N762SW

Part: PITOT SYSTEM — FAILED (ZN 100 FUS LOWER) · airframe 79,687 hrs · 47,358 cycles

AIRSPEED DISAGREE AFTER T/O. F/O INDICATION APPEARED CORRECT.<[01] PERFORMED ADIRS BITE IAW FIM 34-21 TASK 801. NO INFLIGHT FAULT FOUND. 1 PREVIOUS LEG FAULT FOR TAT PROBE FAIL. 34-21022. SEE L/P#2514346 FOR FINAL REPAIR.;[02] REF LOGPAGE# 2514349 FOR FINAL REPAIR

Part: ENGINE — HUNG START (ZN 400 NACELLE/P) · airframe 78,710 hrs · 46,733 cycles

ENG #1 REQUIRED A RESTART AFTER A HUNG START. 2ND ENGINE START NORMAL INCLUDING ALL INDICATION. APPROX 5 MIN LATER PAX REPORTED FLAMES FROM #1<[01] C/W FIM TASK 71-05-811; NO DEFECTS NOTED. VERIFIED OIL CONSUMPTION WITHIN LIMITS. (.431/HR).

Part: DOUBLER — CRACKED (ZN 100 FUS LOWER) · airframe 78,587 hrs · 46,648 cycles

ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER HAS CRACK DAMAGE ON FORWARD LOWER CORNER THAT EXTENDS UNDERNEATH AIRCRAFTS FUSELAGE SKIN THEREFORE BEING OUT OF LIMITS PER ALLOWABLE DAMAGE LIMITS. ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER HAS CRACK DAMAGE ON FORWARD LOWER CORNER THAT EXTENDS UNDERNEATH AIRCRAFTS FUSELAGE SKIN THEREFORE BEING OUT OF LIMITS PER ALLOWABLE DAMAGE LIMITS. PERMANENT REPAIR REQUIRED.<[01] ACCOMPLISHED PERMANENT REPAIR TO ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER TO LOWER FORWARD CORNER PER ENGINEERING EA 23-153-01830 REF (TTG8Q00LH19E)

Part: FAIRING — DELAMINATED (ZN 400 NACELLE/P) · airframe 78,339 hrs · 46,487 cycles

LH ENGINE AFT STRUT FAIRING 431ER PANEL DELAMINATED.<[01] REMOVED AND REPLACED PANEL 431ER REF AMM 54-53-01

Part: GIRT BAR — LOOSE (ZN 200 FUS TOP) · airframe 77,540 hrs · 45,968 cycles

AFT SERVICE DOOR GIRT BAR IS LOOSE<[01] RE-SECURED AFT SERVICE DOOR GIRT BAR PER S.I.P

Part: MEGAPHONE — INOPERATIVE (FWD GALLEY) · airframe 76,768 hrs · 45,470 cycles

F/A REPORTS MEGAPHONE INOP / [01] REMOVED AND REPLACED FORWARD GALLEY MEGAPHONE AMM 25-64-00

Part: SUPPORT — CRACKED (R/H WING) · airframe 76,628 hrs · 45,374 cycles

RIGHT WING #8 SLAT I/B AUX TRACK SKIN TAB I/B TAB SUPPORT IS CRACKED. / [01] R&R RIGHT WING #8 SLAT I/B AUX TRACK SKIN TAB I/B SUPPORT AS PER AMM 27-81-00 AND AMM 20 50-11.

Part: NONE — LOOSE (L/H WING) · airframe 76,628 hrs · 45,374 cycles

LEFT WING LOWER T/E PANEL NOT SECURE AT BRACKET I/B OF PYLON FAIRING / [01] REMOVED AND REPLACED LOWER ATTACHMENT BRACKET ASSY FOR THE LEFT WING LOWER T/E PANEL I/B OF PYLON FAIRING PER AMM 57-50-02

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 76,228 hrs · 45,102 cycles

RH AFT SERVICE SLIDE HANGING LOOSE / [01] REPOSTIONED R2 SLIDE PER MM25-66-01

Part: GIRT BAR — OUT OF POSITION (FWD ENTRY DOOR) · airframe 76,149 hrs · 45,053 cycles

FWD ENTRY GIRT BAR NEEDS ADJUSTMENT / [01] PROPERLY STOWED ESCAPE SLIDE GIRT BAR FLAP MATERIAL IAW AMM 25-66-01.

Part: HANDLE — OUT OF POSITION (R2 DOOR) · airframe 75,146 hrs · 44,416 cycles

R-2 DOOR SLIDE; MANUAL INFLATION HANDLE COVER NOT SECURED R-2 DOOR SLIDE MANUAL INFLATION HANDLE COVER NOT SECURED / [01] SECURED FLAP IAW AMM 25-66-00

Part: HANDLE — OUT OF POSITION (R1 DOOR) · airframe 75,146 hrs · 44,416 cycles

R-1 DOOR SLIDE; MANUAL INFLATION HANDLE COVER NOT SECURED R-1 DOOR SLIDE MANUAL INFLATION HANDLE COVER NOT SECURED / [01] SECURED FLAP IAW AMM 25-66-00

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 75,107 hrs · 44,385 cycles

L1 DOOR EMERGENCY EXIT LIGHT 1 BULB INOP / [01] RESECURED EMERGENCY EXIT LIGHT DOOR L1 AS PER B737-AMM 33-51-01-960-801.PERFORMED EMERGENCY LIGHT TEST FOUND NORMAL.;[02] VERIFIED STEP 1

Part: LIGHT — INOPERATIVE · airframe 75,107 hrs · 44,385 cycles

SEVERAL EMERGENCY LIGHTS INSIDE CABIN AND OUTSIDE INOPS / [01] REMOVED AND REPLACED BATTERY PACK AT M1670 ;M1674;M1672 AND M1668 POSITIONS AS PER REF B737; AMM 33-51-06-960-805.PERFORMED BATTERY PACK SYSTEM TEST AND FOUND NORMAL.

Part: LIGHT — INOPERATIVE · airframe 75,107 hrs · 44,385 cycles

SEVERAL EMERGENCY LIGHTS INSIDE CABIN AND OUTSIDE INOPS / [01] REMOVED AND REPLACED BATTERY PACK AT M1670 ;M1674;M1672 AND M1668 POSITIONS AS PER REF B737; AMM 33-51-06-960-805.PERFORMED BATTERY PACK SYSTEM TEST AND FOUND NORMAL.

Part: LIGHT — INOPERATIVE · airframe 75,107 hrs · 44,385 cycles

SEVERAL EMERGENCY LIGHTS INSIDE CABIN AND OUTSIDE INOPS / [01] REMOVED AND REPLACED BATTERY PACK AT M1670 ;M1674;M1672 AND M1668 POSITIONS AS PER REF B737; AMM 33-51-06-960-805.PERFORMED BATTERY PACK SYSTEM TEST AND FOUND NORMAL.

Part: LIGHT — INOPERATIVE · airframe 75,107 hrs · 44,385 cycles

SEVERAL EMERGENCY LIGHTS INSIDE CABIN AND OUTSIDE INOPS / [01] REMOVED AND REPLACED BATTERY PACK AT M1670 ;M1674;M1672 AND M1668 POSITIONS AS PER REF B737; AMM 33-51-06-960-805.PERFORMED BATTERY PACK SYSTEM TEST AND FOUND NORMAL. REMOVED AND REPLACED BATTERY PACK CHARGER AT POSITION M1668 AS PER B737;AMM 33-51-06-960-806.PERFORMED BATTERY OPERATIONAL CHECK FOUND NORMAL AS PER 33-51-06-805.

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 75,107 hrs · 44,385 cycles

FWD CARGO BAFFLE AT STA.400-STA.420; STR.26L; WL 206; CRACKED / [01] REMOVED BAFFLE AT FWD CARGO COMPARTMENT BETWEEN FS 400-420 STR 26L WL 206 IN REF B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED BAFFLE AT FWD CARGO COMPARTMENT BETWEEN FS 400-420 STR 26L WL 206 IN REF B737-700 SRM 51-40-05-0G-0;[03] VERIFIED STEPS 1 AND 2;[04] OK TO TREAT AND PRIME HOLES;[05] TREATED AND APPLIED PRIMER AT BAFFLE AT FWD CARGO COMPARTMENT BETWEEN FS 400-420 STR 26L WL 206 IN REF B737-700 SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804;[06] VERIFIED STEP 5;[07] OK TO INSTALL BAFFLE;[08] INSTALLED NEW BAFFLE AT FWD CARGO COMPARTMENT BETWEEN FS 400-420 STR 26L WL 206 IN REF B737-700 SRM 51-40-02-0G-0;[09] REMOVED BAFFLE AT FWD CARGO COMPARTMENT BETWEEN FS 400-420 STR 26L WL 206 IN REF B737-700 SRM 51-40-02-0G-0;LOCATED AND DRILLED BAFFLE AT FWD CARGO COMPARTMENT BETWEEN FS 400-420 STR 26L WL 206 IN REF B737-700 SRM 51-40-05-0G-0;INSTALLED NEW BAFFLE AT FWD CARGO COMPARTMENT BETWEEN FS 400-420 STR 26L WL 206 IN REF B737-700 SRM 51-40-02-0G-0;[10] VERIFIED STEPS 8 AND 9

Part: PANEL — CORRODED (AFT CARGO) · airframe 75,107 hrs · 44,385 cycles

CORROSION.....AFT CARGO COMPARTMENT AFT BULKHEAD PANEL 141UW HAS EXFOLIATED CORROSION. / [01] RECEIVED NEW AFT CARGO PANEL 141 UW; NEW PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00ASNPF;[02] VERIFIED STEP 1.

Part: STRIP — ELONGATED (AFT CARGO) · airframe 75,107 hrs · 44,385 cycles

AFT CARGO L/H CAP STRIPS P/N 453A2611-10 AND 543A2611-4 HOLES ELONGATED / [01] RECEIVED NEW CAP STRIPS P/NS 453A2611-10 AND 453A2611-4; NEW CAP STRIPS TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004GEP0;[02] VERIFIED STEP 1.

Part: STRIP — ELONGATED (AFT CARGO) · airframe 75,107 hrs · 44,385 cycles

AFT CARGO L/H CAP STRIP P/N 453A2611-8 WITH HOLES ELONGATED / [01] RECEIVED NEW AFT CARGO CAP STRIP P/N 453A2611-8; NEW STRIP TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004GEP0; T/C 5360-E-16462-NG;[02] VERIFIED STEP 1.

Part: CAP SEAL — ELONGATED (AFT CARGO) · airframe 75,107 hrs · 44,385 cycles

AFT CARGO R/H CAP STRIPS WITH HOLES ELONGATED / [01] RECEIVED NEW AFT CARGO CAP STRIPS 2 EACH ;P/N 453A2611-11 AND 453A 2611-9; NEWS CAP STRIPS TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004GEPO; 5360-E-16462-NG;[02] ORRECTION RECEIVED NEW AFT CARGO CAP STRIPS 2 EACH ;P/N 453A2611-11 AND 453A 2611-9; NEWS CAP STRIPS TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004GEP0; 5360-E-16462-NG;[03] VERIFIED STEP 2.

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 75,107 hrs · 44,385 cycles

FWD CARGO COMPARTMENT RH Z CHANNEL STA 400 TO STA 420 HAS SPOTS OF CORROSION AT HOLE SCREW. CORRODED AROUND HOLES AUTOMATICALLY OUT OF LIMITS / [01] LOCATED AND DRILLED R/H ZEE CHANNEL REF. B737-7 SRM 51-40-05-0G-0;[02] VERIFIED STEP 1;[03] OK TO TREAT AND PRIME;[04] TREATED AND PRIMED ZEE CHANNEL REF. B737-7 SRM 51-20-01-0G-0;[05] VERIFIED STEP 4;[06] INSTALLED NUT PLATES REF. B737-7 SRM 51-40-02-0G-0; AND BOEING DRAWING#143A7500;[07] FABRICATED FWD CARGO COMPARTMENT R/H ZEE <BR>CHANNEL STA. 400 TO STA. 420; REF; USED B737-7 SRM 51-40-05-0G-0; 51-20-01-0G-0; 51-40-02-0G-0; AND DRAWING #143A7500. BEING INSTALLED ON TASK CARD #TTG8Q004E0QK;[08] VERIFIED STEP 6 AND 7

Part: STRAP — CORRODED (FWD CARGO) · airframe 75,107 hrs · 44,385 cycles

FWD CARGO COMPARTMENT LH AFT STRAP SUPPORT HAS SEVERAL SPOTS OF CORROSION. / [01] LOCATED AND DRILLED L/H AFT STRAP REF. B737-7 SRM 51-40-05-0G-0;[02] VERIFIED STEP 1. OK TO TREAT AND PRIME.;[03] TREATED AND PRIMED STRAP FASTENER HOLES REF. B737-7 SRM 51-20-01-0G-0;[04] REPLACED FWD CARGO COMPARTMENT L/H SUPPORT ASSEMBLY (STRAP); RECEIVED NEW ON ISSUE TAG#LY522; P.O.# 1758680; WILL BE INSTALLED ON TASK CARD #TTG8Q00BKCRJ;[05] VERIFIED STEPS 3 AND 4.

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 75,107 hrs · 44,385 cycles

FWD CARGO COMPARTMENT LH Z CHANNEL STA 400 TO STA 500D HAS SEVERAL SPOTS OF CORROSION AT HOLE SCREW. CORROSION AT HOLES AUTOMATICALLY OUT OF LIMITS / [01] LOCATED AND DRILLED L/H ZEE CHANNEL STA.400 TO STA.500D REF. B737-7 SRM 51-40-05-0G-0;[02] VERIFIED STEP 1<BR><BR>OK TO TREAT AND PRIME HOLES;[03] TREATED AND PRIMED ZEE CHANNEL REF. B737-7 SRM 51-20-01-0G-0;[04] VERIFIED STEP 3;[05] INSTALLED NUT PLATES ON ZEE CHANNEL REF. BOEING DRAWING #143A7500;[06] FABRICATED FWD CARGO COMPARTMENT L/H ZEE CHANNEL STA. 400 TO STA. 500D; REF; USED B737-7 SRM 51-40-05-0G-0; 51-20-01-0G-0; AND DRAWING #143A7500. BEING INSTALLED ON TASK CARD #TTG8Q004E0QK;[07] AND B737-7 SRM 51-40-02-0G-0;[08] ACTION: VERIFIED STEP 6 AND 7

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 75,107 hrs · 44,385 cycles

FWD CARGO COMPARTMENT RH Z CHANNEL STA 500A TO STA 500D HAS SEVERAL SPOTS OF CORROSION AT HOLE SCREW. CORROSION AT HOLES AUTOMATICALLY OUT OF LIMITS / [01] LOCATED AND DRILLED R/H ZEE CHANNEL REF. B737-7 SRM 51-40-05-0G-0;[02] VERIFIED STEP 1;[03] OK TO TREAT AND PRIME;[04] TREATED AND PRIMED ZEE CHANNEL REF. B737-7 SRM 51-20-01-0G-0;[05] VERIFIED STEP 4;[06] INSTALLED NUT PLATES ON ZEE CAHENNEL REF. BOEING DRAWING 143A7500 AND B737-7 SRM 51-40-02-0G-0;[07] FABRICATED FWD CARGO COMPARTMENT R/H ZEE <BR>CHANNEL STA. 500A TO STA. 500D; REF; USED B737-7 SRM 51-40-05-0G-0; 51-20-01-0G-0; 51-40-02-0G-0; AND DRAWING #143A7500. BEING INSTALLED ON TASK CARD #TTG8Q004E0QK;[08] ACTION: VERIFIED STEP 6 AND 7

Part: SPLICE — CORRODED (AFT CARGO) · airframe 75,107 hrs · 44,385 cycles

AFT CARGO COMPARTMENT STA 767 SPLICER HAS SURFACE CORROSION / [01] REMOVED CORROSION ON FLOOR SPLICE STRAP PER REF. 737SRM 51-10-02-0G-0;[02] CORROSION PASS THROUGH OUT OF LIMITS PER SRM 53-00-53-1A-2;[03] VALIDATED STEPS 1 & 2;[04] RECEIVED NEW FLOOR SPLICE 'T' P/N 146A9401-4; NEW SPLICE TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004GEP0;[05] VERIFIED STEP 1.;[06] CORRECTION STEP 5. VERIFIED STEP 5.;[07] CORRECTION STEP 5 AND 6. VERIFIED STEP 4.

Part: ANGLE — CORRODED (FWD FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

FLIGHT COMPARTMENT ENTRANCE; FLOOR AREA BS259.5 TO BS 270 BL 0 WL 208 AREA WITH CORROSION / [01] INSTALLED EWIS PROTECTION AT FLOOR STRUCTURE FLIGHT DECK ENTRANCE BETWEEN BS259.5 TO BS270 BL 0 WL208 AS PER B737-7 AMM 20-60-07-913-801.[21] FABRICATED AND DRILLED NEW ANGLE REPAIR 7075-O; 0.063'; ACCOMPLISHED ROUGHNESS TEST 63 RA PER REF SRM 51-20-13-0G-0 TOOL P/N 171854; NO CALIBRATION DUE <BR>NEW ANGLE REPAIR FABRICATION IS FLAT NO REQUIRE MATCH CONTOUR;[22] VERIFIED 21;[23] REMOVED EWIS PROTECTION AT FLIGHT COMPARTMENT ENTRANCE FLOOR AREA REF USED B737-7 AMM 20-60-07-913-801;[24] ACCOMPLISHED LATERAL INTERCOSTAL REPAIR AT FLIGHT COMPARTMENT ENTRANCE AT STA 270 BETWEEN RBL-11 TO LBL-11 REF ADD 22-153-01100- REV A WIP#1;2 AND #3;[25] VERIFIED STEP 24;[26] VERIFIED STEP #23

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

STRINGER 27L SPLICE AT STA. 370 CORRODED / [01] REMOVED CORROSION ON STR27L SPLICE STA. 370; REF. B737-7 SRM 51-10-02-0G-0;[02] ORIGINAL MATERIAL 0.045'; MATERIAL REMOVED 0.022'; MATERIAL REMAINING 0.023' FOUND OUT OF LIMITS REF. B737-7 SRM 53-00-03-1A-1;[03] RECEIVED NEW STRINGER SPLICE TAG#E108134; P.O.#1763933; SPLICE BEING INSTALLED ON TASK CARD # TTG8Q00BFJRL;[04] VERIFIED STEPS 1; 2 AND 3

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

STRINGER 25L SPLICE AT STA. 370 CORRODED / [01] REMOVED CORROSION ON STR25L SPLICE STA. 370; REF. B737-7 SRM 51-10-02-0G-0;[02] ORIGINAL MATERIAL 0.045'; MATERIAL REMOVED 0.018'; MATERIAL REMAINING 0.027' FOUND OUT OF LIMITS REF. B737-7 SRM 53-00-03-1A-1;[03] LOCATED AND DRILLED NEW SPLICE; AT STRINGER 27L ; BETWEEN STA. 360 AND STA. 380; PER REF 737 -700 SRM 51-40-05-0G-0;[04] STRINGER SPLICE BETWEEN STA. 360 AND STA. 380; AT STRINGER 25L WAS REMOVED ON CUSTOMER BAR CODE TTG8QOOBFG5E;[05] CORRECTION STRINGER SPLICE BETWEEN STA. 360 AND STA. 380; AT STRINGER 25L WAS REMOVED ON CUSTOMER BAR CODE TTG8Q00BFG5E;[06] VERIFIED STEPS 1; 2; 3; 4 AND 5. OK TO TREAT AND PRIME SPLICE AND AIRCRAFT SKIN.;[07] LATE ENTRY: RECEIVED NEW STRINGER SPLACE ISSUE TAG#WN14497 PO#1758680;[08] TREATED AND PRIME STRINGER SECTION;SPLACE AND AIRCRAFT SKIN HOLES REF B737-7 SRM 51-20-01-0G-0;[09] THIS SPLICE WILL BY INSTALLED ON CARD #TTG8Q00BFG5E;[10] VERIFIED STEPS 7;8 AND 9.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

STRINGER 26L CORRODED FWD OF STA. 370 SPLICE / [01] FOUND CORR. ON STRINGER 26L; OUT OF LIMITS; CORRODED THRU; REF. B737-7 SRM 53-00-03-1A-1;[15] INSTALLED NEW STRINGER SECTION 26 L ; FROM STA. 294.4 TO STA. 360; PER REF 737-700 SRM 51-40-02-0G-0 AND DRAWING 141A3532; PENDING TO INSTALL FASTENERS UNDER CHOIRING;(6 EACH);[16] VERIFIED SQUEEZE OUT AND FASTENER INSTALLATION ON STRINGER 26L FROM STA. 294.4 TO STA. 360 ON 04/03/22; AT 22:30; PER REF SOPM 20-50-19;[17] VERIFIED STEPS 15 AND 16.;[18] OK TO INSTALL 3 WEBS AT 26L THAT WAS REMOVED ON T/C TTG8Q00BDSJ2 STEPS 21 AND STEP 25.;[19] INSTALLED 3 WEB AT STRINGER 26 L ; THAT WAS REMOVED ON TTG8Q00BDSJ2 PER REF. 737-700 SRM 51-40-02-0G-0 AND DRAWING 143A7505;[20] VERIFIED STEP 19.;[21] COMPLETE INSTALLATION OF STRINGER 26 L FROM STA. 294.4 TO STA. 360 PER REF 737-700 SRM 51-40-02-0G-0 AND DRAWING 141A3502; 141A3532;[22] REMOVED AND REPLACED STRINGER 26 L SECTION; FROM STA. 294.4 TO STA. 360 PER REF. 737-700 SRM 51-40-02-0G-0 AND DRAWINGS 141A3502 AND 141A3532;[23] VERIFIED STEPS 21 AND 22.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

STRINGER 26L SPLICE AT STA. 370 CORRODED / [01] REMOVED CORROSION ON STR26L SPLICE STA. 370; REF. B737-7 SRM 51-10-02-0G-0;[02] ORIGINAL MATERIAL 0.045'; MATERIAL REMOVED 0.020'; MATERIAL REMAINING 0.025' FOUND OUT OF LIMITS REF. B737-7 SRM 53-00-03-1A-1;[03] FABRICATED STRINGER SPLICE MATERIAL USED BAC1498-285-7075 PO#1763843 REF DWG#141A3341-12;[04] VERIFIED STEP 1; 2 AND 3;[05] HEAT TREATED STRINGER SPLICE TO 7075-T62 CONDITION REF. BAC5602 TAG #405072;[06] FABRICATED STRINGER SPLICE MATERIAL USED BAC1498-285-7075 PO#1763843; AND HEAT TREATED TO T62 CONDITION; TAG #4050072; REF USED BOEING DWG #141A3341; STRINGER SPLICE BEING INSTALLED ON TASK CARD # TTG8Q00BDSJ2;[07] VERIFIED STEPS 5 AND 6

Part: STRINGER — CORRODED (FWD FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

STRINGER 27L CORRODED FWD OF STA. 370 SPLICE / [01] FOUND CORR. ON STRINGER OUT OF LIMITS; CORRODED THRU; REF. B737-7 SRM 53-00-03-1A-1;[02] REMOVED FASTENERS BETWEEN STA 300 TO STA 326 STR 27L FORM AIRCRAFT SHORING ACCESS REF B737-7 SRM 51-40-02-0G-0;[03] VERIFIED STEPS 1 AND 2;[04] REMOVED STRINGER SECTION FROM STA. 294.4 TO STA 370; STRINGER 27L PER REF. 737-700 SRM 51-40-02-0G-0;[05] VERIFIED STEP 4.;[06] PERFORMED DVI INSPECTION OF AREA REMOVED INTERCOSTAL AT STR 27L BETWEEN STA 360-380; NO ADDITIONAL DAMAGES FOUND;[07] LOCATED AND DRILLED NEW STRINGER SECTION FROM STA 294.4 TO STA 370 PER REF 737-700 SRM 51-40-02-0G-0;[08] CORRECTION LOCATED AND DRILLED NEW STRINGER SECTION FROM STA 294.4 TO STA 370 PER REF 737-700 SRM 51-40-05-0G-0;

Part: CHANNEL — CORRODED (AFT CARGO) · airframe 75,107 hrs · 44,385 cycles

AFT CARGO R/H Z CHANNEL FROM STA 727 TO STA 767; RBL 33.5 AND WL 156.4 WITH DEEP CORROSION AT NUT PLATE HOLES / [01] REMOVED CORROSION ON AFT CARGO Z CHANNEL FROM STA 727 TO STA 767 I.A.W. SRM 51-10-02-0G-0; OUT OF LIMITS PASS THROUGH.;[02] CORRECTION TO STEP 1; OUT OF LIMITS; PASS THROUGH I.A.W SRM 53-00-53-1A-2.;[03] VERIFIED STEPS 1 AND 2.;[04] LOCATED AND DRILLED NEW R/H 'Z' CHANNEL; FROM STA: 727' TO STA: 767'; PER REF. B737 SRM 51-40-05-0G-0;[05] VERIFIED STEP 4. OK TO TREAT AND PRIME Z CHANNEL.;[06] TREATED AND PRIMED NEW Z CHANNEL; PER REF. B737 AMM 51-21-41-370--802 AND 51-21-72-370-804;[07] VERIFIED STEP #6. OK TO INSTALL NUTPLATES.;[08] INSTALLED NUT PLATES ON NEW 'Z' CHANNEL; PER REF. B737 SRM 51-40-02-0G-0;[09] VERIFIED STEP 8;[10] REMOVED CORROSION ON AFT CARGO Z CHANNEL; FROM STA 727 TO STA 767; I.A.W. SRM 51-10-02-0G-0; OUT OF LIMITS PASS THROUGH I.A.W SRM 53-00-53-1A-2; LOCATED AND DRILLED NEW R/H 'Z' CHANNEL; FROM STA: 727' TO STA: 767'; PER REF. B737 SRM 51-40-05-0G-0; TREATED AND PRIMED NEW Z CHANNEL; PER REF. B737 AMM 51-21-41-370--802 AND 51-21-72-370-804; INSTALLED NUT PLATES ON NEW 'Z' CHANNEL; PER REF. B737 SRM 51-40-02-0G-0;[11] VERIFIED STEP 10

Part: SHIELD — CORRODED (FWD CARGO) · airframe 75,107 hrs · 44,385 cycles

FWD CARGO;CARGO DOOR SURROUND STRUCTURE AFT SHIELD CORRODED AT TOP SURFACE. / [01] REMOVED CORROSION ON AFT SHIELD REF. B737-7 SRM 51-10-02-0G-0 FOUND SEVERAL CRACKS ON PANEL OUT OF LIMITS REF. B737-7 SRM 53-30-15-1A-1;[02] RECEIVED NEW SHIELD AT FWD CARGO COMPARTMENT CUT-OUT DOOR AFT SECTION P/N 143A9403-188 AAR ISSUE TAG LY525 P.O # 1758680;THIS PART WAS REMOVED AND WILL BE INSTALL ON TASK CARD TTG8Q00BFPWX;[03] VERIFIED STEPS 1 AND 2

Part: CHANNEL — CORRODED (AFT CARGO) · airframe 75,107 hrs · 44,385 cycles

AFT CARGO COMPARTMENT L/H Z CHANNEL FROM STA. 727 TO STA 847 AT NUT PLATE HOLES WITH DEEP CORROSION / [01] REMOVED CORROSION ON AFT L/H CARGO Z CHANNEL FROM STA 727 TO STA 847 I.A.W. SRM 51-10-02-0G-0; OUT OF LIMITS PASS THROUGH I.A.W 53-00-53-1A-2.;[02] VERIFIED STEP 1.;[03] LOCATED AND DRILLED NEW L/H 'Z' CHANNEL; FROM STA: 727' TO 847'; PER REF. B737 SRM 51-40-05-0G-0;[04] VERIFIED STEP 3. OK TO TREAT AND PRIME.;[05] TREATED AND PRIMED NEW L/H 'Z' CHANNEL; FROM STA: 727 TO 847; PER REF. B737 AMM 51-21-41-370-802 AND 51-21-72-370-804;[06] VERIFIED STEP 5. OK TO INSTALL NUT PLATES.;[07] INSTALLED NUT PLATES ON L/H Z CHANNEL PER REF 737 SRM 51-40-02-0G-0 AND DRAWING 146A7502;[08] VERIFIED STEP 7.;[09] FABRICATED NEW L/H Z CHANNEL AT AFT CARGO COMPARTMENT BETWEEN STA 727 TO STA. 847 RBL 33.5 AND WL 156.4; PER REF. 737-700 SRM 51-40-02-0G-0 AND DRAWING # 146A7502;[10] VERIFIED STEP 9.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

PANEL 193AR HAS SEVERAL HOLE SCREWS ELONGATED / [01] PREPARED FOR REPAIR AT PANEL 193 AR AS PER B 737-700 SRM 51-70-06-2R-9;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED AT PANEL 193AR ;AS PER B737-700 SRM 51-70-06-2R-9 MATERIAL USED PO.1690463 AND PO.1760049;[04] VERIFIED STEP 3...O.K. TO PAINT AREA..;[05] APPLIED TOPCOAT TO PANEL 193AR REPAIRED AREAS AS PER B737-700 AMM 51-21-73-370-804;[06] REPAIRED AT PANEL 193AR ;AS PER B737-700 SRM 51-70-06-2R-9 MATERIAL USED PO.1690463 AND PO.1760049;[07] VERIFIED STEP 5 AND 6

Part: HANDLE — CRACKED (R1 DOOR) · airframe 75,107 hrs · 44,385 cycles

MAIN CABIN R/H EMERGENCY EXIT DOOR HANDLE IS CRACK / [01] REMOVED AND REPLACED R/H EMERGENCY EXIT DOOR HANDLE ASPER B737-700 AMM 52-22-51-000-801;[02] VERIFIED STEP 1

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

STRINGER 25L CORRODED BETWEEN BS 360 & 380. REMOVED FASTENERS IAW SRM 51-40-02-0G-0. REMOVED STRINGER SPLICE IAW SRM 51-40-02-0G-0. FOUND S25L OUT OF LIMITS IAW SRM 53-00-03-1A-1. LOCATED & DRILLED A NEW STRINGER IAW SRM 51-40-02-0G-0. TREATED & PRIMED STRINGER & SPLICE IAW SRM 51-20-01-0G-0 & 53-00-03-2R-1 STEP 4. I & J. INSTALLED STRINGER REPAIR IAW SRM 53-00-03-2R-1; REP. 1 FIG.5, INSTALLED NEW SPLICE IAW SRM 53-00-03-2R-1.

Part: STRAP — CORRODED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

T FLOOR SPLICE AT STA 727D + 5 WITH DEEP CORROSION. / [01] FOUND EXFOLIATE CORROSION ON FLOOR SPLICE STRAP AT STA 727 D +5; OUT OF LIMITS PER REF 737 -700 SRM 53-00-53-1A-2;[02] VERIFIED STEP 1.;[03] RECEIVED NEW FLOOR SPLICE STRAP P/N 146A9401-8; NEW STRAP TO BE INSTALLED ON TTG8Q004GEP0 T/C 5360-E-16462-NG;[04] VERIFIED STEP 3;CARD COMPLETED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

FOUND STR27L WITH EXFOLIATING CORROSION BETWEEN STA.360 & STA.380 STRINGER 27L FROM STA 370 SPLICE TO AFT / [01] REMOVED FASTENERS AND EXISTING STRINGER SPLICE AT FUSELAGE SKIN S-27L BETWEEN STA 351.2 AND STA 380 REF B7373-700 SRM 51-40-02-0G-0.;[24] INSTALLED STRINGER 27 L SPLICE REPAIR AT STA 410 PER REF 737-700 SRM 53-00-03-2R-1 REPAIR 1;[25] VERIFIED STEP 24.;[26] CUT-OUT DAMAGE SECTION OF STRINGER 27L FROM SPLICE AT STA 370 TO STA 410;INSTALLED NEW SECTION AND SPLICE REPAIR REF USED B737-7 SRM 53-00-03-2R-1 FIG 205 DETAIL A-A;51-40-02-0G-0 AND DWG#143A3230;[27] CLEAN AND CIC APPLICATIONS WILL BY ACCOMPLISHED 0N CARD#TTG8Q00BVL99 AND PAINT CARD#TTG8Q00BVU6A;[28] VERIFIED STEPS 26 AND 27;[29] COMPLIED WORK PERFORMED AND REINSTALL AREAS OPEN

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

ACCESS PANEL 431ER SKIN CORNER SECTION DELAMINATED / [01] PREPARED FOR REPAIR AT PANEL 431ER AS PER B 737-700 SRM 51-70-04-2R-13;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED AT PANEL 431 ER AS PER B 737-700 SRM 51-70-04-2R-13 MATERIAL USED PO.1690463 PO.1760049;[04] VERIFIED STEP 3 O.K. TO PAINT AREA;[05] APPLIED TOPCOAT TO REPAIRED AREA AS PER B737-700 AMM 51-21-73-370-804;[06] REPAIRED AT PANEL 431 ER AS PER B 737-700 SRM 51-70-04-2R-13 MATERIAL USED PO.1690463 PO.1760049;[07] VERIFIED STEP 5 AND 6

Part: FLOOR PANEL — ELONGATED (FWD CARGO) · airframe 75,107 hrs · 44,385 cycles

FWD CARGO COMPARTMENT FLOOR PANEL 120AF; HOLES ENLONGATED / [01] FABRICATED FWD CARGO COMPARTMENT FLOOR PANEL 120AF AS PER B737-700 AMM 25-52-01-201-801;[02] VERIFIED STEP 1

Part: FLOOR PANEL — FRAYED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

MAIN CABIN FLOOR PNL 241DF ;TOP SURFACE FRAYED ON GLASS FABRIC ALONG THE WHOLE PANEL. / [01] PERFORMED VISUAL INSPECTION AT FLOOR PANEL #241DF FOUND OUT LIMITS AS PER B-737 SRM53-00-50-1A-1;[02] VERIFIED STEP 1;[03] REMOVED CENTER PANEL 241 DF AS PER B737-700 AMM 53-21-00-000-801;[04] VERIFIED STEP 3;[05] RECEIVE NEW FLOOR PANEL 241 DF;[06] OK TO INSTALL FLOOR PANEL;[07] INSTALLED MAIN CABIN FLOOR PANEL 241DF AS PER B737-700 AMM 53-21-00-400-801;[08] THIS STEP WAS ENTER IN ERROR;[09] STEP 8 WAS SIGNED IN ERROR.;[10] VERIFIED STEPS 7 AND 8.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

ACCESS PANEL 193CL SCREW HOLES ENLONGATED / [01] PREPARED FOR REPAIR AT PANEL 193 CL AS PER B737- SRM 51-70-06-2R-9;[02] VERIFIED STEP #1.;[03] REPAIRED AT PANEL 193 CL AS PER B 737-700 SRM 51-70-06-2R-9 MATERIAL USED PO.1690463 ;PO. 1760049;[04] VERIFIED STEP 3. OK TO TOP COAT REPAIR AREA;[05] PAINTED ACCESS PANEL 193CL SCREW HOLES AS PER B727 - AMM<BR>51-21-73- 370-803;[06] CORRECTION STEP 5; PAINTED ACCESS PANEL 193CL SCREW HOLES AS PER B737 - AMM 51-21-73- 370-803.;[07] VERIFIED STEP 6.

Part: FLOOR PANEL — FRAYED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

MAIN CABIN FLOOR PNL 231XF ;TOP SURFACE FRAYER ON GLASS FABRIC ALONG THE WHOLE PANEL. / [01] PERFORMED VISUAL INSPECTION AT CABIN FLOOR PANEL #231XF FOUND OUT LIMITS AS PER B-737 SRM 53-00-50-1A-1.;[02] VERIFIED STEP 1;[03] OK TO INSTALL FLOOR PANEL;[04] REMOVED AND REPLACED MAIN CABIN FLOOR PANEL #231XF ASPER B737-700 AMM 53-21-00-21;[05] VERIFIED STEP 4

Part: PANEL — DETERIORATED (AFT CARGO) · airframe 75,107 hrs · 44,385 cycles

AFT CARGO ;FWD BULKHEAD PNL 142MW DETERIORATED. / [01] FABRICATED NEW AFT CARGO BULKHEAD PANEL 142MW IAW B737 AMM 25-52-01-201-801. USED REMOVE LINER AS A TEMPLATE.;[02] VERIFIEED STEP 1.

Part: PANEL — DETERIORATED (AFT CARGO) · airframe 75,107 hrs · 44,385 cycles

AFT CARGO ;FWD BULKHEAD PNL 141KW DETERIORATED. / [01] FABRICATED NEW AFT CARGO FWD BULKHEAD PANEL 141KW; USED OLD PANEL AS A TEMPLATED I.A.W B737 AMM 25-52-01-201-801.;[02] VERIFIED STEP 1.

Part: FITTING — LOOSE (R1 DOOR) · airframe 75,107 hrs · 44,385 cycles

CABIN PASSENGER R1 DOOR GIRT BAR FWD FITTING LOOSE / [01] REMOVED AND REPLACED (2) SCREWS AT CABIN PASSENGER R1 DOOR GIRT BAR FWD FITTING ASPER B 737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP COMPLETED

Part: FLOOR PANEL — DETERIORATED (AFT CARGO) · airframe 75,107 hrs · 44,385 cycles

AFT CARGO;FLOOR PNL 140BF DETERIORATED. / [01] FABRICATED NEW AFT CARGO FLOOR PANEL 140 BF; PER 737-700 AMM 25-52-01-201-801;USING REMOVED LINER AS ATEMPLATE;[02] VERIFIED STEP 1.

Part: FLOOR PANEL — DETERIORATED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

AFT CARGO ;FLOOR PNL 140AF DETERIORATED. / [01] FABRICATED NEW AFT CARGO FLOOR PANEL; USED REMOVED LINER AS A TEMPLATE ;PER REF. B737 AMM 25-52-01-201-801;[02] VERIFIED STEP 1

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

LOWER FUSELAGE BETWEEN ST25 TO ST26; STA360 TO STA380 SKIN AREAS BULGING STRINGER 26L CORRODED FROM STA 370 SPLICE TO AFT. SKIN BULGING DUE TO STR 26L EXFOLIATED CORROSION FOUND. / [01] REMOVED PAINT BY STRIPPING AT LOWER FUSELAGE SKIN BETWEEN STA 351.2 AND STA 380 S-27L- S-25L REF B737-700 AMM 51-21-11-150-810.;[34] LOCATED AND DRILLED NEW STRINGER SECTION FROM STA 370 TO STA 410 STR 26L REF B737-7 SRM 53-00-03-2R-1 STEP 4.F AND 51-40-05-0G-0;[35] CORRECTION <BR>LOCATED AND DRILLED NEW STRINGER SECTION FROM STA 370 TO STA 410 STR 26L REF B737-7 SRM 53-00-03-2R-1 STEP 4.F AND 737 SRM 51-40-05-0G-0;[36] (RII) VERIFIED STEPS 34 AND 35.;FABRICATED STRINGER SPLACE AT STR 26L BETWEEN STA 400 TO STA 420 MATERIAL USED BAC1498-116-707562 PO#1760435 REF B737-7 SRM 53-00-01-2R-1 TYPE 1 TABLE 204 FIG 205DETAIL A-A AND SHIMS MATERIAL USED 2024-T3 0.025" 38.LOCATED AND DRILLED STRINGER SPLACE AND SHIMS REF B737-7 SRM 53-00-01-2R-1 AND 51-40-05-0G-0

Part: FLOOR PANEL — FRAYED (FUSELAGE) · airframe 75,107 hrs · 44,385 cycles

MAIN CABIN FLOOR PNL 241AF ;TOP SURFACE FRAYER ON GLASS FABRIC ALONG THE WHOLE PANEL. / [01] ACCOMPLISHED VISUAL INSPECTION AT FLOOR PANEL #241AF FOUND OUT LIMITS AS PER B-737 SRM 53-00-50-1A-1.;[02] VERIFIED STEP 1;[03] REMOVED CENTER PANEL 241 AF AS PER B737-700 AMM 53-21-00-000-801;[04] OK TO INSTALL FLOOR PANEL;[05] INSTALLED MAIN CABIN FLOOR PANEL 241 AF AS PER B737-700 AMM 53-21-00-400-801;[06] VERIFIED STEP 5

Part: BRACKET — BROKEN (L/H WING) · airframe 75,107 hrs · 44,385 cycles

ACCESS PANEL 551FB FIXED PANE: T/E L BRACKET CRACK / [01] REMOVED AND REPLACED 'L' BRACKET ON L/W T/E PANEL #551FB REF. B737-7 SRM 51-40-02-0G-0; AND DRAWING 115A2710;[02] VERIFIED STEP 1

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,513 hrs · 44,015 cycles

LH EMERGENCY AREA LIGHT AT ROW 24ABC INOP ; / [01] RELAMPED EMERG AREA LIGHT AT ROW 24ABC. OPS CHECK GOOD.

Part: HOOK — OUT OF ADJUST (L1 DOOR) · airframe 74,286 hrs · 43,890 cycles

SUPPLEMENTAL INFORMATION: FORWARD ENTRY DOOR SLIDE GIRT BAR RETAINER (LEFT SIDE) IS LOOSE ; / [01] ADJUSTED FWD ENTRY DOOR SLIDE LEFT ?J? HOOK IN REF TO S.I.P. GIRT BAR RETENTION OKAY FOR CONTINUED SERVICE.

Part: SIGN — LOOSE (CABIN) · airframe 74,069 hrs · 43,765 cycles

EMERGENCY EXIT SIGN FELL OFF BRACKET AND IS HANGING ; / [01] UPDATED PARTS INFORMATION REMOTELY; [02] R&R'D EMERGENCY EXIT SIGN ASSY PER AMM 33-51-01

Part: WIRE HARNESS — OUT OF TOLERANCE (NR 2 EGT) · airframe 73,557 hrs · 43,451 cycles

#2 ENGINE EGT EXCEEDANCE ON CLIMBOUT BETWEEN 5-10 SECONDS. ; / [01] #2 ENGINE EXCEEDED EGT 960 FOR 7 SEC ON TAKEOFF. FOUND TO BE IN AREA A PER M/M 71-00-00. PER POWER PLANT ENGINEERING FIRST OCCURRENCE OF EGT EXCEEDANCE AND SUSPECT FAULTY EGT INDICATION. FOUND FC 75-10832 T3 OUT OF RANGE AND FC 77-20872 T49.5 OUT OF RANGE. REMOVED AND REPLACED CJ10 HARNESS PER FIM 77-21-804 AND PERFORMED FIM 75-33-802. INSPECTED ENGINE PER 71-00-00 NO DEFECTS NOTED. RAN ENGINE WITH NO CURRENT EEC FAULTS.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 73,062 hrs · 43,173 cycles

LEFT WING O/B AFT FLAP HAS DELAMINATION AREA I/B TRAILING EDGE APPROXIMATELY 5 X 3. ; / [01] REMOVED AFT FLAP PER AMM 27-51-22; [02] OK TO INSTALL AFT FLAP REF AMM 27-51-22; [03] REMOVED AND REPLACED LT WING OUTBOARD AFT FLAP REF MM 27-51-22

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 73,062 hrs · 43,173 cycles

RT WING; O/B AFT FLAP DELAMINATED ON I/B TRAILING EDGE; TOP AND BOTTOM / [01] REMOVED OUTBOARD AFT FLAP PER M/M 27-51-22; [02] OK TO INSTALL OTBD AFT FLAP REF AMM 27-51-22; [03] REMOVED AND REPLACED RT WING O/B AFT FLAP REF MM 27-51-22

Part: SMOKE DETECTOR — INTERMITTENT (AFT LAVATORY) · airframe 71,040 hrs · 41,943 cycles

AFT LAV SMOKE DETECTOR INTERMMITENT/INOPERABLE. AFT LAV INOPERABLE, OK TO CONTINUE, PER MEL 26-16-01 SP1B TRAK NR 53937. R & R AFT LAV SMOKE DETECTOR UNIT, IAW AMM 26-14-01 CL NR 54400.

Part: CAP — CORRODED (BS 727-727D) · airframe 70,174 hrs · 41,385 cycles

CORROSION ON THE R/H CAP STRIP FROM BS 727 - 727D WL 156 RBL 21 HAS SEVERE CORROSION / REMOVED AND REPLACED R/H CAP STRIP PO#789923/1 P/N 453A2611 IAW DWG 453A2600 REV.D 57049U 13APR2020

Part: SUPPORT ANGLE — CRACKED (BS 867) · airframe 70,174 hrs · 41,385 cycles

AFT CARGO BAY WASTE TANK ENCLOSURE SUPPORT ANGLE IS CRACKED; BS 867 LBL 10 WL 156 / ACB WASTE TANK ENCLOSURE SUPPORT ANGLE IS GOING TO BE CHANGED ON NON ROUTINE CARD 725002 FUSELAGE 5170; DEFECT NO.U136941; (COPY ATTACHED).

Part: ANGLE — CRACKED (BS 847) · airframe 70,174 hrs · 41,385 cycles

CRACK SUPPORT BRACKET P/N149A8109-114 AT ACB BULKHEAD SUPPORT STA 847 + 18'; LBL 10 WL 165. / LOCATED AND DRILLED NEW ANGLE P/N 149A8109U114; IAW B737-700 SRM 51-40-05-0G-0; FIG.2. AND BOEING DWG. #149A8102; REV.A. REMOVED AND REPLACED ANGLE IAW B737 SRM 51-40-02-0G-0; BOEING DWG.# 149A8102 REV.A AND 149A8104 REV.B.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 70,174 hrs · 41,385 cycles

AFT CARGO BAY; FWD SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO BAY FWD SCUFF PLATE IAW EA NO: 1-A53-2076. REV 11.

Part: ATTACH BOLT — WORN (VERTICAL STAB) · airframe 70,174 hrs · 41,385 cycles

VERTICAL STAB L/H PRIMARY ATTACH POINT BOLT IS WORN / REPLACED VERTICAL STAB 44 PRIMARY ATTACH BOLT; INSTALLATION OF BOLT TO BE ACCOMPLISHED ON CUSTOMER CARD # 753-480-00-00 REV 1

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

***CORROSION*** ON FCB- AFT BULKHEAD CENTER ANGLE STA 500D; RBL 20-LBL 20. WL 156. / LOCATED AND DRILLED B/H COUTER ANGLE STA.500D RBL20- LBL20 PER SRM 51-40-05 AND DWG.143A9481. WILL BE INSTALLED ON CUSTOMER CARD #U136757. 91195U; 3-27-20 .

Part: SHIELD — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

SUPPLEMENTAL INFORMATION: ***CORROSION*** ON FCB SHIELD STA 492 - 500A; RBL 24 WL 156. / REPLACED SHIELD AT B/S492-B/S 500A RBL24 WL156 IAW SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 143A0080 REV:- 59900U 01APR-20

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

FWD CARGO BAY INTERCOSTAL CRACKED AT FASTENER HOLE BETWEEN BS 500 - BS 500A RBL 24 WL 156 / REPLACED INTERCOSTAL AT B/S 500 - 500A RBL 24 WL 156 IAW SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 143A0080 REV:- 59900U 01APR-20

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

MULTIPLE AREAS OF MECHANICAL DAMAGE ON PASSENGER CABIN SEAT TRACK AT B.S. 480 - 522; L.B.L. 24.5; W.L. 208.1. / FOUND DAMAGED SEAT TRACK TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1 FIG 103. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK PER SRM 51-40-02-0G-0 PAR 4 & PAR. 7. AND SRM 51-40-05-0G-0 FIG 3 & FIG 4. AND BOEING DRAWING 143A5300 SH; 42 REV.A. SEAT TRACK REMOVED & REPLACED BS 480-BS 522 LBL 24.5

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

***CORROSION*** IN ACB; ON INTERCOASTAL AT RBL 21 STA 747 - 767 WL 156 / LOCATED; DRILLED AND INSTALLED INTERCOSTAL STA.724 - 767 RBL 21 PER SRM 51-40-02; SRM 51-40-05 AND DWG. 146A7502. 91195U 3-30-20

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

***CORROSION*** CORROSION ON MULTIPLE AREAS OF FLOOR TO SIDEWALL SUPPORT FROM BS 500 TO BS 500D; RBL 24; WL 156 / REMOVED CORROSION IN MULTIPLE AREAS ON FLOOR TO SIDEWALL SUPPORT FROM BS500A TO 500D RBL24; WL156 AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT PER SRM 51-40-02; SRM 51-40-05; AND DWG 143A7501. CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM BS495 TO 500A RBL24; WL156 ADDRESSED ON CUSTOMER CARD #U136811

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

***CORROSION*** CORROSION ON STRINGER CLIP AT BS 500A+8; RBL 6.5; WL 150 / REPLACED STRINGER CAP AT B/S 500A+8 RBL 6.5 WL 150 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 8 AND DWG 143A3230 REV:A 59900U 31MAR20

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

***CORROSION*** CORROSION ON STRINGER CLIP AT BS 500A+8; LBL 6.5; WL 150 / REPLACED STRINGER CLIP AT B/S 500A+8; LBL 6.5 WL 150 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 143A3230 REV:A 59900U 31MAR20

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

***CORROSION*** CORROSION ON STRINGER CLIP AT BS 500+11; LBL 6.5; WL 150 / REPLACED STRINGER CLIP AT B/S 500+11 LBL 6.5 WL 150 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 143A3230 REV:A 59900U 31MAR20

Part: SHIELD — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

***CORROSION*** FLOOR TO SIDEWALL SUPPORT HAS CORROSION AROUND 1 EA. FASTENER HOLE AT BS 436; RBL 24; WL 156 / REMOVED AND REPLACED A.C.B NEW SHIELD AT B/S 420-440 RBL 24 WL 156 P/N 143A8126U21 PO #766182/1 IAW SRM 51-40-02 AND DWG 143A0080 REV:- 5259899U1-4-70

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

***CORROSION*** CORROSION ON STRINGER CLIP AT BS 500+4; LBL 6.5; WL 150 / REPLACED STRINGER CLIP AT B/S 500+4; LBL 6.5 WL 150 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 143A3230 REV: A 59900U 31MAR20

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

***CORROSION*** CORROSION ON STRINGER CLIP AT BS 500A+15; RBL 6.5; WL 150 / REPLACED STRINGER CLIP AT B/S 500A+15; RBL 6.5 WL 150 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 143A3230 REV:A 59900U 31MAR20

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

***CORROSION*** CORROSION ON MULTIPLE AREAS OF FCB THRESHOLD FROM BS 440 TO BS 490; RBL 28; WL 156 / REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM CH 53-30-15-1A-1 REMOVED AND REPLACED WEB IAW SRM CH 51-40-02 AND DRAWING #143A8330.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

***CORROSION*** CORROSION ON STRINGER CLIP AT BS 500A+15; LBL 6.5; WL 150 / REPLACED STRINGER CLIP AT B/S 500A+15; LBL 6.5 WL 150 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 143A3230 REV:A 59900U 31MAR20

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

***CORROSION*** CORROSION ON MULTIPLE AREAS OF FLOOR TO SIDEWALL SUPPORT FROM BS 440 TO BS 500B; LBL 24; WL 156 / REMOVED F.C.B. BULKHEAD FLOOR SUPPORT B/S396 LBL24. RBL24 W.L.156 FDR ACCESS IAW. SRM 51-40-02-0G-0 REMOVED SIDEWALL SUPPORT FCB. FROM B/S396 TO B/S500D LBL24 WL156 IAW SRM 51-40-02-0G FABRICATED LOCATED AND DRILLED FLOOR TO SIDEWALL SUPPORT B/S 396-500 LBL24 WL156 FROM BAC1496-444 #7075T6 LOT#142869 PER DWG SRM 51-40-05 & DWG 5754899U27 AND DWG 143A7501 REV B & INSTALLED NEW SPLICE AND ALL REPAIR PARTS IAW SRM 53-00-53-2R-6 PARA 4-D FIG.202 4-9-2020 54826U

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

CRACKED FLOOR SUPPORT AT B.S. 540; R.B.L. 1 - R.B.L. 24.5; W.L. 208.1. / REMOVED CRACKED FLOOR SUPPORT BS540; RBL-1 TO RBL24 PER SRM 51-10-02-0G-0 PAR.9 AND SRM 51-40-02-0G-0 PAR.7 AND INSTALLED NEW FLOOR SUPPORT PER BOEING DRAWING 143A0060 SH.14 REV.B. SRM 51-40-05-0G-0 FIG 3;4 AND 6 AND SRM 51-40-02-0G-0 PAR. 4 AND 7.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM BS 867 TO BS 887; RBL 16; WL 156 / REMOVED CORROSION FROM SIDEWALL SUPPORT BS867-887 RBL16; WL156 1' X 3' X 0.014 PER SRM 51-10-02 ORIGINAL THICKNESS OF 0.050' FOUND TO OUT OF LIMITS PER SRM 51-10-02-0G-0 REMOVED PER SRM 51-40-02. FABRICATED REPLACEMENT PER SRM 51-40-05 AND DWG 146A7502 APPLIED CHEMICAL CONVERSION COATING ON PRIMER PER SRM 51-20-01 AND INSTALLED REPLACEMENT FLOOR TO SIDEWALL SUPPORT PER SRM 51-40-02-0G-0 ON DWG 146A2500 57627U 24MAR20

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

CORROSION ON INTERCOSTAL AT BS 787; RBL 6.5; WL 152 / INTERCOSTAT BS-787-807; RBL-6.5 WL-152 WAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG 103. FABRICATED AND LOCATED NEW INTERCOSTAL IAW DWG-146A8132 SH-17 & PL FROM 7075-0 LOT#8891881 HEAT TREATED TO T-62 PO# 789018. INSTALLED PER SRM 51-40-02 & DWG 146A8130 SHT-8

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 895; RBL 16; WL 156 / REPLACED FLOOR TO SIDEWALL SUPPORT AT BS880 TO 947 RBL16 WL156 IAW SRM 51-40-02 AND DRAWING 147A7500 DUE TO THE CORROSION 1' X 5' X 0.08' PER SRM 51-10-02-0G-0 ORIGINAL MAX THICKNESS IS 0.040' PER SRM 53-00-53-1A-2 FOUND TO BE BEYOND ALLOWABLE LIMITS PER SRM 53-00-53-1A-2 59861U 26MAR20

Part: STRAP — CORRODED (BS 887) · airframe 70,174 hrs · 41,385 cycles

CORROSION ON FLOOR STRAP AT BS 887; RBL 16 TO LBL 14; WL 156 / REMOVED DAMAGED FLOOR STRAP BS 887 RBL16-LBL 14 W/L 156; AND INSTALLED NEW STRAP IAW SRM 51-40-02-0G-0 AND DWG #146A7500

Part: BEAM — CRACKED (R1 DOOR) · airframe 70,174 hrs · 41,385 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. PER REMOVABLE STRUCTURAL COMPONENT REMOVAL REPORT, THE FWD SERVICE DOOR WAS REMOVED. CLOSED PER SA-M 735 MATTHEW IRVINE (E107304)

Part: SHIELD — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

CORROSION ON ACB LOWER MAIN SILL; FWD SHIELD FROM BS 767 TO BS 787; RBL 21; WL 156 / REMOVED CORROSION FROM ACB LOWER MAIN SILL; FWD SHIELD BS767-787 RBL21 2' X 1' X 0.06' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED DAMAGED SHEILD PER SRM 51-40-02. RECEIVED REPLACEMENT; LOCATED AND DRILLED PER SRM 51-40-05 AND DWG 146A8127. INSTALLED REPLACEMENT SHEILD PER SRM 51-40-02-0G-0 AND DWG 146A0081 57627U 31MAR20

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM BS 727A TO BS 800; LBL 21; WL 156 / REMOVED CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT ANGLE BS727A-800 LBL21 IN AREA OF 6' X 3' X 0.013' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 FABRICATED NE FLOOR SUPPORT AND SPLICE MADE FROM BAC1496-377 #7075T62 LOT# 427520-102 EXTRUSION TREATED AND PRIMED IAW SRM 51-20-01-0G-0 LOCATED AND DRILLED IAW SRM 51-40-05-0G-0 AND DWG #146A7502 AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG# 146A7500

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 70,174 hrs · 41,385 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM BS 727 TO BS 767; RBL 21; WL 156 / REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT BS727 -767 RBL21; WL156 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 REMOVED FLOOR TO SIDEWALL SUPPORT PER SRM 51-40-02-0G-0 FABRICATED REPLACEMENT FLOOR TO SIDEWALL SUPPORT OUT OF BAC1496-377 #7075T62; LOT# 427520-102 PER SRM 51-40-05; SRM 51-40-08 AND DWG 146A7502. APPLIED CHEMICAL CONVERSION COATING AND PRIMER PER AMM 51-21-41-370-802 AND AMM 51-21-72-370-804 AND INSTALLED REPLACEMENT FLOOR TO SIDEWALL SUPPORT BS727-767 RBL21 PER SRM 51-40-02-0G-0 AND DWG 146A7502 57627U 31MAR20

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 70,174 hrs · 41,385 cycles

CHAFED SKATE ANGLE AT B.S. 1007-1009; R.B.L. 14; W.L. 308. / REMOVED AND REPLACED SKATE ANGLE P/N 147A3000 PO# 773653/3 AT BS 1007 TO BS 1016 RBL 14 WL 308 IAW SRM 51-40-02 AND DWG 147A0030 REV B 57049U 19MAR2020

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 70,174 hrs · 41,385 cycles

CHAFED SKATE ANGLE AT B.S. 1009-1016; L.B.L. 14; W.L. 308. / REMOVED AND REPLACED SKATE ANGLE 147A3200U11 PO# 786342/1 AT BS 1007 TO BS 1016 LBL 14 WL 308 IAW SRM 51-40-02 AND DWG 147A0030 REV B 57049U 19MAR2020

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 70,174 hrs · 41,385 cycles

CHAFED SKATE ANGLE AT B.S. 1122; L.B.L. 14; W.L. 308. / REMOVED AND REPLACED SKATE ANGLE PO# 777690/1 AT BS 1016 TO BS 1132 LBL 14 WL 308 IAW SRM 51-40-02 AND DWG 148A8300 REV C 57049U 19MAR2020

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 70,174 hrs · 41,385 cycles

RIGHT HAND HORIZONTAL FORWARD UPPER SLIDE SEAL PLATE IS CRACKED. / REMOVED GAP COVER 342AT FOR ACCESS IAW SOPM 20-50-01. REMOVED & REPLACED R/H HORIZ. STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-801. STEP 3.D.& E. OK TO INSTALL 342AT 2166C 13APR20. INSP 21 13APR20. REINSTALLED 342AT IAW SOPM 20-50-01.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 70,174 hrs · 41,385 cycles

L/H HORIZONTAL STAB REMOVABLE L/E 1ST RIB FROM I/B END IS CRACKED / REMOVED AND REPLACED 1ST RIB FROM I/B END ON L/H HORIZ. STAB REMOVABLE L/E ASSY. IAW SRM 51-40-02-0G-0 PARA 4. AND DWG. # 186A1001.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 70,174 hrs · 41,385 cycles

FCB AFT CORNER SCUFF PLATE HAS DAMAGED FASTENER HOLE AND SIGNS OF CRACKING ON INTERNAL SURFACE. / REPAIRED FWD CARGO DOOR. AFT CORNER SCUFF PLATE IAW SWA EA 1-A53-2076 REV II

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 70,174 hrs · 41,385 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STA. 120.30; 4TH VERTICAL STIFFENER FROM THE FRONT IS CRACKED. / REPAIRED 4TH VERTICAL STIFFENER FROM FRONT ON R/H HORIZONTAL STAB. INSPAR RIB ASSY. AT STAB. 120.30 IAW SRM 55-10-09-2R-4; PARA 4; AND FIG. 202.

Part: LENS — UNSECURE (CABIN) · airframe 68,232 hrs · 40,132 cycles

LT OVERWING SIDEWALL EXIT LIGHT LENS WOULD NOT STAY ON. R&R CHARGER ASSEMBLY PER AMM.

Part: LENS — UNSECURE (CABIN) · airframe 68,232 hrs · 40,132 cycles

LT OVERWING SIDEWALL EXIT LIGHT LENS WOULD NOT STAY ON. R&R LIGHT ASSEMBLY PER AMM.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,909 hrs · 39,913 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD OUTER LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,909 hrs · 39,913 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD INNER LUG FACE CORRODED. / REPAIRED LUG FACE PER SRM.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,909 hrs · 39,913 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD INNER LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,909 hrs · 39,913 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD OUTER LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,909 hrs · 39,913 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD OUTER LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,909 hrs · 39,913 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD INNER LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,909 hrs · 39,913 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD OUTER LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: ELECTRONIC UNIT — FAULTY (MLG) · airframe 67,901 hrs · 39,909 cycles

LANDING GEAR LIGHT (RED) WOULD NOT EXTINGUISH WITH / LEVER IN THE UP & OFF POSITION. DIVERTED, R&R PROXIMITY SWITCH ELECTRONICS UNIT PER AMM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 67,857 hrs · 39,879 cycles

R1 DOOR J HOOK (R/H HOOK) FOR EMERGENCY SLIDE VERY LOOSE. / SECURED HARDWARE PER AMM.

Part: COVER — DISCONNECTED (CABIN) · airframe 67,391 hrs · 39,576 cycles

R2 DOOR EXIT LOWER LIGHT COVER DISCONNECTED FROM LIGHT FIXTURE. R&R LIGHT ASSEMBLY PER AMM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,198 hrs · 39,451 cycles

R2 DOOR SLIDE EMERGENCY LIGHT INOP. / R&R BATTERY CHARGER BASE PER AMM.

Part: PRESSURE DECK — CRACKED (BS 663-675) · airframe 67,198 hrs · 39,451 cycles

BEADED PRESSURE DECK CRACKED BETWEEN BS. 663.75 TO BS. 675, BETWEEN RBL 38 TO RBL 60. / REPAIRED DECK PER SRM.

Part: PLATE — CRACKED (AFT CARGO) · airframe 66,197 hrs · 38,827 cycles

AFT CARGO AFT CORNER PLATE IS CRACKED. / REMOVED AND REPLACED PER AMM.53-11-02.

Part: THRESHOLD — CRACKED (AFT CARGO) · airframe 66,197 hrs · 38,827 cycles

AFT CARGO THRESHOLD CRACKED. / REMOVED AND REPLACED PER AMM.53-11-02.

Part: SPOILER — DELAMINATED (RT WING) · airframe 65,114 hrs · 38,130 cycles

#12 SPOILER UPPER SURFACE FOUND TO BE DISBONDED AT TRAILING EDGE / WORK ACCOMPLISHED ON NRC WINGS 5015 DEFECT N159974

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 64,104 hrs · 37,478 cycles

FWD EMERGENCY EXIT LIGHT LENS MISSING AT BS 480. INSTALLED LENS IAW MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,104 hrs · 37,478 cycles

EMERGENCY LIGHTS BATTERY PACK M1675 INOPERATIVE. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,104 hrs · 37,478 cycles

EMERGENCY LIGHTS BATTERY PACK M1668 INOPERATIVE. R & R THE BATTERY PACK IAW MM.

Part: FITTING — BROKEN (LWR FUSELAGE) · airframe 64,104 hrs · 37,478 cycles

BROKE FITTING ASSY. ON BELLY AT STA. 546.26 RBL.6 / REMOVED BROKEN FITTINGS ASSY ON BELLY AT STA. 546.26 RBL 6 I.A.W. B737 SRM 51-40-07-0G-0. INSTALLED NEW FITTING ASSY LOT #5067957 I.A.W. B737 SRM 51-40-02-0G-0 AND BOEING DWG 149A7701 REV:-

Part: PANEL — DELAMINATED (RT WING) · airframe 64,104 hrs · 37,478 cycles

R/H LOWER WING PANEL 621VB HAS DISBOND FWD I/B CORNER AND DRAIN HOLE / R/H LOWER WING PANEL 621VB DISBOND FWD I/B CORNER REPAIRED IAW SRM 57-41-01-2R-1 TABLE 202 AND IA SRM 51-70-05-2R-10

Part: WEB — CRACKED (BS 294) · airframe 64,104 hrs · 37,478 cycles

R1 DOOR SUB THRESHOLD WEB CRACKED AT BS 294, WL 207. REPAIRED THE WEB IAW ER AND EA.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 64,104 hrs · 37,478 cycles

LOWER BULHEAD WEB CRACKED AT BS 663, RBL 75. REPAIRED THE BULKHEAD WEB IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 64,104 hrs · 37,478 cycles

INTERCOSTAL CORRODED BETWEEN BS 1006 TO BS 1016, LBL 37.95. R&R INTERCOSTAL IAW DWG & SRM.

Part: STUB FRAME — CRACKED (BS 294) · airframe 64,104 hrs · 37,478 cycles

R1 DOOR STUB FRAME CRACKED AT BS 294, WL 208. REPAIRED THE STUB FRAME IAW ER AND EA.

Part: DOOR SILL — CORRODED (FED THRESHOLD) · airframe 64,104 hrs · 37,478 cycles

***CORROSION*** FWD ENTRY DOOR INNER CHORD; ATTACHED ANGLE BS 312 -344 CORRODED / REMOVED CORROSION 12' X 1' X .010' ALLOWED 10% MATERIAL LOSS ORIGINAL MATERIAL THINKNESS IS .080' FOUND O BE OUT OF LIMITS PER SRM 53-10-15-1A-1 REPLACED ANGLE WITH NEW PER SRM 51-10-05 WILL BE INSTALLED ON NRC N129878

Part: STRAP — CORRODED (BS 287) · airframe 64,104 hrs · 37,478 cycles

RIGHT MOPSILL INNER STRAP CORRODED AT BS 287. R & R THE STRAP IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 64,104 hrs · 37,478 cycles

RT VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 40. REPAIRED WEB IAW SRM.

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 64,104 hrs · 37,478 cycles

LOWER BULKHEAD HORIZONTAL STIFFENER CRACKED AT BS 663 BETWEEN RBL 6 TO RBL 30. R & R THE STIFFENER IAW SRM & DWG.

Part: ANGLE — CORRODED (BS 951-992) · airframe 64,104 hrs · 37,478 cycles

AFT SERVICE DOOR LOWER SILL INNER ANGLE MOP SILL CORRODED BETWEEN BS 951 TO 992, WL 207. R & R THE ANGLE IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (BS 663-375) · airframe 64,104 hrs · 37,478 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED BETWEEN BS 663 TO 675, LBL 34. REPAIRED THE PRESSURE DECK WEB IAW ER AND EA.

Part: SEAL — CRACKED (BULKHEAD) · airframe 64,104 hrs · 37,478 cycles

BULKHEAD LOWER SEAL ASSEMBLY CRACKED AT BS 663, BETWEEN LBL 15 TO LBL 25. R & R THE SEAL ASSEMBLY IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (BS 847) · airframe 64,104 hrs · 37,478 cycles

AFT CARGO INTERCOSTAL CORRODED BETWEEN BS 847 TO 847+8, STRINGER 25R. R & R THE INTERCOSTAL IAW SRM.

Part: PANEL — CRACKED (AED) · airframe 64,104 hrs · 37,478 cycles

AFT GALLEY DOOR (R2) LWR HINGE ACCESS PANEL 844DZ LOWER CORNER CRACKED / REPLACED AFT GALLEY DOOR (R2) LWR HINGE ACCESS PANEL 844DZ I.A.W 20-50-11-910-801 STEP 2DI TABLE 205 93042U 4-03-18

Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 64,104 hrs · 37,478 cycles

RIGHT AC BAY BULKHEAD LOWER ATTACH ANGLE CRACKED AT BS 663, RBL 7. REPAIRED THE ATTACH ANGLE IAW EA.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 64,104 hrs · 37,478 cycles

CABIN FLOOR PANEL 221EF HAS DAMAGE AT FWD LH CORNER / REPAIRED DAMAGE AT FWD L/H CORNER IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 ON FLOOR PANEL 221EF

Part: SUPPORT CHANNEL — CRACKED (BS 270-277) · airframe 64,104 hrs · 37,478 cycles

FORWARD WET AREA SUPPORT CHANNEL CRACKED BETWEEN BS 270 TO 277. R & R THE SUPPORT CHANNEL IAW SRM AND DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 64,104 hrs · 37,478 cycles

PASSENGER CABIN FLOOR BOARD 222AF OUTB AFT CORNER DAMAGED / REPAIRED OUT BOARD AFT CORNER OF PASSENGER CABIN FLOOR BOARD 222AF IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,104 hrs · 37,478 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 51 TO LBL 51. R&R TEE CAP PER SRM AND EA.

Part: CREASE BEAM — CORRODED (BS 328-360) · airframe 64,104 hrs · 37,478 cycles

LEFT INNER CREASE BEAM ANGLE CORRODED BETWEEN BS 328 TO 360. R & R THE CREASE BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (BS 285-328) · airframe 64,104 hrs · 37,478 cycles

RIGHT INNER CREASE BEAM ANGLE CORRODED BETWEEN BS 285 TO 328. R & R ANGLE IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 64,104 hrs · 37,478 cycles

FORWARD WET AREA SUPPORT CHANNEL CRACKED BETWEEN BS 360 TO 344, BL 0. R & R THE FLOOR SUPPORT IAW DWG AND SRM.

Part: ANGLE — CRACKED (WHEEL WELL LH) · airframe 64,104 hrs · 37,478 cycles

L/H BS 663 LOWER VAPOR BARRIER; WEB SUPPORT ANGLE CRACKED AT LBL 25 ATTACH POINT / REMOVED AND REPLACED CRACKED SUPPORT ON BS663 L/H VAPOR BARRIER WEB LBL 25 PER SRM 51-40-02 AND DWG 111A1000

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 64,104 hrs · 37,478 cycles

FORWARD WET AREA SUPPORT CHANNEL CRACKED BETWEEN BS 360 TO 344, RBL 33. R & R FLOOR SUPPORT IAW DWG AND SRM.

Part: SKIN — DAMAGED (FWD FUSELAGE) · airframe 64,104 hrs · 37,478 cycles

**CUSTOMER REQUEST** INVESTIGATE DAMAGED FASTENER R/H BS 370; STR 21; SKIN. / REPAIRED SKIN AT BS 370; STR 21R IAW SWA EA 1-753-32493 REV IR AND ATS ER 18-02065 REV IR

Part: SKIN — DAMAGED (FWD FUSELAGE) · airframe 64,104 hrs · 37,478 cycles

**CUSTOMER REQUEST** INVESTIGATE DAMAGED FASTENER R/H BS 294; STR 20; SKIN. / REPAIRED DAMAGED SKIN AT FASTENER R/H BS 294 STR 20; IAW SRM 53-00-01-2R-36 APPLIED EXTERIOR FINISH TO REPAIR PER SRM 53-00-01-2R-36; STEP #4.U

Part: SUPPORT ANGLE — CORRODED (BS 727E-847) · airframe 64,104 hrs · 37,478 cycles

AFT CARGO SIDE WALL TO FLOOR TRANSITION PLATE CORRODED BETWEEN BS 727E+10 TO 847, LBL 23. THE REPAIRED SUPPORT ANGLE IAW SRM.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 64,104 hrs · 37,478 cycles

***CORROSION*** AROUND FASTENER HOLES ON SIDEWALL SUPPORT ANGLE STA. 787 LBL 30-LBL 45 ABOVE STR. 24L-STR. 22L (MARKED) IN AFT CARGO COMPARTMENT / REPAIRED SIDEWALL SUPPORT ANGLE BS 787 LBL 30-45 ABOVE STR 24L-22L IAW ER 18-02205 REV IR AND SWA EA 1-753-32507 REV IR

Part: INTERCOSTAL — CORRODED (BS 847) · airframe 64,104 hrs · 37,478 cycles

AFT CARGO BAY INTERCOSTAL CORRODED AT BS 847, STRINGER 26L. R & R THE INTERCOSTAL IAW SRM AND DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 727-767) · airframe 64,104 hrs · 37,478 cycles

AFT CARGO BAY SIDE WALL TO FLOOR TRANSITION PLATE CORRODED BETWEEN BS 727 TO 767, RBL 17. R & R SIDEWALL SUPPORT IAW SRM AND DWG.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 64,104 hrs · 37,478 cycles

***CORROSION*** ON STRAP IN AFT CARGO COMPARTMENT STA.767+15 RBL 17 WL 163 (MARKED) / CORROSION ON STRAP IN AFT CARGO COMPARTMENT BS 767+15 RBL 17 WL 163 FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 FIG 103. PART TO BE REPLACED ON CUSTOMER CARD N129740

Part: WEB — CORRODED (BS 787-827) · airframe 64,104 hrs · 37,478 cycles

AFT CARGO BAY AFT CARGO DOOR THRESHOLD WEB CORRODED BETWEEN BS 787+15 TO 827, RBL 23. R & R THE THRESHOLD WEB IAW SRM AND DWG.

Part: GUSSET — CORRODED (AFT CARGO BAY) · airframe 64,104 hrs · 37,478 cycles

***CORROSION*** ON GUSSET STRAP STA. 787+4 LBL 37 (MARKED) IN AFT CARGO COMPARTMENT / REMOVED AND REPLACED GUSSET STRAP @ STA791 LBL37 STR 24L WITH FABIRCATED REPLACEMENT PART PER SRM 51-40-02 DWG 146A7550

Part: ANGLE — CORRODED (BS 887-947) · airframe 64,104 hrs · 37,478 cycles

SIDEWALL TO FLOOR TRANSITION STRIP AROUND CORRODED BETWEEN BS 887 TO 947, RBL 15. R & R THE ANGLE IAW SRM AND DWG.

Part: SPLICE — CORRODED (BS 847-867) · airframe 64,104 hrs · 37,478 cycles

AFT CARGO BAY SHIELD CORRODED BETWEEN BS 847 TO 867, RBL 15. R & R THE SPLICE IAW SRM AND DWG.

Part: FRAME — CORRODED (BS 947) · airframe 64,104 hrs · 37,478 cycles

FUSELAGE FRAME CORRODED AT BS 947, LBL 12. WL 178. REPAIRED THE FRAME IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 767) · airframe 64,104 hrs · 37,478 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 767+4, RBL 17. R & R THE FLOOR SUPPORT IAW SRM.

Part: SHIELD — CORRODED (BS 767-787) · airframe 64,104 hrs · 37,478 cycles

AFT CARGO BAY SHIELD CORRODED BETWEEN BS 767 TO 787, RBL 18. R & R THE SHIELD IAW SRM & DWG.

Part: STRAP — CORRODED (BS 847) · airframe 64,104 hrs · 37,478 cycles

AFT CARGO BAY STRAP CORRODED AT BS 847, RBL 15. R & R THE STRAP IAW SRM AND DWG.

Part: FRAME — CRACKED (BS 947) · airframe 64,104 hrs · 37,478 cycles

FUSELAGE FRAME CRACKED AT BS 947, RBL 8, WL 178. REPAIRED THE FRAME IAW EA.

Part: GUSSET — CRACKED (BS 500D) · airframe 64,104 hrs · 37,478 cycles

FORWARD CARGO GUSSET CRACKED AT BS 500D, STRINGER 19L. R & R THE GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 64,104 hrs · 37,478 cycles

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

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 64,104 hrs · 37,478 cycles

AFT CARGO COMPARTMENT FORWARD CORNER SCUFF PLATE CRACKED / LOCATED & DRILLED NEW FWD. CORNER SCUFF PLATE AFT CARGO DOOR IAW SRM 51-40-05 & DWG #146A8341; TO BE INSTALLED ON CUSTOMER CARD #753-140-00-02Y 57171U 06APR18

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 64,104 hrs · 37,478 cycles

LT WHEEL WELL LOWER FIBERGLASS BULKHEAD DELAMINATED AT BS 663. REPAIRED BULKHEAD PER SRM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 64,104 hrs · 37,478 cycles

RT WHEEL WELL LOWER FIBERGLASS BULKHEAD CRACKED AT BS 663. REPAIRED BULKHEAD IAW SRM.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 64,104 hrs · 37,478 cycles

FWD CARGO DOOR AFT SCUFF PLATE CORNER CRACKED / REMOVED DAMAGED FWD. CARGO DOOR AFT. SCUFF PLATE I.A.W. A.M.M. 53-11-02-020-801. LOCATED AND DRILLED NEW SCUFF PLATE PART #143A8331-4; I.A.W. S.R.M. 51-40-05-0G-0 AND DRAWING #143A8330. INSTALLED NEW SCUFF PALTE; I.A.W. A.M.M. 53-11-02-420-801; 51-40-02-0G-0 AND DRAWING #143A8330.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,104 hrs · 37,478 cycles

LEFT OVERWING HATCH EMERGENCY LIGHT INOPERATIVE. R & R THE BULB IAW AMM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 64,104 hrs · 37,478 cycles

RIGHT WING LOWER SKIN OF THE NR 6 LEADING EDGE SLAT FOUND CRACKED. REPAIRED THE SLAT SKIN IAW SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 64,081 hrs · 37,463 cycles

L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 64,072 hrs · 37,459 cycles

R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED THE SLIDE IAW MT.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 64,072 hrs · 37,459 cycles

L2 DOOR SLIDE OUT OF ADJUSTMENT. ADJUSTED THE SLIDE IAW MT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,051 hrs · 37,447 cycles

LEFT OVERWING OUTSIDE EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 63,527 hrs · 37,117 cycles

LEFT OVERHEAD BIN EMERGENCY LIGHT LENS LOOSE AT ROW 4. SECURED THE LENS IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,186 hrs · 36,895 cycles

LT OVERWING EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 62,704 hrs · 36,586 cycles

RT OVERHEAD OVERWING EMERGENCY EXIT LIGHT INOP. R&R POWER SUPPLY IAW AMM.

Part: RETAINER — CRACKED (RT WING) · airframe 62,121 hrs · 36,220 cycles

RIGHT WING; UPPER SHELF PANEL ABOVE PYLON; SEAL RETAINER IS CRACKED ON FORWARD SIDE. / R/R RIGHT WING; UPPER SHELF PANEL ABOVE PYLON; SEAL RETAINER PER SRM 51-40-02

Part: SLIDE — LOOSE (L1 DOOR) · airframe 61,989 hrs · 36,137 cycles

L1 DOOR ESCAPE SLIDE GIRT LOOSE. R&R SLIDE PER MT.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 61,943 hrs · 36,106 cycles

AFT RT EMERGENCY EXIT SIGN BROKEN. R & R THE SIGN IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 61,550 hrs · 35,870 cycles

LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. R&R FUSE PER MM.

Part: FUSE — BLOWN (CABIN) · airframe 61,113 hrs · 35,596 cycles

AFT OF LT OVERWING EMERGENCY EXIT LIGHT INOP. R&R FUSE PER MM.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 61,041 hrs · 35,552 cycles

LEFT OVERWING EXIT LIGHT INOPERATIVE. R & R THE LIGHT ASSY IAW MM.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 59,891 hrs · 34,886 cycles

LEFT INTERCOSTAL CRACKED AT BS 312 TO 328, WL 208. R & R THE INTERCOSTAL IAW SRM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 59,891 hrs · 34,886 cycles

EMERGENCY LIGHT BATTERY M1675 FAILED CAPACITY TEST. R & R THE BATTERY IAW MM.

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 57,751 hrs · 33,647 cycles

RIGHT WING OTBD AFT FLAP, OTBD FLAP TRACK LOOSE AFT SIDE. R & R FLAP TRACK IAW AMM.

Part: PLATE — CRACKED (RT WING) · airframe 57,751 hrs · 33,647 cycles

RIGHT WING WIGGLE PLATE CRACKED INBD OF NR 2 PYLON. R & R WIGGLE PLATE IAW SRM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 57,751 hrs · 33,647 cycles

LEFT WING UPPER FIXED TE PANEL SEAL SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,672 hrs · 33,599 cycles

LEFT EMER OVERWING ESCAPE LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

SHIELD CORRODED AT BS 772, RBL 22. R & R SHIELD IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

INTERCOSTAL CORRODED AT BS 772, RBL 20. REPAIRED INTERCOSTAL IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

LEFT FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 772, LBL 22. REPAIRED SUPPORT IAW SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

AFT CARGO BAY FLOOR TEE SPLICE CORRODED, BETWEEN BS 727D - 727E, BETWEEN LBL 17 - RBL 14. R & R SPLICE IAW SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

AFT CARGO BAY FLOOR T SPLICE CORRODED AT BS 772.6, BETWEEN LBL 17 - RBL 14. R & R T SPLICE IAW AMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

EXTERNAL POWER DOOR CUT OUT INTERNAL BONDED DOUBLER, CRACKED BELOW LOWER HINGE. REPAIRED CUT OUT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED FRAME IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 57,672 hrs · 33,599 cycles

LOWER SILL AFT STRAP CORRODED AT BS 639, WL 222. R & R STRAP IAW SRM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 57,528 hrs · 33,515 cycles

LEFT WING EXTERNAL EMER EXIT LIGHT INOPERATIVE. R & R POWER SUPPLY ASSEMBLY IAW MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 57,448 hrs · 33,465 cycles

FIRST OFFICERS NR 2 WINDOW OUTSIDE PANE ARCED. R & R R2 WINDOW IAW MT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,287 hrs · 32,801 cycles

FUSELAGE SKIN DAMAGED AT BS 850, STRINGER 1. REPAIRED SKIN IAW SRM & EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,695 hrs · 32,453 cycles

R1 DOOR EXTERNAL EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 55,631 hrs · 32,416 cycles

LEFT FWD GALLEY BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 55,631 hrs · 32,416 cycles

RIGHT AFT GALLEY BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 55,631 hrs · 32,416 cycles

LEFT AFT GALLEY BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 55,631 hrs · 32,416 cycles

RIGHT LOWER MID CABIN BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: COVER — LOOSE (CABIN) · airframe 54,578 hrs · 31,820 cycles

R1 DOOR EMER EXIT LIGHT COVER LOOSE. REPAIRED COVER IAW EA.

Part: SIGN — BROKEN (CABIN) · airframe 52,935 hrs · 30,863 cycles

CENTER LINE OVERHEAD OVERWING EXIT SIGN BROKEN. R & R SIGN IAW SIP.

Part: SIGN — LOOSE (CABIN) · airframe 52,236 hrs · 30,460 cycles

R2 DOOR EMER EXIT SIGN LIGHT LOOSE. SECURED SIGN ASSEMBLY IAW AMM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 51,792 hrs · 30,200 cycles

L1 DOOR EMER EVAC SLIDE RT SIDE GIRT BAR HOOK LOOSE. SECURED HOOK IAW SIP.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 50,890 hrs · 29,663 cycles

LEFT WW FWD SIDE STATION 663 BULKHEAD HORIZONTAL ANGLE CRACKED. REPAIRED ANGLE IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,890 hrs · 29,663 cycles

CENTER SECTION WING LT SIDE ABOVE PACK EXHAUST DUCT HORIZONTAL ANGLE CRACKED ON INBD END. R & R ANGLE IAW SRM & DWG.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 50,890 hrs · 29,663 cycles

RT NR 1 FLIGHT DECK WINDOW FRAME CRACKED AT UPPER AFT FASTENER HOLE ON C - D POST. REPAIRED WINDOW IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,890 hrs · 29,663 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM IAW SWA EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,890 hrs · 29,663 cycles

RIGHT HORIZONTAL STABILIZER STATION 92.70 FIRST RIB VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,890 hrs · 29,663 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.75. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,890 hrs · 29,663 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 24.75. REPAIRED BEAM IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,890 hrs · 29,663 cycles

LEFT HORIZONTAL STABILIZER RIB STATION 129.50 2ND VERTICAL STIFFENER AFT OF FRONT STAB SPAR CRACKED. REPAIRED RIB IAW EA.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 50,890 hrs · 29,663 cycles

LEFT HORIZONTAL STABILIZER RIB STATION 111.10, 3RD VERTICAL STIFFENER AFT OF FRONT STAB SPAR CRACKED. REPAIRED STIFFENER IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,890 hrs · 29,663 cycles

COCKPIT RT NR 3 WINDOW FRAME E - F POST CRACKED INDICATION IN 2ND HOLE FROM BOTTOM. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 50,890 hrs · 29,663 cycles

COCKPIT LT NR 3 WINDOW FRAME E - F POST CRACKED IN 2ND HOLE FROM BOTTOM. REPAIRED POST IAW ACO.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,890 hrs · 29,663 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, LBL 42. REPAIRED WEB IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,890 hrs · 29,663 cycles

COCKPIT RT NR 1 WINDOW FRAME OTBD POST CRACKED NEAR UPPER CORNER. REPAIRED FRAME IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 50,890 hrs · 29,663 cycles

COCKPIT LT NR 1 WINDOW FRAME OTBD POST CRACKED NEAR UPPER CORNER. REPAIRED POST IAW ACO.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 50,369 hrs · 29,359 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,276 hrs · 29,302 cycles

AFT EMERGENCY CABIN LIGHT LAMPS INOPERATIVE. RELAMPED LIGHTS IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,448 hrs · 28,792 cycles

LT EMERGENCY LIGHTS INOPERATIVE BETWEEN STATION 560 TO STATION 640. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,448 hrs · 28,792 cycles

RT EMERGENCY LIGHTS INOPERATIVE BETWEEN STATION 560 TO STATION 757. R & R BATTERY PACK IAW MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 48,659 hrs · 28,309 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: COVER — MISSING (EXIT SIGN) · airframe 48,178 hrs · 28,040 cycles

AFT SERVICE DOOR EXIT SIGN COVER MISSING. INSTALLED COVER IAW M.M.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 46,747 hrs · 27,212 cycles

LEFT STAB SLIDING SEAL IS CRACKED. REMOVED AND REPLACED REF AMM.

Part: LENS — DAMAGED (CABIN) · airframe 46,462 hrs · 27,036 cycles

EXIT LIGHT AT R1 DOOR LENS DAMAGE. REPLACE LENS AND VERIFIED NORMAL OPERATION IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 45,657 hrs · 26,510 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: LENS — LOOSE (R2 DOOR) · airframe 45,657 hrs · 26,510 cycles

R2 DOOR EMERGENCY EVAC SLIDE LENS LOOSE. REMOVED AND REPLACED LENS PER AMM & MT.

Part: HOOK — LOOSE (L1 DOOR) · airframe 45,360 hrs · 26,339 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP LOOSE. SECURED GIRT BAR HOOK PER AMM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 45,199 hrs · 26,244 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 45,156 hrs · 26,214 cycles

R2 DOOR LOWER EMERGENCY EXIT SIGN LENS LOOSE. REMOVED AND REPLACED SIGN IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 44,020 hrs · 25,525 cycles

STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,020 hrs · 25,525 cycles

FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,020 hrs · 25,525 cycles

FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,020 hrs · 25,525 cycles

FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 44,020 hrs · 25,525 cycles

FLOOR STRAP CORRODED AT BS 887, LBL 6. REMOVED AND REPLACED STRAP PER SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,020 hrs · 25,525 cycles

FRAME SUPPORT CORRODED AT BS 787, BETWEEN STR 24L AND STR 25L. REPAIRED FRAME SUPPORT PER SRM, DWG, & ER.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,020 hrs · 25,525 cycles

FWD BULKHEAD FLOOR SUPPORT CORRODED AT BS 380, RBL 12. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,020 hrs · 25,525 cycles

SKIN CORRODED AT BS 500A+12, BL 0. REPAIRED SKIN IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 44,020 hrs · 25,525 cycles

WEB CORRODED AT BS 480+8, RBL 24. REMOVED AND REPLACED WEB IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,020 hrs · 25,525 cycles

SKIN CORRODED BS 500+8, BL 0. REPAIRED SKIN IAW SRM AND DWG.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 44,020 hrs · 25,525 cycles

RT AFT EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER AMM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 44,020 hrs · 25,525 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT REAR SPAR BETWEEN STA 134 TO STA 136. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 44,020 hrs · 25,525 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT RIB STA 101.90. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 44,020 hrs · 25,525 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT RIB STA 101.90. REMOVED AND REPLACED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 44,020 hrs · 25,525 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 98 AND STA 99. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 44,020 hrs · 25,525 cycles

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT RIB STA 138.70. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 44,020 hrs · 25,525 cycles

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 138.70. REPAIRED SKIN PER SRM.

Part: FUSE — BLOWN (CABIN) · airframe 43,123 hrs · 25,000 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT FUSE PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 42,535 hrs · 24,661 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS STRIP DISCOLORED AT ROW 12. REMOVED AND REPLACED EEPLS PER MM.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 40,302 hrs · 23,358 cycles

ON DESCENT FLIGHT ATTENDANTS CALLED STATING A STRONG "ELECTICAL BURNING" ODOR IN CABIN. REMOVED AND REPLACED NR 2 COFFEEMAKER PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 43,716 hrs · 25,356 cycles

LT HORIZONTAL LEADING EDGE SKIN CRACKED AT APPROX L/E STA 110. REMOVED AND REPLACED SKIN IAW M/M.

Part: FITTING — CRACKED (CENTER WINGBOX) · airframe 36,901 hrs · 21,360 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, LBL 14.5. REMOVED AND REPLACED SHEAR FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WINGBOX) · airframe 36,901 hrs · 21,360 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, LBL 6.5. REMOVED AND REPLACED SHEAR FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WINGBOX) · airframe 36,901 hrs · 21,360 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, RBL 14.5. REMOVED AND REPLACED SHEAR FITTING PER SRM.

Part: RIB — CRACKED (TE FLAP) · airframe 36,901 hrs · 21,360 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING I/B AFT FLAP L/E RIB CRACKED. REMOVED AND REPLACED RIB PER AAR EA.

Part: LIGHT — WORN (CABIN) · airframe 36,809 hrs · 21,299 cycles

DURING SCHEDULED CV CHECK, FOUND RT EEPLS WORN AT ROW 11. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 35,825 hrs · 20,692 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,721 hrs · 20,634 cycles

DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT 6 ABC. RELAMPED PER MM.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,000 hrs · 20,194 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION SUPPORT FITTING LUG FACES CORRODED. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,000 hrs · 20,194 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION SUPPORT FITTING LUG FACES CORRODED. REPAIRED FITTING PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,632 hrs · 19,366 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 33,488 hrs · 19,280 cycles

DURING SCHEDULED HC1 CHECK, LT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRIP — WORN (CABIN) · airframe 33,488 hrs · 19,280 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS STRIP WORN BETWEEN ROW 5 TO ROW 10. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 33,488 hrs · 19,280 cycles

DURING SCHEDULED HC1 CHECK, RT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — LOOSE (CABIN) · airframe 31,978 hrs · 18,390 cycles

FOUND FWD EMERGENCY EXIT SIGN COVER LOOSE. REMOVED AND REPLACED COVER PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,371 hrs · 17,361 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 986.5, RBL 48 TO LBL 48. REPAIRED CHORD PER SWA EA.

Part: COMPRESSOR — FAULTY (AFT CARGO BAY) · airframe 29,718 hrs · 16,983 cycles

STRONG ELECTRICAL SMELL REPORTED IN CABIN. FOUND WATER AIR COMPRESSOR FAULTY. REMOVED AND REPLACED WATER AIR COMPRESSOR PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,655 hrs · 16,947 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 28,891 hrs · 16,492 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 28,891 hrs · 16,492 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 28,879 hrs · 16,486 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 28,879 hrs · 16,486 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,040 hrs · 15,999 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 27,968 hrs · 15,959 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,124 hrs · 15,496 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — FAULTY (AFT GALLEY) · airframe 25,598 hrs · 14,589 cycles

CABIN REPORTED SMOKE, ELECTRICAL SMELL ON GROUND. SECURED CABIN CEILING LIGHTS SMOKE SMELL DISSIPATED. INSPECTED CABIN LIGHTS, RT AND LT PACKS, RAN GASPER AND RECIRC FANS, NO FAULTS NOTED. REMOVED AND REPLACED AFT GALLEY WORK LIGHT BULBS PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 25,011 hrs · 14,245 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,963 hrs · 13,630 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 7 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 22,109 hrs · 12,576 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,902 hrs · 12,469 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,592 hrs · 12,296 cycles

DURING SCHEDULED HC2 CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT ROW 8 DEF. REMOVED AND REPLACED SOCKET ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 17,089 hrs · 9,729 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 16,640 hrs · 9,466 cycles

R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: PSEU — FAULTY (E/E BAY) · airframe 15,662 hrs · 8,919 cycles

AIR TURNBACK, AFTER TAKEOFF FROM MDW WITH GEAR AND FLAPS RAISED THE TAKEOFF WARNING HORN GOES OFF WITH POWER REDUCTION. REMOVED AND REPLACED PSEU PER MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 14,717 hrs · 8,398 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR SKIN CRACKED AT AFT UPPER CORNER. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,609 hrs · 8,332 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS TRACK LIGHT ROW 2 ABC INOP. RELAMPED PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 11,787 hrs · 6,806 cycles

EEPLS COVERS LOOSE AT ROWS NR 1 AND NR 2. SECURED COVERS PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 11,328 hrs · 6,555 cycles

EEPLS COVER LOOSE AT ROW NR 1 ABC. SECURED EEPLS COVER PER MM.

Part: SLIDE — LOOSE (AFT SVC DOOR.) · airframe 8,202 hrs · 4,835 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: SLIDE — LOOSE (FWD SVC DOOR) · airframe 8,043 hrs · 4,751 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: PANEL — LOOSE (COCKPIT DOOR) · airframe 5,163 hrs · 3,108 cycles

COCKPIT DOOR EGRESS PANELS WOULD NOT LATCH IN PLACE. SECURED EGRESS PANELS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 4,149 hrs · 2,490 cycles

EEPLS TRACK LIGHT BROKEN, AT FWD END OF CABIN. REMOVED AND REPLACED EEPLS LIGHT ASSY PER MM.

Part: SKIN — DELAMINATED (RUDDER) · airframe 3,607 hrs · 2,161 cycles

DURING SCHEDULED A2 CHECK, FOUND 12 X 6 DELAMINATION ON RUDDER, LT SIDE, 35 ABOVE BOTTOM, 12 AFT OF L/E. MX FERRIED AIRCRAFT TO HOU. REMOVED AND REPLACED RUDDER PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 3,607 hrs · 2,161 cycles

DURING SCHEDULED A2 CHECK (SWA SI 11038-55), FOUND RT ELEVATOR TAB OUTBD HINGE FITTING HAS EXCESSIVE PLAY. REMOVED AND REPLACED ELEVATOR TAB BUSHINGS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 3,009 hrs · 1,787 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 1. REMOVED AND REPLACED TRACK COVER PER MM.

Part: SLIDE — DISLODGED (FWD SERVICE DOOR) · airframe 2,716 hrs · 1,603 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE ASSY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM.