LEFT WING FUEL ACCESS PANEL 532EB AND CLAMP RING IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG WN2442 A25675

Part: PANEL — CORRODED (RIGHT WING) · airframe 20,525 hrs · 8,885 cycles

RIGHT WING FUEL TANK ACCESS PANEL 631BB CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON RIGHT WING FUEL ACCESS PANEL 631BB CLAMP RING REMOVED AND REPLACED RIGHT WING FUEL ACCESS PANEL CLAMP RING 631BB IAW B737 SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 TO BE OUT OF LIMITS ATAG 2A64 A25642

Part: PANEL — CORRODED (RIGHT WING) · airframe 20,525 hrs · 8,885 cycles

RIGHT WING FUEL TANK ACCESS PANEL 632NB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON FUEL ACCESS PANEL AND CLAMP RING 632NB REMOVED AND REPLACED RIGHT WING FUEL ACCESS PANEL AND CLAMP RING 632NB IAW B737 SRM 57-20-0-1A-1 TO BE OUT OF LIMITS ATAG 2A56 A25759

Part: PANEL — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING FUEL TANK ACCESS PANEL 532MB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION LEFT WING FUEL TANK ACCESS PANEL 532MP AND CLAMP RING TO BE OUT OF LIMITS REMOVED AND REPALCED LEFT WING FUEL ACCESS PANEL 532 MP AND CLAMP RING IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG 2A75 A25745

Part: PANEL — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING FUEL TANK ACCESS PANEL 532PB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 532PB AND CLAMP RING FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED LEFT WING FUEL ACCESS PANEL 532PB AND CLAMP RING IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG 2A58 A25739

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 20,525 hrs · 8,885 cycles

FWD CARGO PIT FLOOR 120CF HAS EVIDENCE OF CORROSION AS MARKED. / REPLACED FWD CARGO FLOOR PANEL 120CF IAW B737 SRM 51-10-02; SRM 53-00-53-1A-1 AND B737 AIPC 25-52-10-17 ATAG: ZA0053

Part: PANEL — CORRODED (RIGHT WING) · airframe 20,525 hrs · 8,885 cycles

RIGHT WING FUEL TANK ACCESS PANEL 632CB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON RIGHT WING FUEL ACCESS PANEL AND CLAMP RING 632CB FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED RIGHT WING FUEL ACCESS PANEL AND CLAMP RING 632CB IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG 2A81 A25681

Part: PANEL — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING FUEL TANK ACCESS PANEL 532NB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 532NB AND CLAMP RING FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED LEFT WING FUEL ACCESS PANEL 532NB AND CLAMP RING IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG 2A71 A25746

Part: PANEL — CORRODED (RIGHT WING) · airframe 20,525 hrs · 8,885 cycles

RIGHT WING FUEL TANK ACCESS PANEL 632JB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED CORROSION ON FUEL ACCESS PANEL AND CLAMP RING 632JB IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED FUEL ACCESS PANEL AND CLAMP RING 632JB IAW B737 SRM 57-20-0-1A-1 TO BE OUT OF LIMITS ATAG 2A73 A25650

Part: PANEL — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING FUEL TANK ACCESS PANEL 532KB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 532KB AND CLAMP RING FOUND TO BE OUT OF LIMITS REMOVED AND REPALCED LEFT WING FUEL ACCESS PANEL 532KB AND CLAMP RING IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG 2A70 A25667

Part: PANEL — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING FUEL TANK ACCESS PANEL 532AB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 532AB AND CLAMP RING FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED LEFT WING FUEL ACCESS PANEL 532AB AND CLAMP RING IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG 2A86 A25665

Part: PANEL — CORRODED (RIGHT WING) · airframe 20,525 hrs · 8,885 cycles

RIGHT WING FUEL TANK ACCESS PANEL 632FB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON FUEL ACCESS PANEL 632FB AND CLAMP RING FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED RIGHT HAND WING FUEL ACCESS PANEL AND CLAMP RING 632FB AND CLAMP RING IAW SRM B737 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG WN9187 A25644

Part: PANEL — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING FUEL TANK ACCESS PANEL 532QB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 532QB AND CLAMP RING FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED L/H WING FUEL ACCESS PANEL 532QB AND CLAMP RING IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG 2A55 A25754

Part: PANEL — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING FUEL TANK ACCESS PANEL 532BB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON LEFT FUEL TANK ACCESS PANEL 532BB AND CLAMP RING FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED L/H WING TANK ACCESS PANEL 532BB AND CLAMP RING IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG WN8547 A25654

Part: PANEL — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING FUEL TANK ACCESS PANEL 532FB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON L/H WING FUEL TANK ACCESS PANEL 532FB AND CLAMP RING FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED LEFT WING FUEL ACCESS PANEL 532FB AND CLAMP RING IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG WN9960 A25679

Part: PANEL — CORRODED (RIGHT WING) · airframe 20,525 hrs · 8,885 cycles

RIGHT WING FUEL TANK ACCESS PANEL 632EB HAS FRETTING CORROSION; MARKED. / EVALUATED CORROSION ON RIGHT WING FUEL ACCESS PANEL 633EB FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED RIGHT WING FUEL ACCESS PANEL AND CLAMP RING 633EB IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG 2A77

Part: PANEL — CORRODED (RIGHT WING) · airframe 20,525 hrs · 8,885 cycles

RIGHT WING FUEL TANK ACCESS PANEL 633CB CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON RIGHT WING FUEL TANK ACCESS PANEL 633CB CLAMP RING. REMOVE AND REPLACED RIGHT HAND FUEL TANK ACCESS PANEL CLAMP RING IAW B737 SRM 57-20-01-01-1A-1 FIGURE 104 SHEET 7 ATAG A25758

Part: CAP — CORRODED (FWD CARGO LH) · airframe 20,525 hrs · 8,885 cycles

FWD CARGO PIT L/H FLOOR CAP STRIP HAS CORROSION AS MARKED. / NO ALLOWABLE LIMITS REPLACED L/H FLR CAP STRIP P/N 453A1611-16 AS REQUIRED IAW BOEING DWG 453A1611 REV: B.

Part: PANEL — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LEFT WING FUEL TANK ACCESS PANEL 532HB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 532HB AND CLAMP RING FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED LEFT WING FUEL ACCESS PANEL 532HB AND CLAMP RING IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG 2A78 2A54

Part: PANEL — CORRODED (RIGHT WING) · airframe 20,525 hrs · 8,885 cycles

RIGHT WING FUEL TANK ACCESS PANEL 632QB AND CLAMP RING HAVE FRETTING CORROSION; MARKED. / EVALUATED FRETTING CORROSION ON FUEL ACCESS PANEL AND CLAMP RING 632QB FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED RIGHT WING FUEL ACCESS PANEL AND CLAMP RING 632QB IAW SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 ATAG 2A57 A96143

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 20,525 hrs · 8,885 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140AF HAS CORROSION IN SEVERAL PLACES / PANEL 140; BF AFT CARGO PANEL IS OUT; OF LIMITS HAS MORE THAN 3 IN OF CORROSION OUT OF LIMITS IAW SRM 53-00-53-1A-1 RECIEVED NEW PANEL FOR 140BF TO BE INSTALLED ON WO 309140 SA-M 565 S ZA 0043; P/N 453A2610-32

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT)

AFT CARGO COMPARTMENT FLOOR PANEL 140EF IS PUNCTURED AND CORRODED / AFT CARGO FLOOR PANEL 140EF WITH PUNCTURE AND CORROSION; REPLACED WITH NEW FLOOR PANEL P/N 453A2610-58 IAW AIPC 25-52-10-19. FLOOR PANEL TO BE INSTALLED ON NON-ROUTINE CARD X821418.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 20,525 hrs · 8,885 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140DF HAS CORROSION IN SEVERAL PLACES / DAMAGE BEYOND LIMITS REPLACED PANEL #140DF P/N 453A2610-20 AS REQUIRED IAW SRM 53-00-53-1A-1 AIPC 25-52-10-19. BOEING DWG:453A2610 REV:B

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 20,525 hrs · 8,885 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140AF HAS CORROSION IN SEVERAL PLACES / AFT CARGO FLOOR PANEL 140AF WITH CORROSION IN SEVERAL PLACES; REPLACED WITH NEW FLOOR PANEL P/N 453A2610-38 IAW AIPC 25-52-10-19. PANEL TO BE INSTALLED ON DOC NUM SAM5655 PANEL SIGN OFF SHEET.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 20,525 hrs · 8,885 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140CF IS CORRODED IN SEVERAL SPOTS / DAMAGE BEYOND LIMITS SRM 53-00-53-1A-1 REPLACED PANEL #140CF P/N 453A2610-18 AS REQUIRED. IAW AIPC 25-52-10-19 BOEING DWG:453A2600 REV:B

Part: PLATE — CRACKED (RIGHT WING) · airframe 20,525 hrs · 8,885 cycles

R/H WING TRAILING EDGE CAVITY 10' INBD OF #6 FLAP TRACK ASSY WIGGLE PLATE IS CRACKED AT FASTENER HOLE / REMOVED CRACKED R/H WING TRAILING EDGE CAVITIY 10' INBD OF #6 FLAP TRACK ASSY WIGGLE PLATE AND REPLACED WITH NEW PLATE P/N 115A2781-4 IAW IPC 57-50-00-22A1 AND SRM 51-40-02 ATAG# ZA0096

Part: BRACKET — CRACKED (RIGHT WING) · airframe 20,525 hrs · 8,885 cycles

R/H WING TRAILING EDGE CAVITY 10' INBD OF DIFLECTOR RIB ASSY CURVED BULB SEAL RETAINER BRACKET ATTACHED TO WEB IS CRACKED / REMOVED AND REPLACED RTH WING TRAINING EDGE CURVED BULB SEAL RETAINER BRACKET IAW SRM 51-40-02-0G-0 STEP 4/9 AND DWG#115A2930 REV - APPLIED CIC IAW AMM 51-21-91-620-802 STEP 3C. TAG #A05811

Part: BALANCE WEIGHT — CORRODED (LEFT WING) · airframe 20,525 hrs · 8,885 cycles

LH WING AT WINGLET AT 521 ABB COUNTER BALANCE WEIGHT CORRODED. / REMOVED AND REPLACED LH WING AT WINGLET AT 521ABB COUNTER BALANCE WEIGHT. IAW DRAWING 737-9300 SHEET 1 FLAGNOTES 1; 3; 12 AND SHEET 7 VIEWS 1BT WN9453

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 20,525 hrs · 8,885 cycles

FWD CARGO FLOOR PANEL 120 DF CORRODED LH OTBD EDGE. MARKED. / DAMAGE BEYOND LIMITS REPLACED PANEL #120DF P/N 453A1610-20 AS REQUIRED I.A.W. AIPC 25-52-10-17 ATAG: WN9378

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 20,525 hrs · 8,885 cycles

FWD CARGO FLOOR PANEL 120AF CORRODED LH OUTBD EDGE. MARKED. / REPLACED FWD CARGO FLOOR PANEL 120AF IAW B737 SRM 51-10-02 AND B737-800 SRM 53-00-53-1A-1 AND B737 AIPC 25-52-10-17

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 19,006 hrs · 8,206 cycles

RT MAIN WHEEL WELL REAR SPAR VAPOR WEB CRACKED AT BS 663, RBL 36. REPAIRED WEB IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,006 hrs · 8,206 cycles

AFT CARGO COMPARTMENT FRAME FAIL SAFE CHORD CORRODED AT BS. 827, BETWEEN RBL 2 TO RBL 6. R&R CHORD IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 19,006 hrs · 8,206 cycles

RT MAIN WHEEL FORWARD VAPOR BARRIER CRACKED BETWEEN RBL 25+7 TO RBL 25+9.5. REPAIRED BARRIER PER SRM.

Part: PLATE — CRACKED (LT WING) · airframe 19,006 hrs · 8,206 cycles

LT WING REAR SPAR WIGGLE PLATE PHENOLIC STRIP CRACKED NEAR WING STATION 370. R&R WIGGLE PLATE IAW SRM AND DWG.

Part: PLATE — CRACKED (RT WING) · airframe 19,006 hrs · 8,206 cycles

RT WING TRAILING EDGE CAVITY 10" INBOARD OF NR 6 FLAP TRACK ASSEMBLY WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: VAPOR BARRIER — CRACKED (RT WHEEL WELL) · airframe 20,434 hrs · 8,842 cycles

*** DELAY PURPOSES *** R/H WHEELWELL VAPOR BARRIER CRACK / REF TSR 201807223;REPAIRED VAPOR BARRIER

Part: VAPOR BARRIER — CRACKED (RT WHEEL WELL) · airframe 20,434 hrs · 8,842 cycles

R/H MAIN WHEEL FWD VAPOR BARRIER HAS CRACK RBL 25 + 7 TO RBL 25 + 9.5 DOWNWARD APPROX. 3.5' LONG LOWER END TERMINATES AT RIVET UNABLE TO SEE UPPER END TERMINATION POINT DUE TO STRUCTURE / R/H MAIN WHEEL WELL FWD VAPOR BARRIER HAS CRACK RBL 25+7 TO RBL 25+9.5 DOWNWARD APPROX 3.5' LONG LOWER END TERMINATES AT RIVET UNABLE TO SEE UPPER END TERMINATION POINT DUE TO STUCTURE.REPAIRED PER SRM 57-10-10-2R-2 REPAIR 2 PARAGRAPH 6. THIS IS AN INTERIM REPAIR AND REQUIRES A DETAILED VISUAL INSPECTION EVERY 3000 FLIGHT CYCLES. REF 57-10-10-2R-2 REPAIR 2 SECTIONS 1.C 2.C AND PARAGRAPH 6REPETITIVE ACTION REQUIRED:PERFORM A DETAILED VISUAL INSPECTION OF FWD VAPOR BARRIER REPAIR AT RBL 25+7 TO RBL 25+9.5. REF SRM 57-10-10-2R-2

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 20,434 hrs · 8,842 cycles

RT MAIN WHEEL FORWARD VAPOR BARRIER CRACKED BETWEEN RBL 25+7 TO RBL 25+ 9.5. REPAIRED BARRIER PER SRM.

Part: COVER — MISSING (CABIN) · airframe 19,720 hrs · 8,543 cycles

L2 EXIT DOOR LIGHT COVER MISSING. INSTALLED COVER IAW AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 18,755 hrs · 8,093 cycles

L1 DOOR EMERGENCY EXIT LENS LOOSE. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: STRIP — CRACKED (CABIN) · airframe 16,830 hrs · 7,189 cycles

FORWARD LT EGRESS LIGHT STRIP RACEWAY CRACKED. R&R STRIP IAW SIP.

Part: PAN — CRACKED (ASD) · airframe 17,166 hrs · 7,349 cycles

AFT GALLEY SERVICE DOOR LOWER PAN ASSY BENT; CRACKED; AND AFT ATTACH NUT PLATE ASSY BROKEN. / R & R AFT GALLEY SERVICE DOOR LOWER PAN ASSY SOPM 20-50-01. R & R AFT NUT PLATE PER SIP. (INSP 73290)

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 15,364 hrs · 6,532 cycles

L/H EMERGENCY LIGHT LENS CRACKED BETWEEN ROWS 15 TO 27. R & R THE LENS IAW AMM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 15,364 hrs · 6,532 cycles

LEFT EMERGENCY LIGHT LENS CRACKED AT ROW 14. R & R THE LENS IAW AMM.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 14,909 hrs · 6,343 cycles

OVERWING EMERGENCY EXIT SIGN LENS DETACHED. INSTALLED THE LENS IAW SIP.

Part: LENS — CRACKED (CABIN) · airframe 10,347 hrs · 4,323 cycles

LEFT OVERHEAD BIN EMER LIGHT LENS CRACKED ROW 12. R & R LENS IAW AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 10,347 hrs · 4,323 cycles

MID CABIN OVERHEAD EXIT SIGN COVER MISSING. R & R COVER ASSEMBLY IAW SIP.

Part: LENS — BROKEN (CABIN) · airframe 7,994 hrs · 3,362 cycles

L1 DOOR EMER EXT LIGHT LENS BROKEN. R & R LENS IAW SIP.

Part: COVER — MISSING (CABIN) · airframe 7,501 hrs · 3,140 cycles

LEFT OVERWING EMER EXIT LIGHT COVER MISSING. INSTALLED COVER IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 3,970 hrs · 1,621 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

FRAME CRACKED AT BS 827, STRINGER 27R. R & R FRAME IAW SRM & DRAWING.

Part: LENS — CRACKED (CABIN) · airframe 3,970 hrs · 1,621 cycles

LT CABIN CEILING EMERGENCY LIGHT LENSES CRACKED BETWEEN ROW 8 TO ROW 27. R & R LENSES IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

FRAME CRACKED AT BS 967, LBL 31. REPAIRED FRAME IAW ER & EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

FLOOR SUPPORT STIFFENER CRACKED AT BS 887, LBL 3. R & R STIFFENER IAW SRM & DRAWING.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

AFT CARGO BAY FRAME DAMAGED AT BS 927, BETWEEN STRINGER 22R TO STRINGER 24R. REPAIRED FRAME IAW ER & EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

SHEAR TIE CRACKED AT BS 907, BL 0. R & R SHEAR TIE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

FRAME CRACKED AT BS 927, BL 0. REPAIRED FRAME IAW SRM & DRAWING.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

AFT CARGO BAY FRAME DAMAGED AT BS 927, BETWEEN STRINGER 22L TO STRINGER 24L. REPAIRED FRAME PER ER & EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

FRAME DAMAGED AT BS 947 BETWEEN STRINGER 21L TO STRINGER 23L. R & R FRAME IAW SRM & DRAWING.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

AFT CARGO BAY FRAME DAMAGED AT BS 907, BETWEEN STRINGER 22L TO STRINGER 24L. REPAIRED FRAME IAW ER & EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

AFT CARGO BAY FRAME DAMAGED AT BS 907, BETWEEN STRINGER 22R TO STRINGER 24R. REPAIRED FRAME IAW ER & EA.

Part: SUPPORT FITTING — DAMAGED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

AFT CARGO BAY BULKHEAD SUPPORT CLIP DAMAGED AT BS 907, LBL 10. R & R CLIP IAW SRM & DRAWING.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

FUSELAGE SKIN DAMAGED BETWEEN BS 887 TO BS 976, BETWEEN STRINGER 25L TO STRINGER 24R. R & R SKIN IAW DRAWING & SRM.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

FRAME DAMAGED AT BS 947 BETWEEN STRINGER 26L TO STRINGER 26R. R & R FRAME IAW SRM & DRAWING.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

SHEAR TIE DAMAGED AT BS 907, BETWEEN STRINGER 27L TO STRINGER 26L. R & R SHEAR TIE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

FRAME CRACKED AT BS 847, RBL 2. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

FRAME CRACKED AT BS 867, RBL 2.5. REPAIRED FRAME IAW ER.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

AFT CARGO BAY FRAME DAMAGED AT BS 927, BETWEEN STRINGER 26L TO STRINGER 26R. R & R FRAME IAW DRAWING & SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

SHEAR TIE CRACKED AT BS 887, BL 0. R & R SHEAR TIE IAW SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 3,970 hrs · 1,621 cycles

FUSELAGE SKIN DAMAGED BETWEEN BS 840 TO BS 887, BETWEEN STRINGER 25R TO STRINGER 25L. REPAIRED SKIN IAW ER & EA.

Part: FAN — FAILED (RECIRCULATION) · airframe 2,528 hrs · 1,026 cycles

ON CLIMB OUT ELECTRICAL BURNING ODOR. AIR TURNBACK. R&R LT RECIRCULATION FAN & HEPA FILTERS IAW MM.