N8303R

Part: SIGN — BROKEN (ZONE 200) · airframe 44,371 hrs · 20,982 cycles

EMERGENCY EXIT SIGN BROKE. R&R EMERGENCY EXIT SIGN HOUSING IAW AMM 33-51-01.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 43,732 hrs · 20,657 cycles

L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT IS OUT. REPLACED AFT LH (M1673) EMERGENCY SLIDE/OVERWING DOOR LIGHT BATTERY PACK PER [AMM 33-51-06-960-805-NG.

Part: WINGLET — CORRODED (ZONE 500) · airframe 43,475 hrs · 20,517 cycles

LEFT UPPER WINGLET ASSEMBLY MISSING PAINT IS SHOWING SIGNS OF CORROSION APPROXIMATELY 0.5 INCHES WIDE BY 2.0 INCHES IN LENGTH. EVALUATED IAW SRM 57-31-00 AP37.1-0632. REMOVED CORROSION IAW SRM 51-10-02. DAMAGE DIMENSIONS ARE AS FOLLOWS; LENGTH: 2.60 INCHES; WIDTH: 0.70 INCHES; DEPTH: 0.090 INCHES. LOCATED APPROXIMATELY 3 INCHES BELOW THE WINGLET UPPER CAP ON THE INBOARD AFT EDGE. CW PER EA 25-157-02570.

Part: HANDLE — LOOSE (ZONE 800) · airframe 42,819 hrs · 20,173 cycles

L2 DOOR ASSIST HANDLE LOOSE. SECURED L2 DOOR ASSIST HANDLE IAW B737-800 AMM 52-13-31-400-802.

Part: DOUBLER — CRACKED (ZONE 100) · airframe 42,819 hrs · 20,173 cycles

EGPR DOOR CUTOUT LOWER DOUBLER IS CRACKED. ACCOMPLISHED REPAIR ON EGPR DOOR CUTOUT LOWER DOUBLER IAW SRM 53-10-15-2R-4.

Part: HANDLE — LOOSE (ZONE 800) · airframe 42,819 hrs · 20,173 cycles

CR RR L1 DOOR ASSIST HANDLE NEEDS SECURED. SECURED L1 DOOR ASSIST HANDLE IAW B737-800 AMM 52-11-31-400-802.

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 42,303 hrs · 19,905 cycles

R2 DOOR ESCAPE SLIDE GIRT REPACK REQUIRED.<[01] REPACKED R2 DOOR SLIDE GIRT PER AMM 25-66-01.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 41,514 hrs · 19,503 cycles

FWD RH SIDE EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK M2186 PER AMM 33-51-06

Part: LIGHT — BROKEN (ZONE 200) · airframe 41,311 hrs · 19,397 cycles

R1 DOOR EMERGENCY EXIT LIGHT BROKEN.<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW AMM 33-51-14.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 41,225 hrs · 19,351 cycles

EXTERIOR EMERGENCY EXIT SLIDE LIGHT AT FWD SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED LAMP REF. AMM 33-51-04.

Part: SEAT — LOOSE (ZONE 200) · airframe 40,655 hrs · 19,051 cycles

CABIN SEAT ROW 12ABC LOOSE IN TRACK MOUNTS.<[01] ADJUSTED PASSENGER CABIN SEAT ROW 12ABC IN TRACKS IAW AMM 25-22-00.

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 40,566 hrs · 19,001 cycles

CIRCUIT BREAKER P18-3B-10 POPPED ( PAX CBN R AFT)<[01] CYCLED C/B P18-3 B10 & OPS CHECKED EMERG LIGHTS. REF AMM 33-51-00 OPS CHECK GOOD. R&R POWER SUPPLIES M1695; M1672; M1671 & BATTERIES. REF AMM 33-51-06 OPS CHECK GOOD.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 38,917 hrs · 18,128 cycles

PASSENGER CABIN CEILING EMERGENCY EXIT SIGN SCREW ACCESS COVER MISSING AT EMERGENCY EXIT<[01] INSTALLED SCREW COVER AT LIGHT COVER ASSY PER B737 AMM 33-51-00

Part: HANDLE — OUT OF ADJUST (AFT PAX DOOR) · airframe 38,881 hrs · 18,110 cycles

AFT ENTRY DOOR HANDLE POPPED UP 2 TIMES IN FLIGHT. AFT ENTRY CAUTION LIGHT CAME ON AFTER BOTH TIMES<[01] REMOVED AFT ENTRY DOOR LINER TO FOM PER AMM 52-13-00.;[02] ADJUSTED CONTROL RODS I.A.W AMM 52-13-00. OPS CHECK GOOD. REINSTALLED AFT ENTRY DOOR LINER I.A.W AMM 52-13-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,185 hrs · 17,752 cycles

EXTERNAL R1 EMERGENCY LIGHT INOP<[01] RELAMPED EXTERNAL R1 EMERGENCY EXIT LIGHT IAW AMM 33-51-04

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 37,890 hrs · 17,578 cycles

CRACK ACCESS PANEL 331B ON RIB LOCATED LE STA 300.51 AT LT HORIZONTAL STABILIZER 2023-720053<REPLACED RIB AND FASTENERS LOCATED LE STA 300.51 AT LT HORIZONTAL STABILIZER I.A.W. B737-800 SRM 51-40-02 AND DRAWING # 186A1001 REV ? HIGH FREQUENCY EDDY CURRENT INSPECTION DONE ON REMOVED RIB AS PER B737 NDT MANUAL PART 6 51-00-00 PROCEDURE 23. CRACK INDICATION NOT FOUND. TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24 SEE INDIVIDUAL SING OFF BELLOW;[04] CORRECTED STEP 3.<BR>RE-INSTALLED RIB AND FASTENERS LOCATED LE STA 300.51 AT LT HORIZONTAL STABILIZER I.A.W. B737-800 SRM 51-40-02 AND DRAWING # 186A1001 REV ? HIGH FREQUENCY EDDY CURRENT INSPECTION DONE ON REMOVED RIB AS PER B737 NDT MANUAL PART 6 51-00-00 PROCEDURE 23. CRACK INDICATION NOT FOUND. TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24 SEE INDIVIDUAL SING OFF BELLOW;[05] RE-INSTALLED RIB AND FASTENERS LOCATED LE STA 300.51 AT LT HORIZONTAL STABILIZER I.A.W. B737-800 SRM 51-40-02 AND DRAWING # 186A1001 REV ? HIGH FREQUENCY EDDY CURRENT INSPECTION DONE ON REMOVED RIB AS PER B737 NDT MANUAL PART 6 51-00-00 PROCEDURE 23. CRACK INDICATION NOT FOUND. TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24 SEE INDIVIDUAL SING OFF BELLOW

Part: WEB — CRACKED (ZN 500 LEFT WING) · airframe 37,890 hrs · 17,578 cycles

CRACK WEB TRAILING EDGE LOCATED ORSS 261 TO ORSS 273 LT WING 2023-720018<[01] REPLACED WEB ON TRAILING EDGE LOCATED ORSS 261 TO ORSS 273 LT WING IAW B737-800 SRM 51-40-02 AND DWG 115A2512-29.SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1.<BR>REPLACED WEB ON TRAILING EDGE LOCATED ORSS 261 TO ORSS 273 LT WING IAW B737-800 SRM 51-40-02 AND DWG 115A2512. REV:- SEE INDIVIDUAL SIGN OFF BELOW.;[03] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 37,890 hrs · 17,578 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED ORSS319 TO ORSS325 LT WING 2023-720024<[01] REPLACED PLATE ASSY AND FASTENERS LOCATED ORSS319 TO ORSS325 LT WING IAW B737-800 SRM 51-10-02 STEP 9 AND DWG 115A3700 SHEET 60 REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1. REPLACED PLATE ASSY AND FASTENERS LOCATED ORSS319 TO ORSS325 LT WING IAW B737-800 SRM 51-10-02 STEP 9 AND DWG #115A3712 REV: -. SEE INDIVIDUAL SIGN-OFF BELOW;[03] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 37,890 hrs · 17,578 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED IRSS212 TO IRSS219 LT WING 2023-720021<[01] REPLACED PLATE ASSY TRAILING EDGE LOCATED IRSS212 TO IRSS219 LT WING IAW B737-800 SRM 51-40-02 AND DRAWING #115A2001. REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1. REPLACED PLATE ASSY TRAILING EDGE LOCATED IRSS212 TO IRSS219 LT WING IAW B737-800 SRM 51-40-02 AND DRAWING #115A2001. REV:-. SEE INDIVIDUAL SIGN OFF BELLOW.;[03] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN OFF BELLOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,890 hrs · 17,578 cycles

CRACK BILGE AREA ANGLE LOCATED ON BS 500I AT LEVEL STR 23R AT FWD CARGO COMPARTMENT 2023-720017 CORRECTED LOCATION IS: BILGE AREA ANGLE LOCATED ON BS 500I BETWEEN STR 27R TO STR 27L LEVEL RBL 3 AT FWD CARGO COMPARTMENT<[01] REPLACED ANGLE AND FASTENERS; LOC. BILGE AREA; ON BS 500I BETWEEN STR 27R TO STR 27L; LEVEL RBL 3 AT FWD CARGO COMPARTMENT IAW B737-800 SRM-51-40-02 AND DWG-143A7902 REV: B. <BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE AND FASTENERS; LOC. BILGE AREA; ON BS 500I BETWEEN STR 27R TO STR 27L; LEVEL RBL 3 AT FWD CARGO COMPARTMENT IAW B737-800 SRM-51-40-02 AND DWG-143A7902 REV: B. <BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 37,890 hrs · 17,578 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED ORSS288 TO ORSS298 LT WING 2023-720023<[01] REPLACED PLATE ASSY TRAILING EDGE LOCATED ORSS288 TO ORSS298 LT IAW B737-800 SRM-51-40-02 AND DWG-115A3700 REV: - AND MEASUREMENTS OF CRACK IS: L= 0.500? TOOL USED: CALIPER 0-12? P/N: 500-193-30 S/N: 0036617 AND DUE DATE: 19-JUL-24;[02] COMPLETE TASK CERTIFIED

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 37,890 hrs · 17,578 cycles

CRACK ANGLE LOCATED ON AFT SIDE OF FRAME BS500G AT LEVEL STR26R AT FWD CARGO COMPARTMENT 2023-720012 CORRECTED LOCATION CRACK ANGLE LOCATED ON AFT SIDE OF FRAME BS500H AT LEVEL STR26R AT FWD CARGO COMPARTMENT<[01] REPLACED ANGLE LOCATED ON AFT SIDE OF FRAME BS500H AT LEVEL STR26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DRAWING #143A7505REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] COMPLETE TASK CERTIFIED

Part: FRAME — DEFORMED (ZN 100 FUS LOWER) · airframe 37,890 hrs · 17,578 cycles

CREASE ON FRAME BS196.5 BTW STR24R TO STR26R AT ELECTRONIC EQUIPMENT COMPARTMENT 2023-720016<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-23.;[02] REPLACED FRAME LOCATED ON BS196.5 BTW STR24R TO STR26R AT ELECTRONIC EQUIPMENT COMPARTMENT I.A.W B737-800 SRM 51-40-02-0G-0 AND DWG# 141A1502; SHEET 1; REV.F. AND DWG# 141A3502; SHEET 94; REV.-. AND DWG# 141A0650; SHEET 3; REV.E. SEE INDIVIDUAL SING OFF BELOW.;[03] CORRECTED ACTION 2<BR>REPLACED FRAME LOCATED ON BS196.5 BTW STR24R TO STR26R AT ELECTRONIC EQUIPMENT COMPARTMENT I.A.W B737-800 SRM 51-40-02-0G-0 AND DWG# 141A1502; SHEET 1; REV.F. AND DWG# 141A3502; SHEET 94; REV.-. AND DWG# 141A0650; SHEET 3; REV.E. SEE INDIVIDUAL SIGN OFF BELOW.;[04] CORRECTIVE ACTION STEP 3 CERTIFIED RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,890 hrs · 17,578 cycles

CRACK ON ANGLE LOCATED ON AFT SIDE OF FRAME BS196.5 AND BTW STR25R TO STR26R AT FWD ELECTRONIC EQUIPMENT COMPARTMENT 2023-720009<[01] REPLACED ANGLE LOCATED ON AFT SIDE OF FRAME BS196.5 AND BTW STR25R TO STR26R AT FWD ELECTRONIC EQUIPMENT COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG: 141A1502; SHEET: 1; REV: F; SEE INDIVIDUAL SIGN-OFF BELOW.;[02] RII COMPLETED JOB

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 37,890 hrs · 17,578 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS273 RT WING 2023-720010<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS273 RT WING AND FASTENER IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.;[02] REPLACED ANGLE TRAILING EDGE LOCATED ORSS273 RT WING AND FASTENER IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,890 hrs · 17,578 cycles

CRACK ANGLE LOCATED ON AFT SIDE OF FRAME BS500H AT LEVEL STR26L AT FWD CARGO COMPARTMENT 2023-720013<[01] REPLACED ANGLE LOCATED ON AFT SIDE OF FRAME BS500H AT LEVEL STR26L AT FWD CARGO IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 109 REV-;[02] REPLACED ANGLE LOCATED ON AFT SIDE OF FRAME BS500H AT LEVEL STR26L AT FWD CARGO IAW B737-800 SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 109 REV-;[03] REPLACED ANGLE LOCATED ON AFT SIDE OF FRAME BS500H AT LEVEL STR26L AT FWD CARGO IAW B737-800 SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 109 REV-

Part: ANGLE — CRACKED (ZN 300 STABILIZE) · airframe 37,890 hrs · 17,578 cycles

CRACK ANGLE ACCESS PANEL 333AB AT LT HORIZONTAL STAB 2023-719995<[01] REPLACED ANGLE ACCESS PANEL 333AB AT LT HORIZONTAL<BR>STAB I.A.W B737-800 SRM 51-10-02 AND DWG: 186A3005.<BR>SHEET: 2; REV: B;[02] REPLACED ANGLE ACCESS PANEL 333AB AT LT HORIZONTAL<BR>STAB I.A.W B737-800 SRM 51-10-02 AND DWG: 186A3005.<BR>SHEET: 2; REV: B

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 37,890 hrs · 17,578 cycles

CRACK SUPPORT ANGLE LOCATED BS867 AT LEVEL STR3R AT PASSENGER CABIN 2023-719990<[01] REPLACED SUPPORT ANGLE LOCATED BS867 AT LEVEL STR3R AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 AND DWG 146A7901 SHEET 66 REV A;[02] STEP 1 CORRECTED <BR>REMOVED AND REPLACED SUPPORT ANGLE LOCATED BS867 AT LEVEL STR3R AT PASSENGER CABIN AND NOT FOUND ALLOWED DAMAGE IN SRM ANGLE MUST BE REPLACED L:0.530 INCH TOOL USED: DIGITAL CALIPER P/N: 700-113-10 S/N: 0033168 DUE DATE 27-NOV-2023 IAW B737-800 SRM 51-40-02 AND DWG 146A7901 SHEET 66 REV A;[03] STEP 2 CORRECTED <BR>REMOVED AND REPLACED SUPPORT ANGLE LOCATED BS867 AT LEVEL STR3R AT PASSENGER CABIN AND NOT FOUND ALLOWED DAMAGE IN SRM ANGLE MUST BE REPLACED L:0.530 INCH TOOL USED: DIGITAL CALIPER P/N: 700-113-10 S/N: 0033168 DUE DATE 27-NOV-2023 IAW B737-800 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 146A7901 SHEET 66 REV A;[04] REMOVED AND REPLACED SUPPORT ANGLE LOCATED BS867 AT LEVEL STR3R AT PASSENGER CABIN AND NOT FOUND ALLOWED DAMAGE IN SRM ANGLE MUST BE REPLACED L:0.530 INCH TOOL USED: DIGITAL CALIPER P/N: 700-113-10 S/N: 0033168 DUE DATE 27-NOV-2023 IAW B737-800 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 146A7901 SHEET 66 REV A

Part: SKIN — CRACKED (RT WING SLAT) · airframe 37,890 hrs · 17,578 cycles

CRACK LOWER SKIN SLAT 6 LEADING EDGE RT WING. PERFORMED PERMANENT REPAIR ON LOWER SKIN SLAT 6 LEADING EDGE RT WING IAW SRM 57-42-01-2R-8 AND SRM 51-40-02. PERFORMED PERMANENT REPAIR ON LOWER SKIN SLAT 6 LEADING EDGE RT WING IAW SRM 57-42-01-2R-8 AND SRM 51-40-02.

Part: ACCESS PANEL — CRACKED (ZN 500 LEFT WING) · airframe 37,890 hrs · 17,578 cycles

CRACK ACCESS PANEL 551GB TRAILING EDGE ON BRACKET AT LT WING 2023-719987<[01] REPLACED BRACKET ON ACCESS PANEL 551GB TRAILING EDGE AT LT WING IAW B737-800 SRM 51-40-02 SRM 51-10-02 Ï¿½TEM 9 SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED BRACKET ON ACCESS PANEL 551GB TRAILING EDGE AT LT WING IAW B737-800 SRM 51-40-02 SRM 51-10-02 Ï¿½TEM 9 SEE INDIVIDUAL SIGN OFFS BELOW

Part: WEB — CRACKED (ZN 400 NACELLE/P) · airframe 37,890 hrs · 17,578 cycles

CRACK INBOARD FAN COWL WEB ON ENGINE 1 2023-719998<[01] REPLACED WEB INBOARD FAN COWL ON ENGINE 1 IAW B737-800 SRM 51-40-02 AND CMM 71-13-30.;[02] CERTIFIED STEP 1 COMPLETED

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 37,890 hrs · 17,578 cycles

CRACK SUPPORT BRACKET BODY STATION 540 LOCATED LBL7 AT AIR CONDITIONING BAY 2023-719961<[01] REPLACED SUPPORT BRACKET BODY STATION 540 LOCATED LBL7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND 51-10-02 Ï¿½TEM 9. SEE INDIVIDUAL SIGNOFFS BELOW;[02] CORRECTED STEP 1<BR>REPLACED SUPPORT BRACKET BODY STATION 540 LOCATED LBL7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND 51-10-02 Ï¿½TEM 9.;[03] REPLACED SUPPORT BRACKET BODY STATION 540 LOCATED LBL7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND 51-10-02 Ï¿½TEM 9.

Part: ANGLE — CRACKED (ZN 300 STABILIZE) · airframe 37,890 hrs · 17,578 cycles

CRACK ANGLE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2023-719884<[01] REPLACED ANGLE AT ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-800 SRM 51-40-02 AND B737-800 51-10-02 ITEM 9.;[02] TASK COMPLETED

Part: HANDLE — WORN (ZN 800 DOOR) · airframe 37,890 hrs · 17,578 cycles

WEAR NUT ASSIST HANDLE ON ENTRY DOOR LINING (2EA) 2023-719886<[01] REPLACED NUT ASSIST HANDLE ON ENTRY DOOR LINING IAW B737-800 AMM 52-11-31-000-802 STEP 3.G.(2);[02] CORRECTED STEP 1.<BR>REPLACED NUT ASSIST HANDLE ON ENTRY DOOR LINING IAW B737-800 AMM 52-11-31-400-802 STEP 3.G.(2);[03] CERTIFIED STEP 2 COMPLETED

Part: FAIRING — CRACKED (ZN 600 RIGHT WIN) · airframe 37,890 hrs · 17,578 cycles

CRACK RETAINER SEAL FLAP TRACK FAIRING 642AB RT WING 2023-719892<[01] REPLACED RETAINER SEAL FLAP TRACK FAIRING 642AB RT WING IAW B737-800 SRM 51-40-02-0G-0;[02] TASK COMPLETED

Part: FAIRING — CRACKED (ZN 500 LEFT WING) · airframe 37,890 hrs · 17,578 cycles

CRACK FLAP TRACK FAIRING 542BB LT WING 2023-719889<[01] TOOL USED. CALIPER PN: 500-197-30; SN: A18135081; DUE DATE: 21-JUL-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18185733; DUE DATE: 23-JAN-24.;[03] TOOL USED: SCALE P/N: SPX621 S/N: 8340225491 DUE DATE: 15-AUG-24.;[04] REPAIRED FLAP TRACK FAIRING 542BB LT WING IAW B737-800 SRM 51-70-04-2R-2 REPAIR 2. REFER TO INDIVIDUAL SIGN OFFS BELOW.;[05] REPAIRED FLAP TRACK FAIRING 542BB LT WING IAW B737-800 SRM 51-70-04-2R-2 REPAIR 2.

Part: LENS — BROKEN (ZN 200 FUS TOP) · airframe 37,890 hrs · 17,578 cycles

BROKEN GALLEY 1 COVER LENS EMERGENCY EXIT AT FWD GALLEY AREA 2023-719928<[01] REPLACED GALLEY 1 COVER LENS EMERGENCY EXIT AT FWD GALLEY AREA I.A.W B737 AMM 33-51-01-960-801 STEP 2.C ITEM (1)(C)(4);[02] COMPLETED

Part: ACCESS PANEL — CRACKED (ZN 400 NACELLE/P) · airframe 37,890 hrs · 17,578 cycles

CRACK SEAL PLATE ACCESS PANEL 441AT AT RT PYLON (2 EA) 2023-719810<[01] REPLACED SEAL PLATE ACCESS PANEL 441AT AT RT PYLON (2 EA IAW B737-800 SRM-51-40-02 AND SRM-51-10-02 ITEM 9;[02] REPLACED SEAL PLATE ACCESS PANEL 441AT AT RT PYLON (2 EA IAW B737-800 SRM-51-40-02 AND SRM-51-10-02 ITEM 9

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,890 hrs · 17,578 cycles

CRACK ANGLE LOCATED BS500G AT LEVEL STR26R AT FWD CARGO COMPARTMENT 2023-719796<[01] REPLACED ANGLE LOCATED BS500G AT LEVEL STR26R AT FWD CARGO COMPARTMENT I.A.W B737-800 SRM 51-40-02-0G-0 AND DWG 143A7505 SHEET 108 REV.-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED STEP 1 COMPLETED

Part: ACCESS PANEL — CRACKED (ZN 400 NACELLE/P) · airframe 37,890 hrs · 17,578 cycles

CRACK SEAL PLATE ACCESS PANEL 431AR AT LT PYLON 2023-719808<[01] REPLACED SEAL PLATE ACCESS PANEL 431AR AT LT PYLON IAW B737-800 SRM 51-40-02 AND 51-10-02 DWG 313A2200 SHEET 192 REV. A;[02] CERTIFIED WORK PERFORMED.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,890 hrs · 17,578 cycles

CRACK ANGLE LOCATED BS500H AT LEVEL STR26L AT FWD CARGO COMPARTMENT 2023-719798<[01] REPLACED ANGLE LOCATED BS500H AT LEVEL STR26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9 AND DWG: 143A7505 SHEET: 108 REV: -<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CERTIFIED STEP 1 COMPLETED

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 37,890 hrs · 17,578 cycles

CRACK GUSSET LOCATED BS500I AT LEVEL STR19R AT FWD CARGO COMPARTMENT 2023-719797<[01] REPLACED GUSSET LOCATED BS500I AT LEVEL STR19R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9 AND DWG: 143A7902 SHEET: 256 REV: B <BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED GUSSET LOCATED BS500I AT LEVEL STR19R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9 AND DWG: 143A7902 SHEET: 256 REV: B AS RII

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,890 hrs · 17,578 cycles

CRACK ANGLE - SUPPORT LOCATED BS947.5 AT LEVEL STR25L AT AFT CARGO COMPARTMENT 2023-719800<[01] REPLACED SUPPORT ANGLE LOCATED BS947.5 AT LEVEL STR25L AT AFT CARGO COMPARTMENT I.A.W B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTIVE ACTION CERTIFIED

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,890 hrs · 17,578 cycles

CRACK ANGLE LOCATED BS500F AT LEVEL STR26R AT FWD CARGO COMPARTMENT 2023-719795<[01] REPLACED ANGLE LOCATED BS500F AT LEVEL STR26R AT FWD CARGO COMPARTMENT .A.W B737-800 SRM 51-40-02-0G-0 AND DWG# 143A7505; SHEET 109; RE.-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1<BR>REPLACED ANGLE LOCATED BS500F AT LEVEL STR26R AT FWD CARGO COMPARTMENT I.A.W B737-800 SRM 51-40-02-0G-0 AND DWG# 143A7505; SHEET 109; RE.-. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CERTIFIED STEP 2 COMPLETED

Part: TIE CLIP — CRACKED (ZN 200 FUS TOP) · airframe 37,890 hrs · 17,578 cycles

CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-719783<[01] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW SRM B737-800 51-10-02; SRM B737-800 51-40-02; AND DRAWING # 141A1110 REV.-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CERTIFIED STEP 1 COMPLETED <BR>RII

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 37,890 hrs · 17,578 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STAR 17R AT FWD GALLEY AREA 2023-719781<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA I.A.W B737-800 SRM 51-10-02 AND DWG: 141A8310; SHEET: 33; REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[02] CERTIFIED STEP 1 COMPLETED

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 37,890 hrs · 17,578 cycles

CRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO DOOR CUT OUT 2023-719789<[01] TOOL USED DIGITAL CALIPER: P/N: 500-196-30; S/N; A22348594; DUE DATE: 13-JUL-24.;[02] TOOL USED: RADIOMETER/PHOTOMETER P/N:XRP-3000; S/N:1753759; DUE DATE:12-APR-24.;[03] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO DOOR CUT OUT IAW BOEING 737-800 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO DOOR CUT OUT IAW BOEING 737-800 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,890 hrs · 17,578 cycles

CRACK ANGLE SUPPORT LOCATED STA 727B AND LBL51 CEILING AREA AFT CARGO COMPARTMENT 2023-719787<[01] PERFORMED PERMANENT REPAIR ON ANGLE SUPPORT LOCATED STA 727B AND LBL51 CEILING AREA AFT CARGO COMPARTMENT IAW B737-800 SRM 51-70-11-2R-0 REPAIR GENERAL. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 37,890 hrs · 17,578 cycles

CRACK ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2023-719785<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: A18135081 DUE DATE: 21-JUL-24.;[02] TOOL USED: HOT BONDER P/N:HCS9200B; S/N:18165044; DUE DATE: 26-MAR-24.;[03] TOOL USED: SCALE PN: PSX621; SN: 8340225451; DUE DATE: 16-AUG-24.;[04] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18185781; DUE DATE: 24-JAN-24.;[05] TOOL USED: ULTRASONIC FLAW DETECTOR; PN:EPOCH 650; SN: 190859705; DUE DATE: 23-OCT-24;[06] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 41760200 ; DUE DATE: 23-MAR-24;[07] REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10 SEE INDIVIDUAL SIGNOFFS BELOW.;[08] REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10 SEE INDIVIDUAL SIGNOFFS BELOW.

Part: WEB — CRACKED (ZN 200 FUS TOP) · airframe 37,890 hrs · 17,578 cycles

CRACK WEB LOCATED BETWEEN BS312 TO BS328 LBL46 AND WL208 AT PASSENGER CABIN 2023-719770<[01] REPLACED WEB LOCATED BETWEEN BS312 TO BS328 LBL46 AND WL208 AT PASSENGER CABIN IAW B737-800 SRM 51-10-02 AND DWG: 141A5400 SHET: 26; REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[02] CERTIFIED STEP 1 COMPLETED

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 37,890 hrs · 17,578 cycles

CRACK ON INTERCOSTAL LOCATED BS 540 BTW RBL 1 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN 2023-719584<[01] REPLACED INTERCOSTAL LOCATED BS540 BTW RBL1 TO RBL24.75 WL208.1 AT PASSENGER CABIN I.A.W. B737-800 SRM 51-40-02 AND DWG 143A0060 SHEET 64 REV. -<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED INTERCOSTAL LOCATED BS540 BTW RBL1 TO RBL24.75 WL208.1 AT PASSENGER CABIN I.A.W. B737-800 SRM 51-40-02 AND DWG 143A0060 SHEET 64 REV. -<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 37,890 hrs · 17,578 cycles

CRACK SUPPORT ANGLE LOCATED BETWEEN BS695 RBL24.75 AND WL200 AT PASSENGER CABIN 2023-719581<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] REPLACED SUPPORT ANGLE LOCATED BETWEEN BS695 RBL24.75 AND WL200 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 AND DRAWING #273A9110 REV. A. SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: LENS — BROKEN (ZN 200 FUS TOP) · airframe 37,890 hrs · 17,578 cycles

BROKEN SIDEWALL PANEL EMERGENCY LENS ON POSITION 232ZKW AT PASSENGER CABIN (1 EA) 2023-719432<[01] REPLACED SIDEWALL PANEL EMERGENCY LENS ON POSITION 232ZKW AT PASSENGER CABIN (1 EA) I.A.W B737-800 AMM 33-51-01-960-802 STEP 3C ITEM 5(D) AND ITEM (10).;[02] TASK COMPLETED

Part: LIGHT — BROKEN (ZN 200 FUS TOP) · airframe 37,890 hrs · 17,578 cycles

BROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH AT PASSENGER CABIN (9 EA) 2023-719360<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH AT PASSENGER CABIN 9(EA) I.A.W. B737-800-AMM-33-51-15-400-802;[02] JOB COMPLETED.

Part: LIGHT — DAMAGED (ZN 200 FUS TOP) · airframe 37,890 hrs · 17,578 cycles

SCRATCH ON STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH AT PASSENGER CABIN (9 EA) 2023-719361<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH AT PASSENGER CABIN (9 EA) I.A.W B737-800-AMM-33-51-15-400-802;[02] JOB COMPLETED.

Part: EEC — FAILED (ZN 400 NACELLE/P) · airframe 16,637 hrs · 8,445 cycles

DURING CRUISE ATFL230 THE NR 2 ENGINE ROLLED BACK TO IDLE. TURNED OFF AUTO PILOT & AUTOTHROTTLE. NR 2 ENGINE PARAMETERS WERE LOW BUT NORMAL FOR IDLE. NR 2 THROTTLE HAD NO RESPONSE AT ALL RAN QRH & LANDED FLAPS 15. EMERGANCY DECLARED. TAXI TO GATE WAS NORMAL. DURING TROUBLESHOOTING FOUND THE ENTIRE A CHANNEL OF NR 2 EEC FAILED. ALSO FOUND CH B TRA SIGNAL INOP CAUSING A COMPLETE LOSS OF THRUST RESOLVER ANGLE ON NR 2 ENGINE. FOUND CONNECTOR DP0460 LOOSE CAUSING A LOSS OF CH B SINE SIGNAL. RESECURED CONNECTOR DP0460 & REMOVED & REPLACED THE NR 2 EEC IAW AMM 73-21-06 & 73-21-60. PERFORMED HIGH POWER ENGINE RUN IAW AMM 71-00-00 OPS CHECKS GOOD.

Part: MEGAPHONE — INTERMITTENT (ZN 200 FUS TOP) · airframe 36,627 hrs · 16,874 cycles

MEGAPHONE PUSH BUTTON INTERMMITENT<[01] REMOVED AND REPLACED MEGAPHONE AT FWD GALLEY AS PER AMM 25-64-00

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 35,235 hrs · 16,113 cycles

FA REPORTS MEGAPHONE INOP<[01] R&R MEGAPHONE BATTERIES IAW AMM 25-64-00

Part: INDICATOR — FAILED (CABIN PRESSURE) · airframe 34,746 hrs · 15,851 cycles

CABIN FAILED TO PRESSURIZE AT 10;000FT. NO AUTO FAIL LIGHT OR ALTN LIGHTS ILLUMINATED. DUCT PRESSURE NORMAL @ 40 / [01] REMOVED AND REPLACED CABIN ALTITUDE AND DIFFERENTIAL PRESSURE INDICATOR. IAW AMM 21-33-02

Part: PUMP — FAULTY (#1 ENGINE) · airframe 33,156 hrs · 14,979 cycles

DURING TAKEOFF ROLL; AFTER SELECTING TO/GA; THRUST LEVERS ADVANCED TO 91.8% WHEN 98.7% WAS REQUIRED. NEXT MANUALLY ADVANCED BOTH THRUST LEVERS. #1 ONLY MADE TO 92%. #2 AT 98.7%. #1 THRUST LEVER (CONT) ADVANCED FULL FORWARD. HIGHEST #1 OBSERVED STAYED AT 92%. REJECTED AT 85 KNOTS. / [01] DURING TROUBLESHOOTING FOUND #1 ENGINE FUEL PUMP IMPELLER NOT MOVING;[02] FUEL PUMP PACKAGE REMOVAL AND REPLACEMENT ACCOMPLISHED ON FAULT TTG8Q00CTXDT;[03] FUEL PUMP PACKAGE REMOVAL AND REPLACEMENT ACCOMPLISHED ON FAULT TTG8Q00CTXDT;[04] REPAIRED PER MT 773-11-00-ETOPS<BR>EV# E012392

Part: BALANCE WEIGHT — CORRODED (R/H WING) · airframe 31,855 hrs · 14,320 cycles

ON THE RIGHT WING AT THE TIP; THE INSTALLED WEIGHTS HAVE EVIDENCE OF CORROSION. ; / [01] C/W EA; [02] C/W EA 21-157-03731; [03] C/W EA 21-157-03731

Part: LIGHT — INOPERATIVE · airframe 31,855 hrs · 14,320 cycles

FWD ENTRY EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED FWD LEFT EMER. LIGHTS BATTERY PACK. TESTS GOOD PER AMM 33-51-06; [02] 1. RAFAEL ZUNIGA (TECHNICIAN); 14-DEC-2021 18:47 UTC<BR>REMOVED AND REPLACED FWD LEFT EMER. LIGHTS BATTERY PACK. TESTS GOOD PER AMM 33-51-06

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 31,855 hrs · 14,320 cycles

AFT CARGO DOOR AFT CORNER SCUFF PLATE CRACKED -MARKED. ; AFT CARGO DOOR AFT CORNER SCFF PLATE CRACKED -MARKED. / [01] REMOVED AND REPLACED AFT CARGO AFT CORNER SCUFF PLATE IAW AMM 53-11-02. REFERENCE CARD TTG8Q009GRS FOR WORK PERFORMED. LEAK CHECK TO BE ACCOMPLISHED ON POSTDOCK CARD TTG8R008B1A4.; [02] C/W; [03] C/W; [04] C/W

Part: ANGLE — CRACKED (CENTER WING) · airframe 31,855 hrs · 14,320 cycles

CABIN CENTER SECTION FLOOR PANEL BRAKE ASSY. SUPPORT ANGLE IS CRACKED AT F.S. 540 BETWEEN #2 SEAT TRACK AND CENTER BEAM BL.0 ; / [01] REMOVED AND REPLACED SUPPORT ANGLE AT STA 540 BETWEEN #2 SEAT TRACK AND BL ZERO PER SRM 51-40-02.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 31,855 hrs · 14,320 cycles

FUSELAGE PANEL 193CR HAS FIBER GLASS EROSION ON BOTH SIDES AND DELAMINATION ON INTERIOR SIDE. ; / [01] REPAIRED EROSION DAMAGE PER SRM 53-40-70-2R-1.; [02] REPAIRED EROSION AND DELAMINATION DAMAGE PER SRM 53-40-70-2R-.; [03] MISSING REFERENCE

Part: PLATE — CRACKED (RT WING) · airframe 31,855 hrs · 14,320 cycles

RT WING T/E WIGGLE PLATE CRACKED INBD OF #6 FLAP TRACK. REMOVED AND REPLACE WITH NEW WIGGLE PLATE ASSAY. PER SRM 51-40-02

Part: BRACKET — BROKEN (LT WING TE FLAP) · airframe 31,855 hrs · 14,320 cycles

LEFT WING INBD OF #2 FLAP TRACK AFT T/E LWR SHELF PNL STRUCTURE SUPPORT BRACKET IS BROKEN AT LWR REAR SPAR ; / [01] REMOVED AND REPLACED FITTING ASSY. PER SRM 51-40-02.; [02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR FITTING ASSEMBLY REPLACEMENT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,513 hrs · 14,157 cycles

OVERHEAD EMERGENCY LIGHTS AT 13-14F OVERWING INOP / R+R BATTERY PACK FOR 13-14F OVERWING EMERG. LIGHT PER AMM 33-51-06

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 13,694 hrs · 30,527 cycles

ON THE GROUND; WITH BOTH GROUND PWR OR APU POWER; THE FRONT PROVISIONING DOOR EMER. EXIT LIGHT STAYS ILLUMINATED; AND THE FRONT ENTRY EMER EXIT LT AND COCKPIT DOME LIGHT ILLUMINATE INTERMITTENTLY (IN SYNC WITH EACH OTHER). / FOUND C/B EMER. CHARGER 'FWD' POPPED AT P18-3 A-11 - CLEANED CONNECTOR AT DISCONNECT D-13018 - RESET C/N IAW M/M 20-60-01 - EMER. LIGHTS - OPS CK NORMAL IAW M/M 33-51-00

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DUE TO REPEAT FAULTS WITH FWD CABIN EMERGENCY LIGHTING; INSPECT WIRING TO BATTERY PACKS M1675; M1676; M2816; AND M2335 AND REPAIR ANY DEFECTS FOUND. IF NO DEFECTS FOUND; REPLACE BATTERY PACK M2335 AS A PRECAUTION / REMOVED AND REPLACED BATTERY PACK M2335. NO DEFECTS NOTED. REF AMM 33-51-06.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,210 hrs · 13,514 cycles

RH OVER WING EXIT DOOR; FWD; OUTSIDE EMERGENCY EXIT LIGHT INOP. / REMOVED AND REPLACE POWER SUPPLY M1676 AND BATTERY PER AMM 33-51-06

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,210 hrs · 13,514 cycles

RH OVER WING EXIT DOOR; FWD; OUTSIDE EMERGENCY EXIT LIGHT INOP. / REMOVED AND REPLACE POWER SUPPLY M1676 AND BATTERY PER AMM 33-51-06

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,210 hrs · 13,514 cycles

RH OVERWING EXIT DOOR; OUTSIDE; FWD EMERGENCY LIGHT INOP. / CHARGED OVERWING EXIT DOOR BATTERY PACK OPS CK NORMAL PER 33-51-06

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,002 hrs · 13,387 cycles

EMERGENCY LIGHT CHARGER ASSEMBLY INOP. SI #7240002 ROW 21DEF M1671 / REPLACED EMERGENCY LIGHT CHARGER ASSEMBLY @21DEF IAW AMM 33-51-06. OPS CHECK OK.

Part: BULKHEAD WEB — CRACKED (LT MLG WW) · airframe 29,895 hrs · 13,345 cycles

LH WHEEL WELL VAPOR BARRIER HAS 6' CRACK AT LBL 45.64 REMAINING AFTER PERMANENT REPAIR.ACCOMPLISHED INTERIM REPAIR IAW SRM 5710102R2.REPETITIVE ACTION REQUIRED:DO A DETAILED VISUAL INSPECTION EVERY 3000 FLIGHT CYCLES IAW SRM 5710102R2 PAR.2.C. IF ADDITIONAL DAMAGE IS FOUND DURING DETAILED VISUAL INSPECTION AND THE COMBINED LENGTH IS MORE THAN THE LIMITS IN THE INTERIM REPAIR THEN YOU MUST REPAIR WITH A PERMANENT REPAIR PER 517004 REPAIR 10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,537 hrs · 13,180 cycles

R/H AFT LOWER EMERGENCY EXIT LIGHT INOP / RE-LAMPED R/H AFT LOWER EMERGENCY EXIT LIGHT PER AMM 33-51-04. OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,138 hrs · 12,374 cycles

LEFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT BS 500 IAW AMM 31-51-06, AMD REPLACED THE LAMP IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,751 hrs · 12,135 cycles

EMERGENCY EXIT LIGHTS FO SIDE STAY ON WITH SWITCH IN ARMED MODE. FOUND M1695 RT EMERGENCY CHARGER + BATTER PACK INOP. REPLACED CHARGER + BATTERY PACK PER AMM 33-51-06.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,556 hrs · 12,001 cycles

FOUND EMERGECENCY LIGHTS OUT ON LEFT SIDE ISLE / REPLACED BATTERY AT STATION ROW 21 ABC IAW AMM REF # 33-51-06

Part: CHARGER — INOPERATIVE (CABIN) · airframe 27,556 hrs · 12,001 cycles

DURING EMERGENCY LIGHT CHECK FOUND ISLE LIGHT ON RIGHT FWD CABIN OUT BATTERY AT STATION 500C AND CHARGER INOP / R/R BATTERY CHARGER & PACK IAW AMM REF # 33-51-06

Part: RIVET — MISSING (R1 DOOR) · airframe 27,551 hrs · 11,998 cycles

FWD SERVICE DOOR AFT GIRT BAR HANGAR IS BENT. VERY HARD TO STOW THE BAR IS SAFETY POSITION / FOUND AFT BRACKET ON FWD SERVICE DOOR MISSING 1 RIVET. REMOVED SLIDE ASSY AND INSTALLED SLIDE ASSY ON DOOR IAW MT 725-61-06. REMOVED AND REPLACED RIVET ON AFT SLIDE BRACKET IAW SRM 51-40-02.

Part: VAPOR BARRIER — CRACKED (CENTER WING) · airframe 27,399 hrs · 11,932 cycles

SUPPLEMENTAL INFORMATION: L.H W/W VAPOR BARRIER HAS A CRACK 6' IN LENGTH. C/W REPAIR PER SRM 57-10-10-1A-2 REPETITIVE ACTION REQUIRED DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY. MAKE SURE THAT CRACK HAS NOT GROWN PAST THE INTERIM SEAL / A) REPETITIVE ACTION REQUIRED COMPLIED WITH; NO ADDITIONAL DAMAGE OR DETERIORATION NOTED. OK TO CONTINUE SERVICE IN ACCORDANCE WITH REFERENCE SRM 57-10-10-1A-2

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 27,399 hrs · 11,932 cycles

L.H W/W VAPOR BARRIER HAS A CRACK 6' IN LENGTH. C/W REPAIR PER SRM 57-10-10-1A-2 REPETITIVE ACTION REQUIRED DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY. MAKE SURE THAT CRACK HAS NOT GROWN PAST THE INTERIM SEAL /

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 26,604 hrs · 11,530 cycles

FORWARD CABIN FLOOR MACHINED INTERCOSTAL STA 344-360 RBL11 UPPER FLANGE IS CRACKED AT BOTH FLOOR BOARD HOLES / REMOVED AND REPLACED FORWARD CABIN FLOOR MACHINED INTERCOSTAL STA 344-360 RBL II IAW BOEING DWG 141A5400 REV:- AND B737 SRM 51-40-02-0G-0

Part: ANGLE — CORRODED (AFT CARGO) · airframe 26,604 hrs · 11,530 cycles

AFT CARGO COMPARTMENT BETWEEN STA 727C AND 727E+11' L/H ZEE ANGLE AT LBL 20 WL 155.3 HAS CORROSION TO THE TOP SKIN SURFACE IN SEVERAL AREAS AS MARKED / BLENDED CORROSION ON AFT CARGO L/H Z-ANGLE STA 727C AND 727E+11' VERIFIED ORG 'T' .040 REMAINING 'T' .032 LOSS OF .008 FOUND TO BE OUT OF LIMITS REMOVED AND REPLACE AFT CARGO L/H Z-ANGLE STA 727-847. IAW B737-800 SRM 53-00-53-2R-5 BOEING DWG 146A7500 REV- TOOL #41391 CAL DUE 09/30/20 P/N 146A7502-1

Part: WEB — CORRODED (AFT CARGO) · airframe 26,604 hrs · 11,530 cycles

AFT CARGO COMPARTMENT BETWEEN STA 787+7' AND 847 UNDER CENTER LOWER DOOR TRESHOLD PLATE ;TRESHOLD WEB IS CORRODED IN SEVERAL AREAS BETWEEN RBL 20 AND RBL 28 WL 155.3 AS MARKED / REMOVED CORROSION AFT CARGO COMPARTMENT THRESHOLD WEB STA 787+7 TO 847 IAW SRM 51-10-07-0G-0. FOUND TO BE 100% MATERIAL LOSS OUT OF LIMITS IAW SRM 53-60-15-1A-1. REMOVED AND REPLACED WEB IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A812 REV A ATAG IK0572 P/N A46A8123-25

Part: BEAM — CORRODED (AFT FUSELAGE) · airframe 26,604 hrs · 11,530 cycles

AFT CABIN R-2 CREASE BEAM INNER CHORD STA 947+12 TO 986+3 RBL51 WL208 HAS CORROSION / REMOVED CORROSION FROM R2 DOOR CREASE BEAM ORIGINAL 'T' .090. REMAINING .072. LOSS OF .018 OUT OF LIMITS IAW B737 SRM 51-70-15-1A-1. REMOVED AND REPLACED CREASE BEAM IAW B737 SRM 51-40-02-0G-0; AND BOEING DWG # 147A8501 REV L P/N 147A8540-8

Part: CREASE BEAM — CORRODED (BS 947-986) · airframe 26,066 hrs · 11,274 cycles

AFT CABIN R-2 CREASE BEAM INNER CHORD CORRODED BETWEEN BS. 947+12 TO BS. 986+3, RBL 51. / R&R CREASE BEAM IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 26,066 hrs · 11,274 cycles

FORWARD CABIN FLOOR MACHINED INTERCOSTAL UPPER FLANGE CRACKED BETWEEN BS. 344 TO BS. 360, LBL 11 AFT FLOOR BOARD HOLE. / R&R INTERCOSTAL IAW DWG AND SRM.

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 26,604 hrs · 11,530 cycles

FORWARD CABIN FLOOR MACHINED INTERCOSTAL STA 344-360 LBL11 UPPER FLANGE IS CRACKED AT AFT FLOOR BOARD HOLE / REMOVED AND REPLACED FORWARD CABIN FLOOR MACHINED INTERCOSTAL STA 344-360 LBL II IAW BOEING DWG 141A5400 REV:B AND B737 SRM 51-40-02-0G-0

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 26,604 hrs · 11,530 cycles

FORWARD CABIN FLOOR INTERCOSTAL STA 312-328 LBL45 UPPER FLANGE IS CRACKED AT FLOOR BOARD HOLE / REMOVED AND REPLACED FWD CABIN FLOOR INTERCOSTAL AT STA 312 - 328 LBL 45 IAW BOEING DWG 141A5400 REV - BOEING 737-800 SRM 51-40-02-0G-0 P/N 141A10012 ATAG A61068

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 26,066 hrs · 11,274 cycles

FORWARD CABIN FLOOR MACHINED INTERCOSTAL UPPER FLANGE CRACKED BETWEEN BS. 344 TO BS. 360, BL 0 AT AFT FLOOR BOARD HOLE. / R&R INTERCOSTAL IAW DWG AND SRM.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 26,066 hrs · 11,274 cycles

FORWARD CABIN FLOOR MACHINED INTERCOSTAL UPPER FLANGE CRACKED BETWEEN BS. 344 TO BS. 360, RBL 11 BOTH FLOOR BOARD HOLES. / R&R INTERCOSTAL IAW DWG AND SRM.

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 26,604 hrs · 11,530 cycles

FORWARD CABIN FLOOR MACHINED INTERCOSTAL STA 344-360 BL0 UPPER FLANGE IS CRACKED AT AFT FLOOR BOARD HOLE / REMOVED AND REPLACED FORWARD CABIN FLOOR MACHINED INTERCOSTAL STA 344-360 BLO IAW BOEING DWG 141-A5400 REV:- AND B737 SRM 51-40-02-0G-0

Part: ANGLE — CORRODED (AFT CARGO) · airframe 26,604 hrs · 11,530 cycles

AFT CARGO COMPARTMENT BETWEEN STA 727F -11.50' AND 747+9' L/H ZEE ANGLE HAS CORROSION IN SEVERAL AREAS TO THE TOP SKIN SURFACE LBL 20 WL 155.3 AS MARKED / BLENDED CORROSION ON AFT CARGO L/H Z-ANGLE STA 727F-11.50' AND 747+9. VERIFIED ORG 'T' .040 REMAINING 'T' .033 LOSS OF .007 FOUND TO BE OUT OF LIMITS REMOVED AND REPLACE L/H Z-ANGLE STA 727-847 ON W/O Y140681 B737-800 SRM 53-00-53-1A-2 TOOL# 41391 CAL DUE 09/30/20 P/N 146A7502-1

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,604 hrs · 11,530 cycles

AFT CABIN FLOOR BEAM STA 947 LBL13-RBL11 WL208 UPPER FLANGE HAS CORROSION IN AND AROUND FASTENER HOLES / REMOVED CORROSION. BLEND AREA AT RBLID. ORIGINAL 'T' .180 REMAINING .146 LOSS OF .034 OUT OF LIMITS IAW B737 SRM 53-70-51-1A-1. FIG 104. REPAIRED AREA IAW B737 SRM 53-70-51-2R-8 REPAIR 8. AT STA 947

Part: FLOOR SUPPORT — CORRODED (BS 947-986) · airframe 26,066 hrs · 11,274 cycles

AFT CABIN FLOOR SUPPORT CORRODED BETWEEN BS. 947+2 TO BS. 986+3, LBL 50. / R&R FLOOR SUPPORT IAW DWG AND SRM.

Part: ANGLE — CORRODED (BS 727-847) · airframe 26,066 hrs · 11,274 cycles

AFT CARGO COMPARTMENT L/H ZEE ANGLE CORRODED BETWEEN BS. 727 TO BS. 847, LBL 20, TO THE TOP SKIN SURFACE IN SEVERAL AREAS. / R&R L/H Z-ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 26,604 hrs · 11,530 cycles

FORWARD CABIN FLOOR INTERCOSTAL STA 277-294 BL0 UPPER FLANGE IS CRACKED AT BOTH FLOOR BOARD HOLES / REMOVED AND REPLACED FORWARD CABIN FLOOR INTERCOSTAL STA 227 TO 294 BLO IAW B-737 SRM 51-40-02 AND DWG 141A5400 REV- ATAG WN6748 P/N141A5410-3

Part: CAP — CORRODED (AFT FUSELAGE) · airframe 26,604 hrs · 11,530 cycles

AFT CABIN FLOOR BEAM UPPER SURFACE STA 986 LBL43 WL208 HAS CORROSION AROUND DOME NUT FASTENERS / ACCOMPLISHED FLOOR BEAM T-CAP REPAIR AT STA 986 LBL 43 WL 208 I.A.W SRM 53-70-51-2R-6 REV 68

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 26,604 hrs · 11,530 cycles

FORWARD CABIN FLOOR INTERCOSTAL STA 312-328 RBL32 UPPER FLANGE IS CRACKED AT BOTH FLOOR BOARD HOLES / REMOVED CRACKED INTERCOSTAL AT CABIN STA 312 TO 328 REB 32 IAW 737-800 SRM 51-50-02-0G-0. VERIFIED NEW INTERCOSTAL AS P/N: 141A5410-12 IAW BOEING DWG 141A5400 REV - AND A-TAG 161068. PICKED UP HOLED IN NEW INTERCOSTAL IAW 737-800 SDRM 51-40-05-0G-0 AND BOEING DWG 141A5400 REV - INSTALLED INTERCOSTAL AT CABIN STA 312 TO 328. RBL 32 IAW 737-800 SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 REV -. APPLIED CIC TO REPAIR AREA IAW 737-800 AMM 51-21-91-620-802.

Part: SUPPORT — CORRODED (AFT FUSELAGE) · airframe 26,604 hrs · 11,530 cycles

AFT CABIN FLOOR SUPPORT STA 947+2 TO 986+3 LBL50 WL208 HAS CORROSION EMITTING FROM UNDER LAV MOUNT / REMOVED AND REPLACED AFT CABIN FLOOR SUPPORT STA 947 +2 TO STA 967 LBL50 IAW DWG 147A5650 REV C AND B-737 SRM 51-40-02 ORIG 'T' .150; REMAINING .120; LOSS OF .030 FOUND TO BE OUT OF LIMITS IAW B-737 SRM 53-70-51-1A-1 TOOL 36647 DUE 6-7-20. ATAG 1K0568 P/N 147A5660-21

Part: ANGLE — CORRODED (AFT CARGO) · airframe 26,604 hrs · 11,530 cycles

AFT CARGO COMPARTMENT BETWEEN STA 747+9' AND 847 L/H ZEE ANGLE LBL 20 WL 155.3 HAS SEVERAL AREAS OF CORROSION TO TOP SKIN SURFACE AS MARKED / BLENDED CORROSION ON AFT CARGO L/H 'Z' ANGLE STA 747+9 AND 847 VERIFIED ORG 'T' .040 REMAINING 'T' .030 LOSS OF .010 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED ON W/O Y140681 TOOL #41391 CAL DUE 09/30/20 DOEING 737-800 SRM 53-00-53-1A-2 P/N 146A7502-1

Part: FLOORBEAM — CORRODED (BS 986) · airframe 26,066 hrs · 11,274 cycles

AFT CABIN FLOOR BEAM UPPER SURFACE CORRODED AT BS. 986, LBL 43, AROUND DOME NUT FASTENERS. / REPAIRED FLOOR BEAM T-CAP IAW SRM.

Part: CAP — CORRODED (AFT CARGO BAY) · airframe 26,604 hrs · 11,530 cycles

RH. CAP STRIP CORRODED AFT PIT / VERIFIED NEW PART IAW B737 AIPC 25-52-10-04.REPLACED PART ON SHELF. REMOVED CORROSION FROM CAP STRIP . NO PUBLISHED ALLOWABLE LIMITS. REPLACEMENT PART TO BE INSTALLED ON SA-M S ACCOMPLISHMENT

Part: CTOT PANEL — CRACKED (FUSELAGE) · airframe 26,604 hrs · 11,530 cycles

AFT CARGO DOOR FWD CUT OUT PANEL GOUGED/ CRACKED / FOUND GOUGE/CRACK AT AFT CARGO DOOR; FWD CUTOUT PANEL TO BE OUT OF LIMITS IAW 737-800 SRM 53-00-15-1A-1 FIG 103. VERIFIED NEW AFT CARGO; FWD CUTOUT REVEAL PANEL AS P/N: 146A9403-237 IAW 737-800 AIPC 53-11-00-48A AND A-TAG MM3256. PANEL PLACED ON PARTS RACK.

Part: CAP — CORRODED (AFT CARGO BAY) · airframe 26,604 hrs · 11,530 cycles

LH. CAP STRIP CORRODED AFT PIT / VERIFIED NEW PARTS IAW B737 AIPC 25-52-10-04. REPLACED PART ON SHELF. REMOVED CORROSION FROM CAP STRIP. NO PUBLSHED ALLOWABLE LIMITS REPLACEMENT PART TO BE INSTALLED ON SA-M 565S ACCOMPLSMENT

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 26,604 hrs · 11,530 cycles

RH. MID CAP STRIP CORRODED AFT PIT / VERIFIED NEW PART IAW B737 AIPC 25-52-10-04. REPLACED PART ON SHELF. REMOVED CORROSION FROM CAP STRIP. NO PUBLISHED ALLOWABLE LIMITS. REPLACEMENT PART TO BE INSTALLED ON SA-M 565S ACCOMPLISHMENT ATAG# WN0314

Part: CAP — CORRODED (AFT CARGO BAY) · airframe 26,604 hrs · 11,530 cycles

RH. CAP STRIP CORRODED AFT PIT / VERIFIED NEW PART IAW B737 AIPC 25-52-10-04. REPLACED PART ON SHELF. REMOVED CORROSION FROM FROM CAP STRIP. NO PUBLISHED ALLOWABLE LIMITS. REPLACEMENT PART TO BE INSTALLED ON SA-M 565S ACCOMPLISHMENT

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,066 hrs · 11,274 cycles

R/H OVERWING EMERGENCY EXIT LIGHT INOP. / CORRECTED LIGHT CONNECTION IAW WPM AND WDM.

Part: CONTROL VALVE — FAULTY (BLEED AIR SYS) · airframe 25,539 hrs · 11,020 cycles

DIVERSION, L DUCT PRESS READING 4LBS, RT 42. R&R PRECOOLER CONTROL VALVE IAW AMM.

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 24,581 hrs · 10,573 cycles

VAPOR BARRIER IS CRACKED AT FWD LF WHEEL WELL BELOW THE LOWER CHORD AND BETWEEN / ACCOMPLISHED TIME LIMITED REPAIR PER EA # 1-A57-13410. REQ'S REINSPECT EVERY 100 FLT CYCLES TO VERIFY ANY GROWTH AT DAMAGE AND PERMANENT REPAIR MUST BE ACCOMPLISHED BY 600 FLT CYCLES.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 24,304 hrs · 10,435 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1672. / R&R BATTERY PER MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 24,304 hrs · 10,435 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1673. R&R BATTERY PER MM.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 24,581 hrs · 10,573 cycles

LH HORIZONTAL STAB- UPPER FWD SLIDING SEAL IS CRACKED / R&R L./H HORIZONTAL STAB UPPER FWD SLIDING SEAL REF AMM 53-31-31 ( INSP 44444)

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 24,581 hrs · 10,573 cycles

RH HORIZONTAL STAB- UPPER FWD SLIDING SEAL IS CRACKED / R&R R/H HORIZONTAL STAB UPPER FWD SLIDING SEAL REF AMM 53-31-31

Part: LENS — MISSING (EXIT SIGN) · airframe 24,461 hrs · 10,518 cycles

LT OVERWING AFT DOOR EXIT SIGN LOWER RT SIDE MISSING. INSTALLED LENS IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 22,329 hrs · 9,509 cycles

LT FORWARD EMERGENCY LIGHTS INOP AT LOCATION M2816. R&R BATTERY CHARGER PER AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 22,329 hrs · 9,509 cycles

LT FORWARD EMERGENCY LIGHTS INOP AT LOCATION M1675. R&R BATTERY CHARGER PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,329 hrs · 9,509 cycles

LT FORWARD EMERGENCY LIGHTS INOP AT LOCATION M1675. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,329 hrs · 9,509 cycles

RT FORWARD EMERGENCY LIGHTS INOP AT LOCATION M2816. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,329 hrs · 9,509 cycles

LT FORWARD EMERGENCY LIGHTS INOP AT LOCATION M2816. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,329 hrs · 9,509 cycles

RT FORWARD EMERGENCY LIGHTS INOP AT LOCATION M1675. R&R BATTERY PACK PER AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 22,329 hrs · 9,509 cycles

RT FORWARD EMERGENCY LIGHTS INOP AT LOCATION M2816. R&R BATTERY CHARGER PER AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 22,329 hrs · 9,509 cycles

RT FORWARD EMERGENCY LIGHTS INOP AT LOCATION M1675. R&R BATTERY CHARGER PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 21,822 hrs · 9,293 cycles

R2 DOOR EMERGENCY EXIT SIGN LOOSE. R&R SIGN BASE MM.

Part: SIGN — LOOSE (CABIN) · airframe 21,831 hrs · 9,296 cycles

R2 DOOR EMERGENCY EXIT SIGN LOOSE. R&R SIGN BASE IAW MM.

Part: FLAP — OUT OF POSITION (L1 DOOR SLIDE) · airframe 21,160 hrs · 9,007 cycles

L1 DOOR SLIDE FLAP OUT OF POSITION. REPOSITIONED THE SLIDE FLAP IAW AMM.

Part: CONTROL UNIT — FAULTY (COCKPIT) · airframe 20,477 hrs · 8,685 cycles

DECLARED EMERGENCY, ON DESCENT LOST STANDBY POWER. R&R STANDBY POWER CONTROL UNIT PER AMM.

Part: VAPOR BARRIER — CRACKED (RT WHEEL WELL) · airframe 20,402 hrs · 8,650 cycles

RH MAIN WHEEL WELL VAPOR BARRIER HAS CRACKED AT 2 EACH FASTERNER HOLE LOCATIONS / RH MAIN WHEEL WELL VAPOR BARRIER CRACK AT 2 EACH FASTERNER HOLE REPAIRED IAW SRM 57-10-10-2R-2 AND IAW SRM 51-70-04-2R-10.

Part: FLOOR SUPPORT — CRACKED (BS 500G-500H) · airframe 19,245 hrs · 8,104 cycles

FORWARD CARGO BAY FLOOR SUPPORT CRACKED BETWEEN BS 500G TO 500H, RBL 25. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: BARRIER — CRACKED (BS 663) · airframe 19,245 hrs · 8,104 cycles

RT MAIN WHEEL WELL BULKHEAD CRACKED. REPAIRED THE BULKHEAD IAW SRM.

Part: INTERCOSTAL — CRACKED (FWD CARGO BAY) · airframe 20,402 hrs · 8,650 cycles

FWD CARGO COMPARTMENT INTERCOSTAL AT BS 500G-500H RBL 25 FOUND CRACKED UPON REMOVAL OF RH TRANSITION STRIP / REMOVED AND REPLACED FWD CARGO COMPARTMENT INTERCOSTAL AT BS 500G-500H RBL 25 IAWSRM 51-40-02-0G-0 AND BOEING DWG 143A7505 57575U 12/14/17

Part: FLOOR SUPPORT — CORRODED (BS 500D-500E) · airframe 19,245 hrs · 8,104 cycles

FORWARD CARGO BAY FLOOR SUPPORT CORRODED BETWEEN BS 500D TO 500E, RBL 25. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FWD CARGO BAY) · airframe 20,402 hrs · 8,650 cycles

***CORROSION*** FWD CARGO COMPARTMENT INTERCOSTAL AT BS 500D-500E RBL 25 FOUND TO HAVE CORROSION UPON REMOVAL OF RH TRANSITION STRIP / REMOVED AND REPLACED FWD CARGO COMPARTMENT INTERCOSTAL AT BS 500D-500E RBL 25 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7505 57305U 12/14/17

Part: FLOOR SUPPORT — CORRODED (FWD CARGO BAY) · airframe 20,402 hrs · 8,650 cycles

******CORROSION********* FORWARD CARGO PIT; FLOOR SUPPORT STA 500I RBL 25 TO LBL 25 WAS FOUND TO HAVE CORROSION UPON REMOVAL TO FOM OF Z CHANNEL. / FWD CARGO PIT; FLOOR SUPPORT STA. 500I RBL25 TO LBL25 WAS FOUND TO HAVE CORROSION OUT OF LIMITS. PART WAS REQUIRED TO BE REPLACED IAW PART REPLACEMENT SRM 51-10-02-0G-0. 2. LOCATED. DRILLED REPLACEMENT PART ITEM # 7530142 P.O.# 659544 IAW SRM 51-40-02-0G-0. DWG'S 143A9481 FRAME 4 AND 143A7500 FRAME 7. 92058U 12/15/17

Part: FLOORBEAM — CORRODED (BS 500I) · airframe 19,245 hrs · 8,104 cycles

FORWARD CARGO BAY FLOORBEAM CORRODED AT BS 500I, BETWEEN RBL 25 TO LBL 25. R & R THE FLOORBEAM IAW SRM & DWG.

Part: ANGLE — CORRODED (BS 767) · airframe 19,245 hrs · 8,104 cycles

SHIELD ANGLE CORRODED AT BS 767, RBL 22. R & R THE ANGLE IAW SRM.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 20,402 hrs · 8,650 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT STA 727E+13 - 767; WL155; RBL22 / REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT 727E+13-767 WL 155; RBL 22 IN AREA L= 1.0 X W= 3.0 X D= .015 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DETAIL E; REMOVED DAMAGED SECTION 727E+13-767 WL155 RBL 22 FAB'D REPAIR PARTS IAW SRM 53-00-53-2R-5 & DWG 146A7500; TREATED REPAIR PARTS IAW AMM 51-21-41-370-802 PRIMED IAW AMM 51-21-72-370-804; INSTALLED REPAIR PARTS IAW SRM 53-00-53-2R-5 & DWGS 146A7500; 146A7502 81146U 12/14/17

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 20,402 hrs · 8,650 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT STA 727F+6 - 867; WL155; LBL22 / REMOVED DAMAGED FLOOR TO SIDEWALL SUPPORT A STA 727F+6 -867 AND REPLACED FLOOR TO SIDEWALL SUPPORT BS 727 F+ 6 -867 IAW SRM 53-00-53-2R-5

Part: GUSSET — CRACKED (FUSELAGE) · airframe 19,245 hrs · 8,104 cycles

FORWARD CARGO GUSSET CRACKED AT BS 500I, STR 19R. R&R GUSSET IAW SRM & DWG.

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 20,402 hrs · 8,650 cycles

***CORROSION*** ON SIDE SHIELD STA 767-776; WL155; RBL22 / REMOVED DAMAGED SHIELD P/N 146A8127-12 REPLACED W/NEW SHIELD AND INSTALLED IAW DWG 146A0081; SRM 51-10-02-0G-0

Part: SHIELD — CORRODED (BS 767-776) · airframe 19,245 hrs · 8,104 cycles

SHIELD CORRODED BETWEEN BS 767 TO 776, RBL 22. R & R THE SHIELD IAW DWG & SRM.

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 20,402 hrs · 8,650 cycles

***CORROSION*** ON SIDE SHIELD CLIP STA 767; WL155; RBL22 / REMOVED DAMAGED CLIP FROM SHIELD. INSTALLED NEW CLIP ON NEW SHIELD. CLIP PN-145A8125-39. ALL WORK PERFORMED IAW SRM 51-10-02; SRM 51-40-05; AND SRM 51-40-02.

Part: STANCHION — CRACKED (AFT CARGO BAY) · airframe 20,402 hrs · 8,650 cycles

STANCHION CLIP IS CRACKED STA 865; WL164;LBL10 / REMOVED STANCHION CLIP IAW SRM 51-40-02-0G-0 AT STA. 865; WL 164 LBL 10 RECEIVED NEW PART ITEM # 149A8109U114 P.O.# 647599 INSTALLED NEW PART IAW SRM 51-40-02-0G-0 AND BOEING DWG 149A8102

Part: BULKHEAD — CRACKED (BS 663) · airframe 19,245 hrs · 8,104 cycles

LT WHEEL WELL BULKHEAD CRACKED. REPAIRED THE BULKHEAD IAW SRM.

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 20,402 hrs · 8,650 cycles

FWD CARGO GUSSET CRACKED STA500I STR19R / REMOVED AND REPLACED STA. 5003 519R GUSSET PO 66218 IAW SRM 51-40-01-OG-0. BOEING DWG 143A7902. SRM 51-40-05-OG-0

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 20,402 hrs · 8,650 cycles

***CORROSION*** ON FLOOR PANEL SPLICE STA 773; WL155; RBL5-15 / REMOVED SPLICE STRAP BS 773; FABRICATED PER DWG 146A9401; ALODINED & PRIMED PER SRM 51-20-01 & AMM 51-21-72; INSTALLED NUTPLATES PER SRM 51-40-02 & DWG 146A9401 57171U 15DEC17

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 19,245 hrs · 8,104 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727F+6 TO BS 867, LBL 22. R&R SUPPORT IAW SRM.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 20,402 hrs · 8,650 cycles

***CORROSION*** ON FLOOR PANEL SPLICE STA 727I; WL155; RBL17 / REMOVED SPLICE STRAP BS727I; FABRICATED PER DWG 146A9401; ALODINED & PRIMED PER SRM 51-20-01 & AMM 51-21-72; INSTALLED NUTPLATES PER SRM 51-40-02 & DEG 146A9401 57171U 15DEC17

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 20,402 hrs · 8,650 cycles

***CORROSION*** FWD CARGO COMPARTMENT L/H TRANSITION STRIP HAS CORROSION FROM STA 400 TO 500 I AT STR. 25 / REMOVED DAMAGED FWD CARGO L/H TRANSITION ANGLE 400-500I AND REPAIRED DAMAGE SECTION IAW SRM 53-00-53-2R-5

Part: BRACKET — CRACKED (RT WING) · airframe 20,402 hrs · 8,650 cycles

RIGHT TRAILING EDGE L-BRACKET ON INBOARD SIDE OF FIXED TRAILING EDGE SUPPORT BEAM CRACKED. (MARKED) / REMOVED AND REPLACED RIGHT TRAILING EDGE L-BRACKET ON WHOARD SIDE OF FIXED TRAILING EDGE SUPPORT BEAM IAW PERMMENT #115A6200 ID 0002 REV:B AND SRM 51-40-02-OG-04.

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 20,402 hrs · 8,650 cycles

***CORROSION*** FWD CARGO COMPARTMENT R/H TRANSITION STRIP HAS CORROSION FROM STA 500A TO 500 I AT STR. 25 / CORROSION ON R/H TRANSITION STRIP STA 500A-500I RBL 21 REMOVED IN AN AREA OF 2' X 1.3' X 0.020' AT ORIGINAL THICKNESS OF 0.040' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED R/H TRANSITION STRIP FROM STA 500A-500I RBL 21 IAW SRM 51-40-02-OG-0; SRM 53-00-53-22-5; AND BOEING DWG 143A7500

Part: SIDEWALL SUPPORT — CORRODED (BS 727E-767) · airframe 19,245 hrs · 8,104 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727E+13 TO 767, RBL 22. REPAIRED THE SIDEWALL SUPPORT IAW SRM & DWG.

Part: VAPOR BARRIER — DEBONDED (BS 663) · airframe 19,245 hrs · 8,104 cycles

RT WHEEL WELL LOWER BULKHEAD VAPOR BARRIER DISBONDED AT BS 663, LBL 35. REPAIRED BARRIER IAW SRM.

Part: LENS — DAMAGED (CABIN) · airframe 19,684 hrs · 8,306 cycles

LT EMERGENCY EXIT LIGHT LENS DAMAGED BETWEEN ROW 23 TO ROW 27. R&R LENS IAW AMM.

Part: LENS — DAMAGED (CABIN) · airframe 19,684 hrs · 8,306 cycles

RT EMERGENCY EXIT LIGHT LENS DAMAGED AT ROW 25. R&R LENS IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 20,017 hrs · 8,463 cycles

LT EMERGENCY AISLE BULLNOSE LIGHT LENS MISSING AT ROW 8. INSTALLED LENS PER MM.

Part: LATCH — BROKEN (R2 DOOR) · airframe 18,868 hrs · 7,936 cycles

R2 DOOR EMERGENCY EVAC SLIDE LATCH BROKEN. R&R LATCH PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIIGHT) · airframe 18,267 hrs · 7,664 cycles

RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BULB IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 17,172 hrs · 7,203 cycles

AFT GALLEY RIGHT EMERGENCY LIGHT LENS COVER MISSING. INSTALLED COVER PER SIP.

Part: LENS — MISSING (CABIN) · airframe 11,207 hrs · 4,585 cycles

LEFT AFT OVERWING OVERHEAD BIN EMER AISLE LENS MISSING. INSTALLED LENS IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 10,397 hrs · 4,238 cycles

L1 DOOR EXIT LIGHT LENS COVER BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 8,288 hrs · 3,274 cycles

LEFT WING UPPER FIXED TE PANEL AFT OF NR 3 PYLON SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: COVER — MISSING (CABIN) · airframe 7,760 hrs · 3,059 cycles

LEFT AFT CTR OVERHEAD LIGHT COVER MISSING. R & R LIGHT ASSEMBLY IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 6,563 hrs · 2,559 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER IAW SIP.

Part: LENS — BROKEN (CABIN) · airframe 5,040 hrs · 1,916 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LENS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 524 hrs · 176 cycles

EEPLS LENS LOOSE AT ROW 16. SECURED LENS PER MM.