N202WN

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 62,313 hrs · 37,162 cycles

AFT PASS ENTRY DOOR SLIDE GAUGE NOT VISIBLE.<[01] REMOVED; REPOSITIONED; AND REINSTALLED L2 DOOR SLIDE IAW MT 725-61-06.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,897 hrs · 36,883 cycles

RT FLAP SPLIT ON FINAL @ FLAPS 30 DEG. FLAP WOULD NOT RETRACT AFTER LANDING<[01] PREFORM FIM TASK 27-51 TASK 813 FOUND FAULT 27-52259 OPS CHECK OK OF SYSTEM NO FAULTS NOTED AT THIS TIME

Part: FLAP — CRACKED (ZN 500 LEFT WING) · airframe 61,145 hrs · 36,406 cycles

LH IB AFT FLAP DENT/CRACK LH IB AFT FLAP DENT/CRACK LOWER SKIN<[01] APPLIED PERMANENT REPAIR PER SRM 57-53-01-2R-4 AND SRM 51-70-10.

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 60,560 hrs · 36,023 cycles

THE MID LEVEL EMERGENCY EXIT LIGHT LENS IS MISSING AT THE RIGHT OVERWING EMERGENCY EXIT<[01] INSTALLED LENS REF AMM 33-51-01

Part: GIRT BAR — LOOSE (FWD ENTRY DOOR) · airframe 58,974 hrs · 35,001 cycles

FED AFT GRIT BAR FITTING IS LOOSE. / [01] TIGHTENED FED AFT GIRT BAR FITTING PER AMM 25-66-02-400-801 PARA: 3.D.(1)(G) - (J);[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] VERIFIED MEASUREMENTS TABLE.;[04] CERTIFY

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 58,974 hrs · 35,001 cycles

EMERGENCY LIGHTS ON BIN BULLNOSE INOP AT SEATS 9CBA AND 11CBA. REPLACED EMERGENCY LIGHTS BATTERY PACK M1670 AND PERFORMED GOOD TEST PER AMM 33-51-06-960-805.

Part: LIGHT — INOPERATIVE · airframe 58,974 hrs · 35,001 cycles

EMERGENCY LIGHT BULBS BURNED OUT AT R OWE EXIT SIGNS. REPLACED LAMPS AND PERFORMED GOOD FUNCTIONAL TEST OF EMERGENCY LIGHT RT OWE EXIT SIGNS IAW AMM 33-51-01-960-801.

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

FWD CARGO BAY BAFFLE CRACKED BS 400 - BS 420 LBL 25 / [01] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS ; CRACK FOUND OUT LIMITS;[02] REMOVED FWD CARGO BAY BAFFLE FROM BS 400 TO BS 420 ; LBL 25 IAW SRM 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW FWD CARGO BAY BAFFLE P/N 143A7510-33 IAW SRM 51-40-05-0G-0 AND DWG 143A7505; ID:0002; REV:B; OK TO INSTALL NEW BAFFLE;[04] VERIFIED CORRECTIVE ACTIONS 1 AND 3.<BR>OK TO INSTALL;[05] INSTALLED NEW FWD CARGO BAY BAFFLE BETWEEN BS 400 TO BS 420; LBL 25 IAW SRM 51-40-02-0G-0 AND DWG 143A7505; ID:0002; REV:B;[06] VERIFIED CORRECTIVE ACTION 5;[07] VERIFIED MEASUREMENT TABLE

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

FWD CARGO BAY BAFFLE CRACKED BS 500B - BS 500C LBL 25 / [01] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS ; CRACK FOUND OUT OF LIMITS;[02] REMOVED FWD CARGO BAY BAFFLE FROM BS 500B TO BS 500C ; LBL 25 IAW 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW FWD CARGO BAY BAFFLE P/N 143A7510-11 IAW SRM 51-40-05-0G-0 AND DWG 143A7505; ID:0005; REV:B; OK TO INSTALL NEW BAFFLE;[04] VERIFIED CORRECTIVE ACTIONS 1 AND 3.<BR>OK TO INSTALL;[05] INSTALLED NEW FWD CARGO BAY BAFFLE BETWEEN BS 500B TO BS 500C ; LBL25 IAW SRM 51-40-02-0G-0 AND DWG 143A7505; ID:0005; REV:B;[06] VERIFIED CORRECTIVE ACTION 5;[07] VERIFIED MEASUREMENT TABLE

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

FWD CARGO BAY BAFFLE CRACKED BS 500 - BS 500A LBL 25 / [01] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS;[02] FWD CARGO BAY BAFFLE FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 ; STEP 4C;[03] REMOVED FWD CARGO BAY BAFFLE FROM BS 500 TO BS 500A ; LBL 25 IAW SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW FWD CARGO BAY BAFFLE P/N 143A7510-15 IAW SRM 51-40-05-0G-0 AND DWG 143A7505; ID:0007; REV:-; OK TO INSTALL NEW BAFFLE;[05] VERIFIED CORRECTIVE ACTIONS 1; 2 AND 4.<BR>OK TO INSTALL;[06] INSTALLED NEW FWD CARGO BAY BAFFLE BETWEEN BS 500 TO BS 500A ; LBL 25 IAW SRM 51-40-02-0G-0 AND DWG 143A7505; ID: 0037; REV:-;[07] VERIFIED CORRECTIVE ACTION 6;[08] VERIFIED MEASUREMENT TABLE

Part: LIGHT — BROKEN (PAX CABIN) · airframe 58,974 hrs · 35,001 cycles

SIDEWALL PANEL 232YHW EMERGENCY EXIT LIGHT LENS COVER IS BROKEN / [01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS COVER ON SIDEWALL PANEL 232YHW IAW AMM 33-51-01-960-801 STEPS 2. C. (1)(A) AND (4);[02] VERIFIED CORRECTIVE ACTION 1

Part: FRAME SPLICE — CORRODED · airframe 58,974 hrs · 35,001 cycles

CORROSION ON PASSENGER CABIN FRAME SPLICE AT BS 277 BL 0 STRINGER 1.(MARKED) / [01] NOT ALLOWABLE LIMITS FOUND ON SRM FOR BS277 FRAME SPLICE;SRM 51-10-02-0G-0 PAR. 9.C REPLACEMENT OF THE PART IS APPLICABLE;[02] REMOVED BS277 FRAME SPLICE LBL3-RBL3 WL287 I.A.W SRM 51-40-02-0G-0;[03] REQUEST UT THICKNESS IN BLENDED AREA;[04] UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2.<BR>REMAINING MATERIAL THICKNESS IS 0.049' ADJACENT TO 0.051'. <BR>EQUIP USED: <BR>-EPOCH 650 ID: ATS2031 CAL DUE: 03/23;[05] CERTIFY;[06] OK TO INSTALL FRAME SPLICE.;[07] OK TO INSTALL;[08] INSTALLED FRAME SPLICE AT BS 277 BL 0 IAW SRM 51-40-02-0G-0; DWG 141A1110.;[09] VERIFIED CORRECTIV ACTION 8.;[10] VERIFIED THE MEASUREMENT TABLE.;[11] WORKSCOPE COMPLETE PER EA 22-153-02247.

Part: WEB — CRACKED (FWD ENTRY DOOR) · airframe 58,974 hrs · 35,001 cycles

CRACK ON PASSENGER CABIN FWD ENTRY DOOR FWD WEB AT BS 294+1 L/H STRINGER 16.(MARKED) / [01] CLEANED PASSENGER CABIN FWD ENTRY DOOR FWD WEB AT BS 294+1 L/H<BR>STRINGER 16.;[02] VERIFIED WORK PERFORMED;[03] NDT HFEC SURFACE INSPECTED AREA PER 737 NDTM PART 6 51-00-00 PROC 23; LARGE CRACK NOTED; ENDS MARKED.<BR>EQUIP ID. NORTEC 500D IS000681 DUE 02/23;[04] UPON FURTHER INVESTIGATION OF FWD ENTRY DOOR FWD (WEB) INTERCOSTAL FITTING. INTERCOSTAL IS OUT OF LIMITS -NO CRACKS ARE PERMITED. PART TO BE REPAIR BY REPLACEMENT I.A.W SRM 51-10-02-0G-0 PARA 9.;[05] PARTIAL UPDATED STEPS 1-2.;[06] REMOVED CRACKED FWD ENTRY DOOR FWD(WEB) INTERCOSTALL FITTING -STA 295; STR 16L. PER SRM 51-40-02.;[07] VERIFIED CORRECTIVE ACTION #4; 6;[08] LOCATED AND DRILLED INTERCOSTAL FITTING ;PASSENGER FWD CABIN ENTRY DOOR FWD WED STA 295;STR 16L; PER SRM 51-40-05 ;OK TO INSTALL;[09] VERIFIED CORRECTIVE ACTION STATEMENT 8; MEASUREMENT TABLE AND OK TO INSTALL THE FITTING.;[10] CERTIFY;[11] INSTALLED NEW FWD ENTRY DOOR FWD(WEB) INTERCOSTALL FITTING -STA 295; STR 16L;STRAP PN 141A8182-3 AND T-BRACKET PN 141A8184-8 ; PER SRM 51-40-02; AND BOEING DWG 141A8180;COMPLETED STEP 1 AND STEP 2;[12] COMPLETED ALL AMT TASK;[13] VERIFIED CORRECTIVE ACTION 11.;[14] VERIFIED WORKSCOPE IS COMPLETE.

Part: STRINGER CLIP — CRACKED (FWD ENTRY DOOR) · airframe 58,974 hrs · 35,001 cycles

CRACK ON PASSENGER CABIN FWD ENTRY DOOR CLIP AT BS 294 L/H STRINGER 13.(MARKED) / [01] REMOVED CRACKED CLIP AT BS 294 STR 13 L/H IAW SRM 51-40-02-0G-0;[02] UPDATED MEASUREMENT TABLE;[03] FABRICATED NEW CLIP FROM BAC1489-360 LOT# 1464682-1 .050' IAW DWG PL 141A1311; LOCATED AND DRILL HOLES IAW SRM 51-40-05-0G-0.;[04] SRM 53-10-15-1A-1 DOES NOT COVER CRACKS AT A FASTENER HOLE. OUT OF LIMITS IAW SRM 51-10-02-0G-0 STEP 9; REPLACEMENT OF PART.;[05] OK TO APPLY CHEMICAL CONVERSION AND PRIMER TO FABRICATED CLIP.;[06] VERIFIED CORRECTIVE ACTION 1-5. OK TO PRIME;[07] UPDATED THICKNESS ON MEASUREMENT TABLE;[08] CERTIFY;[09] APPLIED CHEMICAL CONVERSION AND PRIMER IAW SRM 51-20-01-0G-0 & AMM 51-21-72-370-804;[10] OK TO INSTALL;[11] VERIFIED CORRECTIVE ACTION 9; 10 AND MEASUREMENT TABLE. OK TO INSTALL.;[12] INSTALLED CLIP AT BS 294 STR 13 L/H IAW SRM 51-40-02-0G-0; DWG 141A1311;[13] VERIFIED CORRECTIVE ACTION 12.

Part: STRINGER CLIP — CRACKED (PAX CABIN) · airframe 58,974 hrs · 35,001 cycles

CRACK ON PASSENGER CABIN STRINGER CLIP AT BS 277 R/H STRINGER 10.(MARKED) / [01] CLEANED PASSENGER CABIN STRINGER CLIP AT BS 277 R/H STRINGER 10.;[02] VERIFIED WORK PERFORMED;[03] NDT HFEC SURFACE INSPECTED AREA PER 737 NDTM PART 6 51-00-00 PROC 23; LARGE SEVERED CRACK NOTED; EDGE TO FASTENER.<BR>EQUIP ID. NORTEC 500D IS000681 DUE 02/23;[04] REMOVED CABIN STRINGER CLIP DUE TO NOT ALLOWABLE LIMITS FOUND AND REPLACED NEW STRINGER CLIP BS277 STR 10R/H IAW SRM 51-10-02-0G-0 PAR. 9.C REPLACEMENT OF THE PART AND SRM 51-40-02 0G-0 SRM 51-40-05-0G-0 AND DWG # 141A1110;[05] VERIFIED CRACKED STRINGER CLIP WAS REPLACED WITH NEW STRINGER CLIP.;[06] VERIFIED CORRECTIVE ACTION #4<BR>VERIFIED MEASUREMENTS

Part: FLOOR PANEL — FRAYED · airframe 58,974 hrs · 35,001 cycles

AFT FLOOR PANEL 242VF UPPER SKIN FRAYED AT SEVERAL PLACES / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 6 TABLE 6.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>REMOVED 5EA THROUGH INSERTS TO FACILITATE REPAIR IAW SRM 53-00-50-2R-1 PARA 3.B.<BR>REMOVED DAMAGED SKIN AND CLEANED REPAIR AREA IAW SRM 53-00-50-2R-1 PARA 3C;E-F.;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1.;[03] VERIFIED CORRECTIVE ACTION #1; 2;[04] FABRICATED REPAIR PLIES FROM BMS 9-3H2 LOT#1493221-1 IAW SRM 53-00-50-2R-1 PARA 3K.<BR>OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION #4;[06] INSTALLED REPAIR PLIES USING BMS 8-201 LOT#1482288-1; VACUUM BAGGED; LEAK CHECK GOOD USING VACUUM VACUUM GAUGE ID:E11543 DUE:08/2022 IAW SRM 53-00-50-2R-1 PARA 3.K(1)L(1).;[07] VERIFIED CORRECTIVE ACTION STEP 6.;[08] COMPLETED CURE AND UNBAGGED REPAIR; INSTALLED 5EA THROUGH INSERTS USING BMS 5-107 LOT#AK1KP9159K IAW SRM 53-00-50-2R-1 PARA 3.M; N.<BR>USED THERMOMETER ID:ATS2208 CAL DUE 10/2022;[09] VERIFIED CORRECTIVE ACTION ITEM 8;[10] ATTACHED CURE SHEETS;[11] VERIFIED REPAIR COMPLETE.;[12] VERIFIED MEASUREMENT FIELDS; FAULT COMPLETE.

Part: FLOOR PANEL — FRAYED · airframe 58,974 hrs · 35,001 cycles

AFT FLOOR PANEL 241ADF UPPER SKIN FRAYED AT SEVERAL PLACES / [01] IDENTIFIED AFT FLOOR PANEL 241ADF IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F. DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>REMOVED DAMAGED SKIN AND CLEANED REPAIR AREA IAW SRM 53-00-50-2R-1 PARA 3.A;C.E&F.;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1.;[03] VERIFIED CORRECTIVE ACTION #1; 2;[04] FABRICATED REPAIR PLIES USING BMS 9-3 LOT#1493221-1 IAW SRM 53-00-50-2R-1 PARA 3.K<BR>OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION #4<BR>VERIFIED MEASUREMENTS;[06] INSTALLED REPAIR PLIES USING BMS 8-201 LOT#1482288-1; VACUUM BAGGED; LEAK CHECK GOOD USING VACUUM VACUUM GAUGE ID:ATS2545 DUE:08/2022 IAW SRM 53-00-50-2R-1 PARA 3.K(1)L(1).;[07] VERIFIED CORRECTIVE ACTION STEP 6.;[08] CURED REPAIR PLIES USING THERMOMETER ID:ATS2209 DUE:10/2022; UNBAGGED; AND TRIMMED EXCESS MATERIAL IAW SRM 53-00-50-2R-1 PARA 3.M;[09] VERIFIED CORRECTIVE ACTION 8;[10] VERIFIED COMPLETION OF REPAIR IAW SRM 53-00-50-2R-1 ON FRAYED UPPER SURFACE SKIN OF PANEL 241ADF;[11] VERIFIED CORRECTIVE ACTION 10;[12] VERIFIED CORRECTIVE ACTION 10

Part: SEAL DEPRESSOR — CRACKED (FWD SERVICE DOOR) · airframe 58,974 hrs · 35,001 cycles

FSD UPPER HINGE CUTOUT UPPER REVEAL IS CRACKED. / [01] LOCATED AND DRILLED NEW SEAL DEPRESSOR P/N 141A8372U1 LOT# 1485850-1 I.A.W. B737-700 SRM 51-40-05-0G-0 FIGURE 2 AND FIGURE 3 TABLE A. OK TO INSTALL NEW SEAL DEPRESSOR FORWARD SERVICE DOOR CUTOUT.;[02] VERIFIED COERRECTIVE ACTION1. OK TO INSTALL SEAL DEPRESSOR.;[03] INSTALLED NEW UPPER REVEAL (SEAL DEPRESSOR) PER SRM 51-40-02-0G-0 AND DWG 141A8370.;[04] CERTIFIED CORRECTIVE ACTION 3;[05] UPDATED PARTS;[06] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 3.;[07] APPLIED FILLET SEAL IAW B737-700 AMM 51-31-00-390-804; APPLIED PROTECTIVE FINISHES IAW B737-700 AMM 51-21-72-370-801 AND 51-21-73-370-801; APPLIED FILL AND FAIR COMPOUND IAW B737-700 AMM 53-11-01-420-801;[08] VERIFIED CORRECTIVE ACTION 7; STEP 1 AND MEASUREMENT TABLE;[09] COMPLETED STEP 2;[10] TASK CARD COMPLETE;[11] VERIFIED;[12] VERIFIED STEP 2. WORKSCOPE COMPLETE

Part: SUPPORT FITTING — CORRODED (FWD ENTRY DOOR) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON FED GIRT BAR LATCH SUPPORT FITTING BS312 LBL9. MARKED. / [01] PITTING CORROSION EXCEEDS 50% OF MACHINED THICKNESS ON UPPER SURFACE OF FITTING. SRM DOES NOT HAVE ALLOWABLE DAMAGE LIMITS FOR GIRT BAR LATCH FITTINGS. R&R IAW SRM 51-10-02-0G-0 STEP 9.;[02] UPDATED MEASUREMENT TABLE;[03] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE;[04] REMOVED FED GIRT BAR FITTING AT B.S. 312 LBL56 IAW SRM 51-40-02-0G-0;[05] OK TO INSTALL FED FWD GIRT BAR FITTING M;[06] VERIFIED CORRECTIVE ACTION 5. OK TO INSTALL NEW GIRT BAR SUPPORT FITTING.;[07] INSTALLED FED FWD GIRT BAR FITTING IAW SRM 51-40-02-OG-0 AND AIPC 53-42-00-29 .;[08] VERIFIED CORECTIVE ACTION 7.;[09] REMOVED AND REPLACED FED FWD BS312 LBL9. GIRT BAR LATCH SUPPORT FITTING IAW SRM 51-40-02-0G-0 AND AIPC 53-42-00-29 .<BR>SCREW GUN USED ATS547 SERIAL # UNKNOW DUE DATE 02/2023 <BR>ALL AMT BLOCKS COMPLETED .;[10] VERIFIED CORRECTIVE ACTION 9;[11] WORKSCOPE COMPLETE.

Part: INTERCOSTAL — CRACKED (PAX CABIN) · airframe 58,974 hrs · 35,001 cycles

CRACKED INTERCOSTAL AT FWD CABIN BS284 BL0 WL208. MARKED. / [01] UPDATED MEASUREMENTS. CRACKED INTERCOSTAL FOUND TO BE OUT OF LIMITS AND WILL BE REPLACEMENT OF THE PART IAW SRM 51-10-02 STEP 9. REMOVED CRACKED INTERCOSTAL AT BS284 BL0 WL208 IAW SRM 51-40-02. RECEIVED NEW INTERCOSTAL LOT#240015; LOCATED FASTENER HOLES; DRILLED; AND DEBURRED IAW SRM 51-40-05; AND BOEING DWG 141A5400. ALSO; OK TO INSTALL.;[02] VERIFIED CORRECTIVE ACTION #1;[03] INSTALLED A NEW INTERCOSTAL AT BS284 BL0 WL208 IAW SRM 51-40-02 AND BOEING DWG 141A5400.;[04] VERIFIED CORRECTIVE ACTION #3

Part: CHANNEL — CRACKED (FWD ENTRY DOOR) · airframe 58,974 hrs · 35,001 cycles

CRACKED FWD ENTRY DOOR MOP SILL BS303 LBL55 WL208. MARKED. / [01] FED MOPSILL AT B.S 303 LBL55 WL208 IS CRACKED ON VERTICAL FLANGE. OUT OF LIMITS IAW SRM 53-10-15-1A-1. STARTED FASTENER REMOVAL IAW SRM 51-40-02-0G-0.;[02] UPDATED MEASUREMENT TABLE;[03] REMOVED FED MOPSILL IAW SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW FED MOPSILL IAW SRM 51-40-05-0G-0; DWG 141A8110;[05] VERIFIED CORRECTIVE ACTION 4.;[06] OK TO INSTALL FED MOPSILL;[07] VERIFIED CORRECTIVE ACTION 6; OK TO INSTALL GIVEN.;[08] 100% OF ALL PERMANENT OR TEMPORY FASTENERS HAVE BEEN INSTALLED WITH FAYING SURFACE SEALED LOCATIONS WITH IN SEALANT SQUEEZE OUT TIME.;[09] VERIFIED CORRECTIVE ACTION 8.;[10] COMPLETED INSTALLATION OF FED MOPSILL IAW SRM 51-40-02-0G-0; DWG 141A8110;[11] VERIFIED CORRECTIVE ACTION 10.;[12] VERIFIED MEASUREMENT TABLE.

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 58,974 hrs · 35,001 cycles

CRACKED INTERCOSTAL AT FWD CABIN BS353 LBL11 WL208. / [01] VERIFIED APPLICABILITY PER SRM 53-00-04-1A-1 AND BOEING DWG 141A5400<BR><BR>LOCATED AND MATCH DRILLED NEW INTERCOSTAL AT FWD CABIN BS349 LBL11 WL208 IAW SRM 51-40-05 AND BOEING DWG 141A5400;[02] VERIFIED;[03] REQUEST OK TO INSTALL INTERCOSTAL LBL11 BS 344-360;[04] VERIFIED CORRECTIVE ACTIONS 1 AND 3.;[05] INSTALLED NEW INTERCOSTAL AT BS 353 LBL11 WL208 IAW SRM 51-40-02 AND DRAWING 141A5400 REV A DATED 11-3-98;[06] UPDATED TO PRIMARY;[07] CERTIFY;[08] VERIFIED MEASUREMENT TABLE.;[09] VERIFIED CORRECTIVE ACTION 5.

Part: INTERCOSTAL — CRACKED (FWD CABIN) · airframe 58,974 hrs · 35,001 cycles

CRACKED INTERCOSTAL AT FWD CABIN BS294+6 RBL31. MARKED. / [01] REMOVED HI-LOCKS FROM INTERCOSTAL AT FWD CABIN BS 294+6 RBL 31 <BR>IAW SRM 51-40-02-0G-0.;[02] VERIFIED APPLICABILITY PER SRM 53-00-04-1A-1 AND BOEING DWG 141A5400<BR>REPAIR PER REPLACEMENT PER SRM 53-00-04-1A-1<BR>LOCATED AND MATCH DRILLED NEW INTERCOSTAL AT FWD CABIN BS294+6 RBL31 WL208 IAW SRM 51-40-05 AND BOEING DWG 141A5400;[03] VERIFIED CORRECTIVE ACTIONS #1 AND 2; AND UPDATING OF MEASUREMENTS;[04] VERIFIED CORRECTIVE ACTION 1-3 OK TO INSTALL;[05] INSTALLED INTERCOSTAL AT FWD CABIN BS294+6 RBL31 IAW SRM 51-40-02 AND BOEING DWG 141A5400;[06] VERIFIED;[07] VERIFIED CORRECTIVE ACTION ITEM 5.<BR><BR>** FLOOR PANEL FASTENER HOLES REQUIRE LOCATION AND DRILLING.;[08] VERIFIED APPLICABILITY PER SRM 53-00-04-1A-1 AND BOEING DWG 141A5400<BR>REPAIR PER REPLACEMENT PER SRM 53-00-04-1A-1<BR>LOCATED AND MATCH DRILLED NEW INTERCOSTAL AT FWD CABIN BS294+6 RBL31 WL208 IAW SRM 51-40-05 AND BOEING DWG 141A5400 <BR>UPDATED MEASUREMENTS TABLE.;[09] VERIFIED;[10] LOCATED AND DRILLED FLOOR PANEL HOLES IAW SRM 51-40-05-0G-0;[11] VERIFIED CORRECTIVE ACTION #5; 8<BR>VERIFIED MEASUREMENTS

Part: INTERCOSTAL — CRACKED (FWD CABIN) · airframe 58,974 hrs · 35,001 cycles

CRACKED INTERCOSTAL AT FWD CABIN BS353 RBL11 WL208. / [01] UPDATED STEP 1 AND VERIFIED APPLICABILITY PER SRM 53-00-04-1A-1 AND BOEING DWG 141A5400<BR><BR>LOCATED AND MATCH DRILLED NEW INTERCOSTAL AT FWD CABIN BS349 RBL11 WL208 IAW SRM 51-40-05 AND BOEING DWG 141A5400;[02] VERIFIED;[03] REQUEST OK TO INSTALL INTERCOSTAL RBL 11 BS 344-360;[04] VERIFIED CORRECTIVE ACTIONS 1 AND 3.;[05] COMPLETED STEP 1;[06] INSTALLED NEW INTERCOSTAL BS 353 RBL11 WL208 IAW SRM 51-40-02 AND DRAWING 141A5400 REV- DATED 2-24-96;[07] UPDATED TO PRIMARY;[08] CERTIFY;[09] VERIFIED MEASUREMENT TABLE.;[10] VERIFIED CORRECTIVE ACTION 6.

Part: INTERCOSTAL — CRACKED · airframe 58,974 hrs · 35,001 cycles

CRACKED INTERCOSTAL AT FWD CABIN BS349 BL0 WL208. / [01] LOCATED AND MATCH DRILLED NEW INTERCOSTAL AT FWD CABIN BS349 BL0 WL208 IAW SRM 51-40-05 AND BOEING DWG 141A5400;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION 1;[04] INSTALLED INTERCOSTAL IAW SRM 51-4-02 AND BOEING DWG 141A5400;[05] INSTALLED INTERCOSTAL IAW SRM 51-40-02 AND BOEING DWG 141A5400;[06] VERIFIED;[07] VERIFIED APPLICABILITY PER SRM 53-00-04-1A-1 AND BOEING DWG 141A5400 DAMAGE OUT OF LIMITS IAW SRM 53-00-04-1A-1 AND SRM 53-10-04-2R-1 UPDATED MEASUREMENTS AND INSTALLED INTERCOSTAL IAW SRM 51-40-02 AND BOEING DWG 141A5400;[08] VERIFIED;[09] VERIFIED CORRECTIVE ACTION ITEM 7. CONFIRMED SRM 53-00-04-1A-1 APPLICABILITY FOR DAMAGE LIMITS; PART BEING REPAIRED BY REPLACEMENT.VERIFIED MEASUREMENT TABLE.;[10] INTERCOSTAL AT BS 349 BL 0 WL 208 WAS REMOVED FOR ACCESS ON FAULT TTG8Q00DG8U7;[11] REINSTALLED INTERCOSTAL AT BS 349 BL0 WL208 IAW SRM 51-40-02 AND DRAWING 141A5400 REV - DATED 08-13-96;[12] UPDATED TO PRIMARY;[13] CERTIFY;[14] VERIFIED CORRECTIVE ACTION 11.

Part: SUPPORT ANGLE — CORRODED (FWD SERVICE DOOR) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON FSD THRESHOLD SUPPORT ANGLE BS305 - BS323 RBL57. MARKED. / [01] FOUND SRM 53-10-15-1A-2 IS APPLICABLE FOR CORROSION REMOVAL AT BS 305-323 RBL 57 WL 209;[02] REMOVED CORROSION IN MULTIPLE AREAS ON FSD THRESHOLD SUPPORT ANGLE AT BS 305-323; RBL 57. DEEPEST BLENDOUT AT BS 313-316; RBL 57 MEASURES 3'X1'; MAX DEPTH .014'. ORIGINAL THICKNESS IS .090'; CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-15-1A-2. MEASURED WITH MICROMETER CAL ID: IS000459 CAL DATE: 01/2022.<BR><BR>REMOVED FSD THRESHOLD SUPPORT ANGLE AT BS 295-326; RBL 57; PER SRM 51-40-02-0G-0.;[03] VERIFIED ACTION #1;2;[04] LOCATED AND DRILLED NEW FSD THRESHOLD SUPPORT ANGLE AT BS 295-326; RBL 57 PER DWG 141A8310 SHEET 23 AND SRM 51-40-05.;[05] VERIFIED ITEM 4 CORRECTIVE ACTIONS. <BR>VERIFIED MEASUREMENTS.;[06] INSTALLED FSD THRESHOLD SUPPORT ANGLE AT BS 295-326; RBL 57 PER DWG 141A8310 SHEET 23 AND SRM 51-40-05.;[07] VERIFIED CORRECTIVE ACTIONS STEP 6.;[08] COMPLETE

Part: FLOOR SUPPORT — CORRODED (FWD CABIN) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON FLOOR SUPPORT AT FWD CABIN BS330 LBL11. MARKED. / [01] UPDATED MEASUREMENTS LIST.;[02] DAMAGE EVALUATION; ORIGINAL THICKNESS .080. <BR>CORROSION MATERIAL LOSS MEASURES (.022) FOUND TO BE OUT OF LIMITS AS PER SRM 53-10-04-0I-1.;[03] UPDATING TO ADD TOOL ID.<BR>DEPTH GAUGE:<BR>TOOL ID:ATS2678<BR>S/N: UNKNOWN<BR>DUE: 04/2023<BR><BR>DIAL CALIPER 6':<BR>TOOL ID:NCX000336<BR>S/N: UNKNOWN<BR>DUE: 06/2023;[04] VERIFIED;[05] LOCATED AND MATCH DRILLED NEW INTERCOSTAL REPLACEMENT IN ACCORDANCE WITH SRM 51-40-05-0G-0.;[06] VERIFIED;[07] SRM 53-10-04-OI-1 IS APPLICABLE FOR ALLOWABLE DAMAGE.;[08] VERIFIED APPLICABILITY OF SRM 53-10-04-OI-1;[09] LOCATED AND MATCH DRILLED NEW INTERCOSTAL REPLACEMENT IN ACCORDANCE WITH SRM 51-40-05-0G-0 AND DRAWING: 141A5410.;[10] VERIFIED STEP 9;[11] VERIFIED CORRECTIVE ACTIONS 2; 3; 7; 9.<BR>OK TO INSTALL;[12] INSTALLED NEW INTERCOSTAL; PICKED UP FLOORBOARD HOLES AND INSTALLED NEW NUTPLATES IAW SRM 51-40-02-0G-0; 141A5410; IAW 51-40-05; SRM 51-40-10-2R-0 AND DRAWING 141A5410.;[13] VERIFIED;[14] RII VERIFIED CORRECTIVE ACTION ITEM 12-13.;[15] ALL STEPS COMPLETE; CARD COMPLETE. MEASUREMENT FIELD ITEM 18 REQUIRES THICKNESS REMAINING NOT N/A; ITEM 22 REQUIRES 'MINOR' REPAIR NOT N/A.;[16] UPDATED ITEM 22 OF CHART;[17] CERTIFY;[18] COMPLETE;[19] CORRECTED P/N;[20] CERTIFY;[21] VERIFIED MEASUREMENT TABLE.

Part: FITTING — CORRODED (FWD ENTRY DOOR) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON FED GIRT BAR LATCH SUPPORT FITTING BS344 LBL14. MARKED. / [01] PITTING CORROSION EXCEEDS 50% OF MACHINED THICKNESS ON UPPER SURFACE OF FITTING. SRM DOES NOT HAVE ALLOWABLE DAMAGE LIMITS FOR GIRT BAR LATCH FITTINGS. R&R IAW SRM 51-10-02-0G-0 STEP 9.;[02] UPDATED MEASUREMENT TABLE;[03] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE;[04] REMOVED FED AFT GIRT BAR FITTING AT BS344 LBL60 IAW SRM 51-40-02-0G-0;[05] OK TO INSTALL FED AFT GIRT FITTING .;[06] VERIFIED CORRECTIVE ACTION 5 AND MEASUREMENT TABLE. OK TO INSTALL NEW GIRT BAR SUPPORT FITTING.;[07] INSTALLED FED AFT GIRT FITTING IAW SRM 51-40-02-0G-0 AND AIPC 53-42-00-29 .;[08] VERIFIED CORRECTIVE ACTION 7.;[09] REMOVED AND REPLACED FED AFT GIRT BAR LATCH SUPPORT FITTING IAW SRM 51-40-02-0G-0 AND AIPC 53-42-00-29 .<BR>SCREW GUN USED ATS547 SERIAL # UNKNOW DUE DATE 02/2023 <BR>ALL AMT BLOCKS COMPLETED .;[10] VERIFIED CORRECTIVE ACTION 9.;[11] WORKSCOPE COMPLETE.

Part: SUPPORT ANGLE — CORRODED (FWD CABIN) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON THRESHOLD SUPPORT ANGLE AT FWD PASSENGER CABIN BS318 TO 338 LBL59. MARKED / [01] UPDATED MEASUREMENT TABLE;[02] REMOVED CORROSION ON THRESHOLD SUPPORT ANGLE AT FWD CABIN BS318 TO 338 LBL59 IN A 1X1.5X.010' AREA IAW SRM 51-10-02-0G-0. ORIGINAL THICKNESS .080'. OUT OF LIMITS IAW SRM 53-10-15-1A-1.;[03] BLENDS MEASURED BY DIAL DEPTH GAUGE ATS2678; S/N UNKNOWN; DUE 04/2023AC;[04] CERTIFY;[05] VERIFIED CORRECTIVE ACTION #2<BR>VERIFIED MEASUREMENT TABLE;[06] LOCATED AND DRILLED NEW THRESHOLD SUPPORT ANGLE IAW SRM 51-40-05-0G-0; DWG 141A8112;[07] OK TO INSTALL THRESHOLD SUPPORT ANGLE TO FED MOPSILL;[08] VERIFIED CORRECTIVE ACTIONS 6 AND 7. OK TO INSTALL GIVEN.;[09] INSTALLED THRESHOLD ANGLE SUPPORT TO THE FED MOPSILL IAW SRM 51-40-02-0G-0; DWG 141A8110;[10] VERIFIED CORRECTIVE ACTION 9.;[11] UPDATED CHART TO LEVEL 2;[12] CERTIFY

Part: FRAME — CRACKED (CABIN FLOOR) · airframe 58,974 hrs · 35,001 cycles

FWD PASSENGER CABIN CRACKED FRAME AT BS312 11' BELOW S-4L WL283. MARKED. / [01] REMOVED DAMAGE ON FRAME AT BS312; 11' BELOW S-4L WL283 IAW SRM 51-10-02.;[02] REMOVED DAMAGE ON FRAME AT BS312; 11' BELOW S-4L WL283 IN AN AREA OF 1' X .2' IAW SRM 51-10-02.;[03] REQUEST NDI FOR CRACK FREE CONDITION ON FRAME AT BS312; 11' BELOW S-4L WL283.;[04] HFEC INSPECTED CUTOUT AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23;[05] COMPLETE;[06] CERTIFY;[07] REPAIRED ON EA FAULT TTG8Q00DKPDE;[08] VERIFIED REPAIRED ON EA FAULT TTG8Q00DKPDE;[09] VERIFIED REPAIRED ON EA FAULT TTG8Q00DKPDE AND MEASUREMENT TABLE.

Part: BEAR STRAP — CRACKED (FWD SERVICE DOOR) · airframe 58,974 hrs · 35,001 cycles

PASSENGER CABIN FSD CUTOUT BARE STRAP CRACKED BS299; 3' BELOW FWD UPPER DOOR STOP FITTING. MARKED. / LOCATED & DRILLED NEW UPPER STUB FRAME P/N 141A8370U13 LOT# 1497302-1 P.O. CERT# 875637 I.A.W B737-700 SRM 51-40-05-0G-0 FIGURE 2 & FIGURE 3 TABLE A. OK TO INSTALL NEW UPPER STUB FRAME FSD CUTOUT.;[07] VERIFIED CORRECTIVE ACTION 6 AND MEASUREMENT TABLE. OK TO INSTALL THE STUB FRAME;[08] INSTALLED 100% OF PERMANENT FASTENERS PER SRM 51-40-02-0G-0 AND DWG 141A8370.;[09] INSTALLED 100% OF PERMANENT FASTENERS AT FSD NEW UPPER STUB FRAME P/N 141A8370U13 PER SRM 51-40-02-0G-0 AND DWG 141A8370.;[10] CERTIFIED CORRECTIVE ACTION 9;[11] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 9.;[12] UPDATED STEPS 1 AND 5.;[13] UPDATED STEPS 1 AND 5 AS COMPLETE. INSTALLED IN CORRECTIVE ACTION 9 AND INSPECTED IN CORRECTIVE ACTION 11;[14] APPLIED FILLET SEAL IAW B737-700 AMM 51-31-00-390-804; APPLIED PROTECTIVE FINISHES IAW B737-700 AMM 51-21-72-370-801 AND 51-21-73-370-801; APPLIED FILL & FAIR COMPOUND IAW B737-700 AMM 53-11-01-420-801;[15] VERIFIED CORRECTIVE ACTION 14 AND STEPS 2;3;4.;[16] VERIFIED MEASUREMENT TABLE.;[17] ADJUSTED FORWARD UPPER LATCH FITTING; FSD PER AMM 52-41-00-820-801 STEP 2N; AMM 52-71-11-710-801; FSD CHECKS GOOD;

Part: FLOORBEAM — CORRODED · airframe 58,974 hrs · 35,001 cycles

CORROSION ON FLOORBEAM AT AFT WET AREA BS986 LBL34 - LBL43. MARKED. / [01] VERIFIED APPLICABILITY PER SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] REMOVED DAMAGE ON BS986 FLOOR BEAM UPPER CHORD FLANGE LBL34-LBL43 WL208 9'X1' AND FOUND TO BE OUT LIMIT AT NUT PLATE LOCATION LBL43 ORIGINAL MAT. THICKNESS IS 0.150' REMAINING MATERIAL THICKNESS IS .090 AND FLOORBOARD HOLE LBL41 ORIG MAT.THICKNESS .150' REMAINING MATERIAL THICKNESS IS 0.120' ALL I.A.W SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 PAR 4.D(2) FIG.103/ALLOWQABLE DAMAGE 1 DETAIL C;E DAMAGE TO BE REPAIRED PER SRM 53-70-51-2R-4 REPAIR 4;[03] DAMAGED ON BS986 LBL34-LBL43 WL208 UPPER CORD TO BE REPAIRED PER SRM 53-70-51-2R-4 REPAIR 4 ON COSTUMER CARD TTG8Q00DFLPB;[04] VERIFIED CORRECTIVE ACTION #3;[05] VERIFIED DAMAGE ON BS986 LBL34-LBL43 WL208 UPPER CORD TO BE REPAIRED PER SRM 53-70-51-2R-4 REPAIR 4 ON COSTUMER CARD TTG8Q00DFLPB;[06] TASK COMPLETE;[07] VERIFIED MEASUREMENT TABLE

Part: WEB — CORRODED · airframe 58,974 hrs · 35,001 cycles

CORROSION ON WEB AT AFT WET AREA BS1016 LBL11; LBL34. MARKED. / [01] NO ALLOWABLE LIMITS FOUND ON SRM FOR BS1016 L/H SHEAR WEB ;REMOVED AND REPLACED OF THE PART IS APPLICABLE I.A.W SRM 51-10-02-0G-0 PAR 9.C ALL REMOVAL AND REPLACED TO BE ACCOMPLSHED ON COSTUMER CARD TTG8Q00DFLMW ALL AMT BLOCKS COMPLETED;[02] VERIFIED CORRECTIVE ACTION 1.;[03] UPDATED TABLE MEASUREMENT;[04] VERIFIED MEASUREMENT TABLE JOB COMPLETE

Part: WEB — CORRODED · airframe 58,974 hrs · 35,001 cycles

CORROSION ON WEB AT AFT WET AREA BS1028 LBL4 TO LBL19. MARKED. / [01] NO ALLOWABLE LIMITS FOUND ON SRM FOR BS1028 LBL4-LBL19 SHEAR WEB ;REMOVED AND REPLACED OF THE PART IS APPLICABLE I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED BS1016<BR>L/H SHEAR WEB I.A.W SRM 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW L/H SHEAR WEB BS1016 I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 147A5600;[04] VERIFIED CORRECTIVE ACTION 3.;[05] OK TO INSTALL;[06] OK TO INSTALL GIVEN.;[07] UPDATED TABLE MEASUREMENT;[08] INSTALLED NEW L/H SHEAR WEB BS1016 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600;[09] VERIFIED MEASUREMENT TABLE.;[10] VERIFIED CORRECTIVE ACTION 8.

Part: WEB — CORRODED · airframe 58,974 hrs · 35,001 cycles

CORROSION ON 1016 WEB AT AFT WET AREA BS1016 RBL6. MARKED. / [01] BEGAN REMOVING FASTENERS COMMON TO WEB BS1016-BS1031 BL0-RBL37 IAW SRM 51-40-02.;[02] NO ALLOWABLE LIMITS FOUND ON SRM FOR BS1016 SHEAR WEB ;REMOVED AND REPLACED OF THE PART IS APPLICABLE I.A.W SRM 51-10-02-0G-0 PAR 9.C;[03] REMOVED BS1016 R/H SHEAR WEB I.A.W SRM 51-40-02-0G-0;[04] REPLACEMENT OF THE BS1016 R/H SHEAR WEB TO BE COMPLETED ON COSTUMER CARD TTG8Q00DFLLX ALL AMT BLOCKS COMPLETED;[05] VERIFIED CORRECTIVE ACTION 4.;[06] ADDITION TO CORRECTIVE ACTION 5; VERIFIED MEASUREMENT TABLE.;[07] UPDATED CORROSION TABLE

Part: TENSION TIE — CORRODED · airframe 58,974 hrs · 35,001 cycles

CORROSION ON TENSION STRAP AT AFT WET AREA BS1016 - BS1028 LBL3. MARKED. / [01] NOT LIMITS FOUND ON MANUAL; PART TO BE REPLACED IAW SRM 51-10-02 PART REPLACEMENT; REMOVED DAMAGED STRAP; LOCATED AND DRILLED NEW STRAP P/N 147A5620U3 IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-0 AND DWG 147A5600. AND OK TO INSTALL.;[02] VERIFIED CORRECTIVE ACTION #1;[03] INSTALLED NEW STRAP P/N 147A5620U3 IAW SRM 51-40-02-0G-0 AND DWG 147A5600.;[04] VERIFIED MEASUREMENT TABLE.;[05] VERIFIED CORRECTIVE ACTION 3.

Part: FRAME — CRACKED · airframe 58,974 hrs · 35,001 cycles

CRACKED FRAME AT AFT PASSENGER CABIN S-8L BS927. MARKED. / [01] REMOVED FRAME TO BIN RAIL ATTACH ANGLE BS 927; STR 8L FOR ACCESS IAW SRM 51-40-02-0G-0. NO VISUAL SIGN OF CRACK ON FRAME;[02] VERIFIED CORRECTIVE ACTION #1;[03] REQUEST NDI FOR CRACK FREE CONDITION ON BS 927 FRAME AT STR 8L;[04] HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23 <BR>-MINIMITE ID: IS000934 CAL DUE: 08/22;[05] UPON FURTHER INVESTIGATION FOUND THERE TO BE NO CRACK ON BS 927 FRAME AT STR 8L;[06] REINSTALLED FRAME TO BIN RAIL ATTACH ANGLE BS 927; STR 8L IAW SRM 51-40-02-0G-0; DWG# 147A1027.;[07] VERIFIED CORRECTIVE ACTIONS #5 AND #6

Part: BRACKET — LOOSE (CABIN FLOOR) · airframe 58,974 hrs · 35,001 cycles

LOOSE FASTENERS CHAFING ON INTERCOSTAL AT FWD PASSENGER CABIN BS277 3' OB OF S-2R WL282. / [01] GAINED ACCESS BY REMOVING COCKPIT DOOR POST PER SRM 51-40-02;[02] REMOVED CHAFFED BRACKET AT BS 277 ;3' OUTBD OF STR 2R; WL 282 IAW SRM 51-40-02;[03] LOCATED NEW BRACKET AND DRILLED IAW SRM 51-40-05 AND DRAWING 141A9402 REV E DATED 9-28-07. OK TO INSTALL REQUESTED;[04] UPDATED CHART;[05] VERIFIFIED CORRECTIVE ACTION 2.;[06] VERIFIED MEASUREMENT TABLE.;[07] INSTALLED NEW BRACKET AND REINSTALLED DOOR POST IWA SRM 41-40-02 AND DWG #141A9402 REV:E DATE 08/16/2022;[08] JOB COMPLOTTED;[09] CORRECT THE STEP #7 <BR>INSTALLED NEW BRACKET AND REINSTALLED DOOR POST IWA SRM 51-40-02 AND DWG #141A9402 REV:E DATE 11-15-07;[10] VERIFIED CORRECTIVE ACTION 9.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON FLOOR BEAM AT AFT WET AREA BS986 RBL36 - RBL43. MARKED. / [01] VERIFIED APPLICABILITY PER SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] REMOVED DAMAGE ON BS986 FLOOR BEAM UPPER CHORD FLANGE RBL36-RBL43 WL208 7'X1' AND FOUND TO BE OUT LIMIT AT NUT PLATE LOCATION RBL43 ORIGINAL MAT. THICKNESS IS 0.150' REMAINING MATERIAL THICKNESS IS .090 AND FLOORBOARD HOLE RBL36 ORIG MAT.THICKNESS .150' REMAINING MATERIAL THICKNESS IS 0.110' ALL I.A.W SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 PAR 4.D(2) FIG.103/ALLOWQABLE DAMAGE 1 DETAIL C;E DAMAGE TO BE REPAIRED PER SRM 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 2 FROM LBL50-RBL50. INSTALLED NEW L/H AND R/H SHEAR TIES BS 986 LBL50 AND RBL50,INSTALLED 2 FLOOR SUPPORT AT BS967-BS986 LBL17 AND RBL17 WL208 RECORD ON STEP 1,INSTALLED FLOOR SUPPORT AT BS986-BS1002 RBL45 WL208,INSTALLED MOPSILL SUPPORT AT BS967-BS986 RBL45 WL208,INSTALLED MOPSILL AT BS967-BS986 LBL45,INSTALLED FLOOR SUPPORT AT BS986-BS1002 LBL45,INSTALLED FLOOR SUPPORT AT BS986-BS1004 LBL43 WL208 ALL I.A.W SRM 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 1 PAR 4.N,O,S BOEING DWGS 145A5730,147A5600,147A8501,147A0000 FIG204 AND EA. 22-153-02093-WIP1. INSTALLED FASTENER BS975-1006 WL208 LBL50-RBL50 COMMON TO THE REPAIR APPLIED FILLET SEAL PRIMED FASTENER HEAD AND CIC ALL I.A.W SRM 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 1 PAR 4.O-Q COMPLETED ALL REPAIIR TASK I.A.W SRM 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 1 AND EA. 22-153-02093-WIP1.

Part: TENSION TIE — CORRODED (AFT WET AREA) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON TENSION STRAP AT AFT WET AREA BS1016 RBL3. MARKED. / [01] NOT LIMITS FOUND ON MANUAL; PART TO BE REPLACED IAW SRM 51-10-02 PART REPLACEMENT; REMOVED DAMAGED STRAP; LOCATED AND DRILLED NEW STRAP P/N 147A5744U1 IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-0 AND DWG 147A5600. AND OK TO INSTALL.;[02] VERIFIED CORRECTIVE ACTION #1;[03] INSTALLED NEW STRAP P/N 147A5744U1 IAW SRM 51-40-02-0G-0 AND DWG 147A5600.;[04] VERIFIED MEASUREMENT TABLE.;[05] VERIFIED CORRECTIVE ACTION 3.

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,974 hrs · 35,001 cycles

FWD FLOOR PANEL 222BF UPPER SURFACE HAS AREAS OF PULLED STRANDS. / REMOVED ALL INSERTS TO FACILITATE REPAIR IAW SRM 53-00-50-2R-1 PARA 3B<BR>REMOVED PREVIOUS REPAIR AND ALL DAMAGE NOTED AND CLEANED REPAIR AREAS IAW SRM 53-00-50-2R-1 PARA 3C-F;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1.;[03] CORRECTION TO ITEM 1: PANEL IS 222BF NOT 222DF.;[04] VERIFIED CORRECTIVE ACTION 1 AND 3 COMPLETED;[05] FABRICATED REPAIR PLIES FROM BMS 9-3 H2 LOT#1493221-1; OK TO INSTALL IAW SRM 53-00-50-2R-1 PARA 3K;[06] VERIFIED CORRECTIVE ACTION #5;[07] INSTALLED REPAIR PLIES USING BMS8-201 TYPE 4 LOT#1482288-1; VACUUM BAGGED; CHECKED FOR LEAKS; LEAK CHECKED GOOD AND SET FOR CURE IAW SRM 53-00-50-2R-1 PARA 3K-M<BR><BR>USED VACUUM GAUGE ATS2107 CAL DUE DATE 09/2022;[08] VERIFIED CORRECTIVE ACTION #7;[09] CURED REPAIR PLIES USING THERMOMETER ATS2208 CAL DUE DATE 10/2022 AND INSTALLED BLIND INSERTS USING BMS5-28 TYPE 19 LOT#AK2AP8108K IAW SRM 53-00-50-2R-1 PARA 3M-N;[10] VERIFIED CORRECTIVE ACTION #9;[11] INSTALLED THROUGH INSERTS USING BMS5-107 LOT#AK1KP9159K IAW SRM 53-00-50-2R-1 PARA 3N;[12] CURED BLIND INSERTS USING HOTBONDER ID: IS000678 CAL DUE DATE 04/2023 AND THROUGH INSERTS WITH A HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2022 IAW SRM 53-00-50-2R-1 PARA 3N;[13] VERIFIED CORRECTIVE ACTION ITEMS 11 AND 12.;[14] ATTACHED CURE SHEETS

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,974 hrs · 35,001 cycles

FWD FLOOR PANEL 221DF UPPER SURFACE HAS AREAS OF PULLED STRANDS. / REMOVED AN APPROX. 19'X9' AREA OF DAMAGED TOOLSIDE PLY DAMAGE LOCATED 10' FROM THE OUTBOARD EDGE AND 14' FROM THE FORWARD EDGE WITH NO DISBOND; EXPOSED CORE CELLS OR CONTAMINATION NOTED; ALSO REMOVED 19 EA INSERTS FROM PANEL; WORK PERFORMED IAW SRM 53-00-50-2R-1 PARAGRAPH 3.A-F.;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1.;[03] VERIFIED CORRECTIVE ACTION #1; 2;[04] FABRICATED REPAIR PLIES FROM BMS9-3 TYPE H2 CLASS 7 STYLE 1581 LOT NUMBER 1493221-1 IAW SRM 53-00-50-2R-1 PARAGRAPH 3.K.(1).(A). OK TO INSTALL REPAIR PLIES.;[05] VERIFIED CORRECTIVE ACTION #4;[06] INSTALLED PLIES USING BMS8-201 LOT NUMBER 1494809-1; AND VACUUM BAGGED; VERIFIED SATISFACTORY 5X5 SUING VACUUM GAUGE ID: ATS2438 DUE: 03/2023; WORK PERFORMED IAW SRM 53-00-50-2R-1 PARAGRAPH 3.K.(1).(B-C) AND L.(1).(A-C).;[07] VERIFIED CORRECTIVE ACTION #6;[08] CURED PLIES UNDER HEAT LAMP USING THERMOMETER ID: ATS1174 DUE: 03/2023; WORK ACCOMPLISHED IAW SRM 53-00-50-2R-1 PARAGRAPH 3.M.;[09] UNBAGGED PANEL AND INSTALLED THROUGH INSERTS USING BMS5-107 LOT#AK1KP9159K AND INSTALLED BLIND INSERTS USING BMS5-28 TYPE 19 LOT#AK2AP8108K IAW SRM 53-00-50-2R-1 PARA 3M-N;[10] CURED BLIND INSERTS USING HOTBONDER ID: IS000678 CAL DUE DATE 04/2023 AND THROUGH INSERTS WITH A HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2022 IAW SRM 53-00-50-2R-1 PARA 3N;[

Part: FLOOR PANEL — PULLED (PAX CABIN) · airframe 58,974 hrs · 35,001 cycles

FWD FLOOR PANEL 221EF UPPER SURFACE OF FWD EDGE HAS AREA OF PULLED STRANDS. / REPAIRS TO BE ACCOMPLISHED IAW SRM 53-00-50-2R-1<BR><BR>REMOVED ALL INSERTS TO FACILITATE REPAIR IAW SRM 53-00-50-2R-1 PARA 3B<BR>REMOVED ALL DAMAGE NOTED AND CLEANED REPAIR AREAS IAW SRM 53-00-50-2R-1 PARA 3C-F OK TO POT EXPOSED CORE.;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1.;[03] VERIFIED CORRECTIVE ACTION 1 COMPLETED OK TO POT EXPOSED CORE;[04] POTTED EXPOSED CORE WITH BMS5-28 TYPE 19 LOT#1488901-1; CURED AND SANDED POTTING FLUSH THEN CLEANED REPAIR AREA IAW SRM 53-00-50-2R-1 PARA 3G-J<BR><BR>USED THERMOMETER ATS2208 CAL DUE DATE 10/2022;[05] FABRICATED REPAIR PLIES FROM BMS9-3 H2 LOT#1493221-1; OK TO INSTALL IAW SRM 53-00-50-2R-1 PARA 3K;[06] VERIFIED CORRECTIVE ACTIONS 4 AND 5<BR><BR>] INSTALLED REPAIR PLIES USING BMS8-201 TYPE 4 LOT#1482288-1; VACUUM BAGGED; CHECKED FOR LEAKS; LEAK CHECKED GOOD AND SET FOR CURE IAW SRM 53-00-50-2R-1 PARA 3K-USED VACUUM GAUGE ATS2545 CAL DUE DATE 08/2022 CURED REPAIR USING THERMOMETER ATS2208 CAL DUE DATE 10/2022 AND TRIMMED EXCESS MATERIAL IAW SRM 53-00-50-2R-1 PARA 3M;[ INSTALLED INSERTS USING BMS 5-107 LOT#AK1KP9159K IAW SRM 53-00-50-2R-1 PAR 3.N AND BOEING DWG 141A5810-249.<BR>USED THERMOMETER ID:ATS2545 CAL DUE 08/2022;

Part: FLOOR PANEL — DAMAGED (CABIN FLOOR) · airframe 58,974 hrs · 35,001 cycles

FWD FLOOR PANEL 222DF HAS A RIPPED OUT INSERT ALONG THE O/B EDGE. (MARKED) / [01] IDENTIFIED FWD PANEL 222DF IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW 53-00-50-1A-1 PARA 4.F. <BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>REMOVED 9EA INSERTS TO FACILITATE REPAIR; REMOVED DAMAGED SKIN; REMOVED DAMAGED CORE; AND CLEANED REPAIR AREA IAW SRM 53-00-50-2R-1 PARA 3.A-F.;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1.;[03] VERIFIED CORRECTIVE ACTION #1<BR><BR>VERIFIED MEASUREMENTS;[04] APPLIED BMS 5-28 LOT#1488901-1 AND SET TO CURE IAW SRM 53-00-50-2R-1 PARA 3.G.;[05] CURED POTTING USING THERMOMETER ID:ATS2209 DUE:10/2022; SANDED REPAIR AREA TILL SMOOTH; CLEANED REPAIR AREA; AND FABRICATED REPAIR PLIES USING BMS 9-3 LOT#1493221-1 IAW SRM 53-00-50-2R-1 PARA 3.H-K.<BR>OK TO INSTALL.;[06] VERIFIED CORRECTIVE ACTION #4; 5;[07] INSTALLED REPAIR PLIES USING BMS 8-201 TY3 LOT#AK2CP8139K; VACUUM BAGGED; LEAK CHECK GOOD USING VACUUM GAUGE ID:ATS2438 DUE:03/2023 DUE: IAW SRM 53-00-50-2R-1 PARA 3.K(1)&L(1).;[08] VERIFIED CORRECTIVE ACTION #7;[09] CURED REPAIR PLIES; UNBAGGED; TRIMMED EXCESS MATERIAL; AND INSTALLED/CURED INSERTS USING BMS 5-107 LOT:AK1KP9159K<BR>IAW SRM 53-00-50-2R-1 PARA 3.M(1)&N AND BDWG 141A5810-185<BR>THERMOMETER ID:ATS2209 DUE:10/2022;[10] VERIFIED CORRECTIVE ACTION #9;[11] ATTACHED CURE SHEET TO THIS FAULT RECORD.;[12] JOB COMPLETE

Part: PRESSURE DECK — CRACKED · airframe 58,974 hrs · 35,001 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS 664.5; LBL 30.5 AND 32; WL 202.5. (CRACKS CIRCLED IN RED) / CUTED AND REMOVED THE DAMAGE PART OF THE WEB PER SRM 53-40-51-2R-2. PAR. 4 A;B;C (1)(2)(3).HFEC INSPECTED CUTOUT AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.TRIMMED AND FLAP PEENED 2EA LOWER STIFFENERS PER SRM 53-40-51-2R-2 TABLE 202 FLAG NOTE 1 AND FIG 204 SHT 1;[10] VERIFIED CORRECTIVE ACTION #9;[11] LOCATED; DRILLED; AND TRIMMED TO SIZE ALL REPAIR PARTS COMPLETED INSTALLATION OF ALL REPAIR PARTS AT BBS663-675 AND LBLL25-60 IAW SRM 53-40-51-2R-2 REP.2 AND EA 22-153-02091. EXCEPT FASTENERS OF ATTACHMENT PONITS OF 4EA BRACKETS REMOVED FOR ACCESS.; INSTALLAED BRACKETS 4EA REMOVED FOR ACCESS IAW SRM 53-40-51-2R-2 REP.2 .;[29] OK TO SEALING AROUND REPAIR AREA AND FASTENERS;

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,974 hrs · 35,001 cycles

FWD FLOOR PANEL 221CF UPPER SURFACE HAS AREAS OF PULLED STRANDS. / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 6 TABLE 6.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>REMOVED ALL INSERTS TO FACILITATE REPAIR IAW SRM 53-00-50-2R-1 PARA 3.B<BR>REMOVED DAMAGED UPPER SURFACE SKIN AND LOOSE PIECES OF CORE; CLEANED REPAIR AREA IAW SRM 53-00-50-2R-1 PARA 3C-F.;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1.;[03] VERIFIED CORRECTIVE ACTION #1; 2;[04] APPLIED POTTING TO EXPOSED CORE USING BMS 5-28TY19 LOT#AK2AP8108K IAW SRM 53-00-50-2R-1 PARA 3.G.;[05] CURED POTTING COMPOUND; SANDED SMOOTH TO SURFACE AND FABRICATED REPAIR PLIES USING BMS 9-3H2 LOT#1493221-1 IAW SRM 53-00-50-2R-1 PARA 3H-K.<BR>OK TO INSTALL<BR>USED THERMOMETER ID:ATS2208 CAL DUE 10/2022;[06] VERIFIED CORRECTIVE ACTION #5;[07] INSTALLED REPAIR PLIES USING BMS 8-201TY4 LOT#1482288-1; VACUUM BAGGED; LEAK CHECK GOOD WITH VACUUM GAUGE ID:ATS2545 CAL DUE 08/2022 IAW SRM 53-00-50-2R-1 PARA 3K-L.;[08] VERIFIED CORRECTIVE ACTION #7<BR>VERIFIED MEASUREMENTS;[09] CURED REPAIR; UNBAGGED AND TRIMMED EXCESS MATERIAL; INSTALLED INSERTS USING BMS 5-107 LOT#AK1KP9159K IAW SRM 53-00-50-2R-1 PARA 3M;N AND BOEING DWG 141A5810-9.<BR>USED THERMOMETER ID:ATS2208 CAL DUE 10/2022;[10] VERIFIED CORRECTIVE ACTION #9;[11] JOB COMPLETE

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON FWD SHIELD AT FWD CARGO BAY BS426 RBL24. MARKED. / [01] UPDATED MEASUREMENTS;[02] EVALUATED CORROSION. REMOVED CORROSION IN A 1.0'X1.5. BLENDED AREA. PART HAS NO SRM LIMIT FOR DAMAGE. REPAIR BY REPLACEMENT. RECEIVED NEW PART AND DRILL AND LOCATED NEW PART IAW DWG 143A0080 ID 0019 REV:-; SRM 51-10-02; SRM 51-40-05; SRM 51-40-06.;[03] VERIFIED CORRECTIVE ACTION #2 AND MEASUREMENT FIELD.

Part: SUPPORT STRAP — CORRODED (MID CABIN) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON SUPPORT STRAP AT MID CABIN ABOVE MLG WELL BS703 LBL66. MARKED / [01] REMOVED CORROSION ON SUPPORT STRAP AT MID CABIN ABOVE MLG WELL BS703 LBL66 IN A 1'X1'X.004' AREA FROM .071' ORIGINAL IAW SRM 51-10-02-0G-0. SRM DOES NOT HAVE LIMITS FOR STIFFNER/ANGLES ON CREASE BEAM WEB.;[02] VERIFIED CORROSION REMOVAL AT REWORK AREA PER SRM 51-10-02-0G.;[03] HFEC INSPECTED BLENDED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR><BR>UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2.<BR>REMAINING MATERIAL THICKNESS IS 0.068' ADJACENT TO 0.071'.<BR><BR><BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23<BR>-EPOCH 650 ID: ATS2031 CAL DUE: 03/23;[04] REFER TO FAULT TTG8Q00DDX00 WHERE EA22-153-02114 WAS ADDED AS A SUBTASK;[05] VERIFIED CORRECTIVE ACTION 4. NO FURTHER ACTION REQUIRED.

Part: TIE DOWN — CORRODED (FUSELAGE) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON TRACK TIEDOWNS AT FWD CARGO BAY LBL18 BS400; BS435; BS433; BS495; BS496. / [01] VERIDFIED APPLICABILITY IAW SRM 53-00-53-1A-2;[02] REMOVED CORROSION AT: BS 400 MAT. REMOVED 0.015; AREA FOUND WHIT IN LIMITS; BS 435 MAT. REMOVED 0.016; AREA FOUND WHIT IN LIMITS; BS 436 MAT. REMOVED 0.020; AREA FOUN WHIT IN LIMITS; BS 495 MAT. REMOVED 0.012 AREA FOUND WHIT IN LIMITS; BS 496 MAT. REMOVED 0.050 AREA FOUND OUT OF LIMITS IAW SRM 53-00-5301A-2;[03] USED TOOL DEPTH GAGE ID ATS1738 S/N UNKNOWN D.D. 09/2022;[04] MAT. REMOVED AT BS 496 0.029 AREA FOUND WHIT IN LIMITS IAW SRM 53-00-53-1A-2 USED DEPTH GAGE ID ATS1738 S/N UNKNOWN D.D. 09/2022;[05] UPDATED MEASUREMENTS;[06] REQ. OK TO TREAT AND PRIME REWORK AREAS;[07] VERIFIED CORRECTIVE ACTION ITEMS 1-4; AND THE CORRECTION TO BS 496 DEPTH IS 0.029; NOT OUT OF LIMITS. MEASUREMENT FIELDS HAS SEVERAL INCORRECT ITEMS; AND THIS NOT A LEVEL 3 TYPE CORROSION.;[08] UPDATED MEASUREMENTS;[09] REQ. OK TO APPLY TREAT AND PRIME;[10] VERIFIED CORRECTIVE ACTION #9<BR> OK TO APPLY TREAT AND PRIME GIVEN;[11] APPLIED CHEMICALL CONVERSION AND PRIME AT REWORK AREAS IAW SOPM 20--43-03 AND SRM 51-20-01-0G-0;[12] VERIFIED CORRECTIVE ACTION #11;[13] EDIT MEASUREMENTS;[14] VERIFIED MEASUREMENT TABLE<BR>TASK COMPLETE

Part: SIDEWALL SUPPORT — CORRODED (FWD CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY RBL 23 BS400 - BS420. MARKED. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2.;[02] REMOVED CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 23 BS 400 DIMENSIONS L=1' W= 0.750 DEPTH:0.010' IAW SRM 51-10-02 PARAGRAPH 15 ; EVALUATED REWORKED AREA ;ORIGINAL MATERIAL THICKNESS 0.040' REMAINING THICKNESS : 0.030' AND FOUND TO BE OUT LIMITS; ALLOWABLE DAMAGE IAW SRM 53-00-53-1A-2;TOOL USED MICROMETER ID ATS400 S/N UNKNOWN DUE 08/2022.;[03] :FABRICATED ; LOCATED AND DRILLED FCB RBL 23 BS 400 TO BS 420 FLOOR TO SIDEWALL SUPPORT USING BAC1496-444#7075T62 LOT:1490548-1 IAW SRM 51-40-05-0G-0;; AND DWG 143A7501 REV:-. APPLY CHEMICAL CONVERSION COATING AND PRIMER.;[04] UPDATED MEASUREMENTS;[05] VERIFIED CORRECTIVE ACTIONS 3 AND 4.;[06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON FCB FLOOR TO SIDEWALL SUPPORT AT RBL 23 WL 156; BS 400 TO BS 420 IAW SRM 51-20-01 AND AMM 51-21-72-370-804;[07] VERIFIED CORRECTIVE ACTION #6;[08] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLE.

Part: SUPPORT STRAP — CORRODED (MID CABIN) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON SUPPORT STRAP AT MID CABIN ABOVE MLG WELL BS707 RBL63. MARKED / [01] REMOVED 4 FASTENERS ON STRAP IAW SRM 51-40-02-0G-0;[02] REMOVED CORROSION IN 4 AREAS IN A 1'X1' AREA IAW SRM 51-10-02-0G-0. SRM DOES NOT HAVE ALLOWABLE DAMAGE LIMITS FOR STIFFNER ANGLES. ORIGINAL THICKNESS IS .071'.;[03] NDI VERIFY REMAINING THICKNESS.;[04] VERIFIED CORRECTIVE ACTION #2;[05] HFEC INSPECTED BLENDED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR><BR>HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16.<BR>NO CRACKS NOTED.<BR><BR>UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2.<BR>REMAINING MATERIAL THICKNESS IS 0.068' ADJACENT TO 0.071'.<BR><BR><BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23<BR>-MINIMITE ID: IS000934 CAL DUE: 08/22<BR>-EPOCH 650 ID: ATS2031 CAL DUE: 03/23;[06] REFER TO FAULT TTG8Q00DDX00 WHERE EA22-153-02114 WAS ADDED AS A SUBTASK;[07] VERIFIED CORRECTIVE ACTION 6. NO FURTHER ACTION REQUIRED.

Part: SIDEWALL SUPPORT — CORRODED (FWD CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY RBL24 BS500A+10; BS500B+19 - BS500C+15. MARKED. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2.;[02] COMPLETED STEP 1;2;3;[03] :FABRICATED ; LOCATED AND DRILLED FCB RBL 24 BS 500ATO BS 500D NEW FLOOR TO SIDEWALL SUPPORT USING BAC1496-444#7075T62 LOT:1490548-1 IAW SRM 51-40-05-0G-0;; AND DWG 143A7501 REV:-. APPLY CHEMICAL CONVERSION COATING AND PRIMER.;[04] UPDATED MEASUREMENTS;[05] VERIFIED CORRECTIVE ACTION ITEM 1-4; OK TO PROCEED.;[06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON FCB FLOOR TO SIDEWALL SUPPORT AT RBL WL 156; BS 500A TO BS 500D IAW SRM 51-20-01 AND AMM 51-21-72-370-804;[07] CORRECTION :<BR>APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON FCB FLOOR TO SIDEWALL SUPPORT AT RBL 24 WL 156; BS 500A TO BS 500D IAW SRM 51-20-01 AND AMM 51-21-72-370-;[08] VERIFIED CORRECTIVE ACTION #7;[09] ALL STEPS COMPLETE.

Part: SUPPORT STRAP — CORRODED (MID CABIN) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON SUPPORT STRAP AT MID CABIN ABOVE MLG WELL BS707 LBL63. MARKED / [01] REMOVED CORROSION ON STRAP IN A 1'X1' AREA IAW SRM 51-10-02-0G-0. SRM DOES NOT HAVE LIMITS FOR STIFFNER/ANGLES ON CREASE BEAM WEB. ORIGINAL THICKNESS IS .071';[02] NDI VERIFY REMAINING THICKNESS.;[03] VERIFIED CORROSION REMOVAL AT REWORK AREA PER SRM 51-10-02-0G-0.;[04] HFEC INSPECTED BLENDED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR><BR>HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16.<BR>NO CRACKS NOTED.<BR><BR>UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2.<BR>REMAINING MATERIAL THICKNESS IS 0.069' ADJACENT TO 0.071'.<BR><BR><BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23<BR>-MINIMITE ID: IS000934 CAL DUE: 08/22<BR>-EPOCH 650 ID: ATS2031 CAL DUE: 03/23;[05] REFER TO FAULT TTG8Q00DDX00 WHERE EA22-153-02114 WAS ADDED AS A SUBTASK;[06] VERIFIED CORRECTIVE ACTION 5. NO FURTHER ACTION REQUIRED.

Part: TIE DOWN — CORRODED (FWD CARGO) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON TRACK TIEDOWNS AT FWD CARGO BAY RBL13 BS400; BS500C+2; BS500C+16. / [01] VERIFIED APPLICABILITY IAW SRM 53-00-53-1A-2;[02] REMOVED CORROSION AT: BS 400; MAT. REMOVED 0.020 AREA FOUN WHIT IN LIMITS; BS500-C + 2 MAT. REMOVED 0.002 AREA FOUND WHIT IN LIMITS; BS 500-C + 16 MAT. REMOVED 0.055 AREA FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2;[03] USED TOLL; DEPTH GAGE ID ATS1738; S/N UNKNOWN; D.D. 09/2022;[04] UPDATED MEASUREMENTS;[05] VERIFIED CORRECTIVE ACTION ITEM 1-4; MEASUREMENT FIELDS HAS SEVERAL INCORRECT ITEMS.;[06] CUT OUT DAMAGED PART OF THE CARGO TRACK AT RBL13 BETWEEN BS 550B AND BS 500C IAW SRM53-0053-2R-3 FIG 203;[07] VERIFIED CORRECTIVE ACTION #6;[08] REMOVED TRACK FORM BS 400 TO BS 500 D RBL 13 IAW SRM 51-40-02-0G-0;[09] LOCATED AND DRILLED NEW CARGO TRACK ASSY FROM ITEM 143A7501-10 PO. NUMBER:857275/1 IAW SRM 51-40-05; SRM 51-40-05;SRM 51-40-08 AND BOEING DWG 143A7500 0O TO INSTALL NEW TRACK;[10] VERIFIED CORRECTIVE ACTION #9;[11] EDIT MEASUREMENTS;[12] VERIFIED CORRECTIVE ACTION STEP 9. VERIFIED OK TO INSTALL.;[13] LOCATED AND DRILLED NEW CARGO TRACK ASSY FROM ITEM 143A7501-10 PO. NUMBER:857275/1 IAW SRM 51-40-02; SRM 51-40-05;SRM 51-40-08 AND BOEING DWG 143A7500 REV:- TO INSTALL NEW TRACK;[14] EDIT STEP #9;[15] INSTALLED NEW CARGO TRACK ASSY AT FCB BS400 TO BS500D RBL 13' WL 156' FROM ITEM 143A7501-10 PO. NUMBER:857275/1 IAW SRM 51-40-02 AND BOEING DWG 143A7500 REV:-

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY LBL24 BS446;BS450; BS454; BS494 - 500+10; BS500A - BS500A+13; BS500B+2; BS500C - BS500D. MARKED. / [01] SRM 53-00-53-1A-2 IS FOUND TO BE APPLICABLE;[02] EVALUATED CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT LBL 24 <BR>BS 446 L=1.8'XW=.8'XD=.002'<BR>BS 450 L=1.5'XW=.9'XD=.005'<BR>BS 454 L=.9'XW=.8'XD=.002'<BR>BS 496 L=1.8'XW=.8'XD=.0025'<BR>BS 504 L=1'XW=.6'XD=.006'<BR>BS 500A L=1.2'XW=.8'XD=.003'<BR>BS 500A+13 L=.8'XW=.7'XD=.003'<BR>BS 500B+2 L=1.2'XW=.8'XD=.002'<BR>BS 500C+10 L=1.4'XW=1'XD=.005'<BR>BS 500C+18 L=2.3'XW=1.2'XD=.005'<BR>CORROSION IS FOUND TO BE OUT OF LIMITS WITH REMAINING THICKNESS OF .034' OF ORIGINAL THICKNESS .040' IAW SRM 53-00-53-0I-2 AND SRM 53-00-53-1A-2<BR>DIAL DEPTH GAUGE USED; ID: ATS2677 S/N:UNKNOWN DUE:11/2022;[03] VERIFIED CORRECTIVE ACTIONS #1 AND #2<BR>VERIFIED MEASUREMENT TABLE;[04] LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT FCB LBL24 BS396-500D FROM BAC1496-444#7075T62 LOT#1490548-1 IAW BOEING DWG 143A7500; BOEING DWG 143A7501 AND SRM 51-40-05;[05] LOCATED AND DRILLED NEW REPAIR SPLICE FOR FCB FLOOR TO SIDEWALL SUPPORT LBL24 BS480-500 IAW SRM 53-00-53-2R-6 AND SRM 51-40-05;[12] INSTALLED SPLICE REPAIR AT SIDEWALL SUPPORT LBL 24 ; WL 156 ;BTW 480 TO 500 FCB L/H IAW SRM 53-40-02 AND SRM 53-00-53-2R-6; TASK COMPLETED.;[13] VERIFIED CORRECTIVE ACTION #12

Part: FAIRING — CRACKED (L/H WING) · airframe 58,974 hrs · 35,001 cycles

L/W FLAP TRACK FAIRING 543BB HAS CRACK ON FWD EDGE / [01] IDENTIFIED L/W FLAP TRACK FAIRING 543BB IAW SRM 57-53-70-0I-2 FIGURE 4; SHEET 1; TABLE 3; ITEM 1. <BR><BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-53-70-1A-1 PAR 4B(2).<BR><BR>REPAIR TO BE ACCOMPLISHED IAW SRM 57-53-70-2R-5.[07] APPLIED AND CURED SEALER RESIN BMS 8-207 (1838) LOT # 1139Q1194A TO BLENDED AREA IAW SRM 57-53-70-2R-5 PARA 4.E(1); SRM 51-70-08-0G-0 PARA 3 C-E; SRM 51-30-10-0G-0 TABLE 1; RESIN MIX 5<BR><BR>FLUKE 62 IR THERMOMETER ID ATS2209 SN 43300739WS DATE 10/2022<BR><BR>APPLIED AND CURED CONDUCTIVE COATING; RESISTANCE CHECK 'GOOD' IAW SRM 57-53-70-2R-5 PARA 4.E(2); AMM 51-21-71-370-801 PARA 3.D(2-4) AND 3.D(7)(A)<BR><BR>FLUKE 62 IR THERMOMETER ID ATS2208 SN 43300740WS DATE 10/2022<BR>FLUKE 77 MULTIMETER ID ATS1658 SN 34000350 DATE 03/2023<BR><BR>REFINISHED IAW SRM 57-53-70-2R-5 PARA 4.E(3-4) AND AMM 51-21-99-300-802 PARA 3.C(1)(A-E)<BR><BR>REPAIRED CRACK ON FWD EDGE OF L/W FLAP TRACK FAIRING 543BB IAW SRM 57-53-70-2R-5;[08] VERIFIED CORRECTIVE ACTION 7

Part: SUPPORT STRAP — CORRODED (MID CABIN) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON SUPPORT STRAP AT MID CABIN ABOVE MLG WELL BS686 LBL68. MARKED / [01] REMOVED 2 FASTENERS IAW SRM 51-40-02-0G-0;[02] REMOVED CORROSION ON SUPPORT STRAP IN A 1'X1.5' AREA IAW SRM 51-10-02-0G-0. SRM DOES NOT HAVE LIMITS FOR SUPPORT STIFFNER/ANGLES ON CREASE BEAM WEB. ORIGINAL THICKNESS IS .071';[03] VERIFIED CORROSION REMOVAL AT REWORK AREA PER SRM 51-10-02-0G.;[04] HFEC INSPECTED BLENDED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR><BR>HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16. <BR>NO CRACKS NOTED.<BR><BR>UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2.<BR>REMAINING MATERIAL THICKNESS IS 0.068' ADJACENT TO 0.071'.<BR><BR><BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23<BR>-MINIMITE ID: IS000934 CAL DUE: 08/22<BR>-EPOCH 650 ID: ATS2031 CAL DUE: 03/23;[05] UPDATED CHART;[06] COMPLETED STEP 1.;[07] COMPLETED STEP 1;[08] VERIFIED MEASUREMENTS;[09] COMPLETE;[10] COMPLETED STEP 2;[11] COMPLETE;[12] CERTIFY;[13] VERIFIED STEP 2 COMPLETE. WORKSCOPE COMPLETED PER EA 22-153-02114

Part: TRACK — CORRODED (AFT CARGO) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY TRACK AT RBL 14 BS 787+13; BS 787+15; BS 787+17; BS 807+12; BS 827+4; BS 827+17. / [01] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS;[02] BLENDED DAMGE ON AFT CARGO BAY TRACK AT RBL 14 ; BS 787+13 ; L 0.500' X W 0.400 X D 0.009'; BS 787+15 ; L 1.0' X W 0.200' X D O.012'; BS 787+17 ; L 1.0' X W 0.500' X D 0.012' ; BS 807+12; L 1.4' X W 0.150' X D 0.013';BS 827+4 ; L 1.3' X W 0.200' X D 0.014' ; 827+17; L 1.4' X W 0.300' X D 0.012' ; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; STEP 4B; FIGURE103 ; USED DEPTH GAUGE ; ID:ATS401; S/N: UNKNOWN; DUE: 10/2022;[07] LOCATED AND DRILLED NEW CARGO BAY SECTION TRACK BETWEEN BS 747+8 TO BS 887; RBL 14 IAW SRM 51-40-05-0G-0 AND DWG 146A7500; ID:0027; REV:A . OK TO INSTALL;10] INSTALLED NEW CARGO BAY TRACK SECTION FROM BS 767 TO BS 887; RBL 14 IAW SRM 51-40-02-0G-0 AND DWG 146A7500; ID:0027 ; REV:A[13] LOCATED AND DRILLED CARGO TRACK SPLICE BETWEEN BS 747 AND BS 767; RBL 14 IAW SRM 53-00-53-2R-3 ; OK TO INSTALL SPLICE;[16] INSTALLED SPLICE BETWEEN BS 747 AND BS 767 ; RBL 14 IAW SRM 53-00-53-2R-3

Part: STIFFENER — CRACKED (R/H HORIZ. STAB.) · airframe 58,974 hrs · 35,001 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 3RD VERTICAL STIFFENER IS CRACKED. / [01] VALIDATED APPLICABILITY OF SRM 55-10-09-2R-4&5.11] FABRICATED REPAIR T-SECTION FROM 60-5872 7075T6511 .063' CLAD LOT#476286-1. REPAIR ANGLE FROM BAC 1490-2793 7075T62 .063' LOT#1464923-1. REPAIR FILLER FROM 7075T6 .050' CLAD LOT#5087747-1 AND REPAIR SHIMS FROM 7075T6 .016' CLAD LOT#1351319-2. APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO REAIR PARTS AND BARE AREAS OF RIB REPAIR AREA. WORK ACCOMPLISHED IAW SRM 55-10-09-2R-5 PARA. 4. AND FIG. 203. OK TO INSTALL.;

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727A+15; BS 727B+14; BS 727C+2; BS 727C+5; BS 727C+10; BS 727D+5; BS 727D+16; BS 727E+10. / [01] VERIFIED SRM 53-00-53-1A-2 ALLOWABLE DAMAGE IS APPLICABLE. <BR>REMOVED CORROSION FROM ACB L/H FLOOR TO SIDEWALL SUPPORT WITH ORIGINAL THICKNESS 0.040'.<BR>BS 727A+15 L= 0.900' W= 1' D= 0.008' FOUND OUT OF LIMITS <BR>BS 727B+14 L= 0.800' W= 0.900' D= 0.006' FUND OUT OF LIMITS <BR>BS 727C+2 L= 1.200' W= 1' D= 0.005' FOUND OUT OF LIMITS <BR>BS 727C+5 L= 2' W= 1' D= 0.003' FOUND IN LIMITS <BR>BS 727C+10 L= 1.400' W= 1' D= 0.008' FOUND OUT OF LIMITS<BR>BS 727D+5 L= 0.900' W= 1' D= 0.009' FOUND OUT OF LIMITS<BR>BS 727D+16 L= 1' W= 1' D= 0.001 FOUND IN LIMITS<BR>BS 727E+10 L= 2' W= 1' D= 0.004 FOUND IN LIMITS <BR>TOOL= ID: ATS2472 S/N: UNKNOWN DATE: 12/2021 DUE: 12/2022<BR>IAW SRM 51-10-02 AND SRM 53-00-53-1A-2;;[06] FABRICATION OF REPLACEMENT FLOOR TO SIDEWALL SUPPORT BS727-847 LBL 21 IS ACCOMPLISHED ON CUSTOMER CARD TTG8Q00DDBZX;[07] EDIT MEASUREMENTS;[08] VERIFIED CORRECTIVE ACTION #6; VERIFIED MEASUREMENTS;[09] UPDATED MEASUREMENTS

Part: BRACKET — CRACKED (AFT CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CRACK ON AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+11.5 RBL 11. / [01] UPDATED MEASUREMENT<BR><BR>REMOVED ACB WATER SERVICE BRACKET AT BS 907+11.5 RBL 11 IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-05-0G-0 AND DWG 147A7221 ID:0017 REV:D;[03] RECEIVED NEW BRACKET<BR>ITEM# : 147A7221Y32<BR>PO# : 874787/1;[04] VERIFIED CORRECTIVE ACTIONS 2 AND 3.;[05] REQUEST; OK TO INSTALL;[06] REQUEST; OK TO INSTALL;[07] OK TO INSTALL GIVEN; VERIFIED MEASUREMENTS.;[08] INSTALLED FASTENERS IAW SRM 51-40-02 AND DWG 147A7221 ID:0017 REV:D. REQUEST OK TO APPLIED CAP SEAL.;[09] INSTALLED FASTENERS IAW SRM 51-40-02 AND DWG 147A7221 ID:0017 REV:D. REQUEST OK TO APPLIED CAP SEAL;[10] VERIFIED INSTALLATION OF FASTENERS;[11] JOB COMPLETED AS NO CAP SEAL NEEDED PER DWG 147A7221;[12] VERIFIED ALL STEPS COMPLETE.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727E+14; BS 727E+18; BS 747+2; BS 747+6; BS 747+14; BS 767+10; BS 767+14. / [01] VERIFIED SRM 53-00-53-1A-2 ALLOWABLE DAMAGE IS APPLICABLE. <BR>REMOVED CORROSION FROM ACB L/H FLOOR TO SIDEWALL SUPPORT WITH ORIGINAL THICKNESS 0.040'.<BR>BS727E+14 L= 0.900' W= 1' D= 0.009' FOUND OUT OF LIMITS <BR>BS727E+18 L= 1.200' W= 1' D= 0.007' FOUND OUT OF LIMITS <BR>BS747+2 L= 2' W= 1' D= 0.004' FOUND IN LIMITS<BR>BS747+6 L= 2' W= 1' D= 0.002' FOUND IN LIMITS <BR>BS747+14 L= 1.100' W= 1' D= 0.005' FOUND OUT OF LIMITS <BR>BS767+10 L= 0.900' W= 1' D= 0.008' FOUND OUT OF LIMITS <BR>BS767+14 L= 1.300' W= 0.900' D= 0.006' FOUND OUT OF LIMITS <BR>TOOL= ID: ATS2472 S/N: UNKNOWN DATE: 12/2021 DUE: 12/2022<BR>IAW SRM 51-10-02 AND SRM 53-00-53-1A-2;[04] :FABRICATED ; LOCATED AND DRILLED REPLACEMENT ACB FLOOR TO SIDEWALL SUPPORT USING BAC1496-377#7075T62 LOT:1473823-1 IAW SRM 51-40-05-0G-0;; SRM 53-00-53-2R-6 AND DWG 1467502 REV:-. FABRICATED FLOOR TO SIDEWALL SUPPORT SPLICE REPAIR AT B/S BTW 727E TO 747 LBL 21 USING BAC1496-377#7075T62 LOT:1473823-1 IAW SRM 53-00-53-2R-6 AND SRM 51-40-05. [10] INSTALLED SPLICE REPAIR AT SIDEWALL SUPPORT LBL 21; WL 156 ;BTW 727E TO 747 ACB IAW SRM 51-40-02 SRM 53-00-53-2R-6;

Part: TRACK — CORRODED (AFT CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY TRACK AT RBL 13 BS 927+7. / [01] REMOVED CORROSION ON ACB ON TRACK BS 927+7' RBL 13 IN L=1' X W=1' X D=0.012' FROM ORIGINAL TICKNESS OF 0.070' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR 4.B FIG 103. <BR><BR>USED TOOL :<BR>ID:ATS601<BR>S/N:87172291<BR>DATE:06/2022<BR>DUE:06/2023;[02] VERIFIED CORRECTIVE ACTION 1 COMPLETED;[03] CORROSION ON TRACK ITS OUT OF LIMITS WILL BE REPAIRED BY REPLACEMENT OF PART IAW SRM 51-10-02 PAR 9.<BR><BR>REMOVED TRACK AT ACB BTW BS 887 TO BS 947 RBL 13 IAW SRM 51-40-02;[04] REMOVED AFT BAY TIE DOWN TRACK BS 887-947 RBL 13 IAW SRM 51-40-02 0G-0;[05] LOCATED AND DRILLED NEW AFT CARGO BAY TRACK AT RBL 13 ; BETWEEN BS 887 TO BS 947.5 IAW SRM 51-40-05-0G-0 AND DWG 147A7500; ID:0005 ; REV:C; OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION 4; OK TO INSTALL GIVEN.;[07] INSTALLED NEW AFT CARGO BAY TRACK AT RBL 13 ; BETWEEN BS 887 TO BS 947.5 IAW SRM 51-40-05-0G-0 AND DWG 147A7500; ID:0005 ; REV:C;[08] EDIT MEASUREMENTS;[09] VERIFIED CORRETIVE ACTION 7.;[10] VERIFIED MEASUREMENT TABLE.

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY AFT R/H LOWER BULKHEAD SUPPORT AT BS 947 RBL 22. / [01] EVALUATED DAMAGE: NO SRM LIMITS FOR THIS PART REPAIR BY REPLACEMENT IAW SRM 51-10-02 PARA # 9.;[02] REMOVED ON AFT CARGO BAY AFT R/H LOWER BULKHEAD SUPPORT AT BS 947 RBL 22 IAW SRM 51-40-02;[03] LOCATED AND DRILLED ON AFT CARGO BAY AFT R/H LOWER BULKHEAD SUPPORT AT BS 947 RBL 22.ITEM :149A8118-27 LOT#1497077-1 PO#875205/1 IAW SRM 51-40-02 AND DWG 149A8118 REV:B.;[04] MADE COUNTERSINK IAW SRM 51-40-08/0G1. REQUEST OK TO INSTALL;[05] COUNTERSUNK R/H BS 947 BULKHEAD SUPPORT IAW SRM 51-40-08/0G1. REQUEST OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTIONS STEP 3;4. OK TO INSTALL GIVEN.;[07] BEGAN INSTALLING R/H LOWER BULKHEAD SUPPORT AT BS 947 IAW SRM 51-40-02; DWG 149A8110 ID:0008 REV: A AND 149A8117 ID: 0006 REV: -;[08] INSTALLED R/H LOWER BULKHEAD SUPPORT AT BS 947 IAW SRM 51-40-02; DWG 149A8110 ID:0008 REV: A AND 149A8117 ID: 0006 REV: -;[09] VERIFIED FASTENER INSTALLATION;[10] VERIFIED CORRECTIVE ACTION 7; 8 AND MEASUREMENT TABLE

Part: FRAME — CRACKED (AFT CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY FRAME AT BS 947 LBL 8; RBL 8; RBL 11. / FRAME IS CRACKED.;[04] UPON FURTHER EVALUATION AFT CARGO BAY- LWR LOBE FRAME SECTION STA 947 RBL 29 - LBL 29 FOUND TO BE OUT OF LIMITS. NO CRACKS ARE PERMITED PER SRM 53-00-07-1A-1 ALLOWABLE DAMAGE 1. FRAME SECTION STA 947 RBL 29 - LBL 29 TO BE REPAIR BY REPLACEMENT OF PART PER SRM 51-10-02-0G-0 PARA 9.COMPLETED- INSTALLATION OF FRAME HAS BEEN COMPLETED AND DOCUMENTED ON STEP 19;[23] COMPLETED STEPS 1; 11 AND 12.;[24] VERIFIED STEPS 1; 11 AND 12.;[25] COMPLETED STEP 3.;[26] VERIFIED STEP 3.;[27] PARTIAL UPDATE ON STEPS 4; 5 AND 7.;[28] VERIFIED STEPS 4; 5 AND 7;[29] COMPLETED STEPS 8-10 AND 16.;[30] VERIFIED STEPS 8;9;10 AND 16.;[31] VERIFIED ALL STEPS ON TASK CARD HAVE BEEN COMPLETED<BR>FRAME REPLACEMENT COMPLETED STA 947 BETWEEN STRINGER 23L- 23R; LBL28-RBL28.;[32] VERIFIED CORRECTIVE ACTION 31 AND MEASUREMENT TABLE.

Part: BRACKET — CRACKED (AFT CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CRACK ON AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+7.5 RBL 12. / [01] UPDATED MEASUREMENT<BR><BR>RECEIVED NEW BRACKET<BR>ITEM# : 147A7221Y32<BR>PO# : 874805/1;[02] REMOVED ACB WATER SERVICE BRACKET AT BS907+7.5 RBL12 IAW SRM 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-05-0G-0 AND DWG 147A7221 ID:0017 REV:D;[04] VERIFIED CORRECTIVE ACTIONS 2 AND 3.;[05] REQUEST; OK TO INSTALL;[06] REQUEST; OK TO INSTALL;[07] OK TO INSTALL GIVEN. VERIFIED MEASUREMENTS.;[08] INSTALLED FASTENERS IAW SRM 51-40-02 AND DWG 147A7221 ID:0017 REV:D. REQUEST OK TO APPLIED CAP SEAL.;[09] INSTALLED FASTENERS IAW SRM 51-40-02 AND DWG 147A7221 ID:0017 REV:D. REQUEST OK TO APPLIED CAP SEAL;[10] VERIFIED INSTSALLATION OF FASTENERS;[11] JOB COMPLETED AS NO CAP SEAL NEEDED PER DWG 147A7221;[12] VERIFIED COMPLETION OF TASK.

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 867+3; BS 867+6; BS 867+16. / [01] SRM 53-00-53-1A-2 FOUND TO BE APPLICABLE FOR THIS EVALUATION. REMOVED DAMAGE FROM THE FOLLOWING LOCATION: BS867+3 1.3LX1.0W D:0.006; BS867+6 1.3LX1.1W D:0.006; BS867+16 1.7LX1.0 D:0.004 ORIGINAL THICKNESS IS 0.040 PART FOUND TO BE OUT OF LIMITS. IAW SRM 51-10-02; SRM 53-00-53-1A-2. BAC1496-377 CAL TOOL INFO. ID:ATS2595 S/N F03295; EXP; 02/2023;[02] VERIFIED CORRECTIVE ACTION #1;[03] FABRICATED ; LOCATED AND DRILLED NEW AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BETWEEN BS 867 T0 BS 947.5 ; FROM BAC1496-377 7075-T62 ; LOT# 1494598-1 ; IAW SRM 51-40-05-0G-0 AND DWG 146A7501; ID:0006;REV:A; APPLIED CHEMICAL CONVERSION AMM 51-21-41-370-802; OK TO APPLY PRIMER;[04] VERIFIED CORRECTIVE ACTION #3;[05] APPLIED PRIMER ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 FROM BS 867 TO BS 947.5 IAW AMM 51-21-72-370-804;[06] VERIFIED CORRECTIVE ACTION #5<BR>VERIFIED MEASUREMENT TABLE

Part: THRESHOLD — CORRODED (AFT CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY THRESHOLD AT RBL 26 BS 787+13; RBL 26 BS 807+2; RBL 26 BS 807+4; RBL 26 BS 807+6; RBL 26 BS 807+17; RBL 26 BS 807+19; RBL 26 BS 827+4; RBL 24 BS 827+16; RBL 20 BS 827+19. / [01] REMOVED CORROSION AT<BR>BS 787+13 0.004'<BR>BS 807+2 0.005'<BR>BS 807+4 0.004'<BR>BS 807+6 0.002'<BR>BS 807+17 0.002'<BR>BS 807+19 0.004'<BR>BS 827+4 0.006' (THE DEEPEST DAMAGE)<BR>BS 827+16 0.006' (THE DEEPEST DAMAGE)<BR>BS 827+19 0.004'<BR><BR>IAW SRM 51-10-02-0G-0;[02] VERIFIED APPLICABILITY IAW SRM 53-60-15-01-1 AND SRM 53-60-15-1A-1;[03] ORIGINAL MATERIAL THICKNESS : 0.050' THE DEEPEST DAMAGE REMOVED : 0.006' REMAINING THICKNESS : 0.044' AT BS 827+4 AND BS 827+16.<BR>DAMAGE EXCEED 10% OF ORIGINAL MATERIAL THICKNESS. FOUND TO BE OUT OF LIMIT IAW SRM 53-60-15-1A-1<BR><BR>CALIBRATION TOOL DEPTH GAUGE<BR>ID : ATS401<BR>S/N : UNKNOWN<BR>DUE : 10/2022;[04] VERIFIED CORRECTIVE ACTIONS 1-3;[05] RECEIVED NEW THRESHOLD AT ACB ITEM: 146A8123U25 LOT: 1496302-2. LOCATED AND DRILLED NEW THRESHOLD IAW SRM 51-40-05 AND DWG 146A8123 ID: 0006 REV: C;[06] VERIFIED CORRECTIVE ACTION #5;[07] LOCATED; DRILLED; AND COUNTERSANK NEW THRESHOLD IAW SRM 51-40-05; SRM 51-40-08 AND DWG 146A8123 ID: 0006 REV: C;[08] UPDATED MEASUREMENTS PARAMETERS;[09] FILLED OUT PARTS REQ;[10] VERIFIED CORRECTIVE ACTION #7-9; VERIFIED MEASUREMENT FIELD.

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 747+2; BS 747+5; BS 747+9; BS 747+14. / [01] REMOVED DAMAGE FROM THE FOLLOWING LOCATION: BS747+2 1.0L X 0.7W D:0.03; BS747+5 0.8L X 0.6W D: 0.04; BS747+9 0.8L X 0.6W D: 0.06; BS747+14 1.0L X 0.7W D: 0.06;IAW SRM 51-10-02; SRM 53-00-53-1A-2. PART FOUND TO BE OUT OF LIMIT.;[02] CAL TOOL INFO. ID:ATS2595 S/N F03295; EXP; 02/2023;[03] SRM 53-00-53-1A-2 IS FOUND TO BE APPLICABLE FOR THIS EVALUATION;[04] ORIGINAL THICKNESS IS 0.40 IAW BAC1496-377;[05] CORRECTION TO LINE 1.REMOVED DAMAGE FROM THE FOLLOWING LOCATION: BS747+2 1.0L X 0.7W D:0.003; BS747+5 0.8L X 0.6W D: 0.004; BS747+9 0.8L X 0.6W D: 0.006; BS747+14 1.0L X 0.7W D: 0.006;IAW SRM 51-10-02; SRM 53-00-53-1A-2. PART FOUND TO BE OUT OF LIMIT.;[06] CORRECTION TO LINE 4 ORIGINAL THICKNESS IS 0.040 IAW BAC1496-377;[07] VERIFIED CORRECTIVE ACTION 1-6;[08] JOB WILL BE ACCOMPLISH ON CUSTMER CARD NBR: TTG8Q00DDCS3;[09] UPDATED MEASUREMENTS;[10] UPDATED MEASUREMENTS;[11] VERIFIED CORRECTIVE ACTION #8 AND MEASUREMENT FIELD

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 787+6; BS 787+8; BS 787+10; BS 787+12; BS 787+15; BS 807+14. / [01] VERIFIED SRM 53-00-53-1A-2 ALLOWABLE DAMAGE IS APPLICABLE.<BR>REMOVED CORROSION FROM ACB L/H FLOOR TO SIDEWALL SUPPORT WITH ORIGINAL THICKNESS 0.040'.<BR>BS787+6 L= 1' W= 0.900' D= 0.007' FOUND OUT OF LIMITS<BR>BS787+8 L= 1.200' W= 1' D= 0.001' FOUND IN LIMITS<BR>BS787+10 L= 1' W= 1' D= 0.005' FOUND OUT LIMITS <BR>BS787+12 L= 1.100' W= 0.900' D= 0.004' FOUND IN LIMITS<BR>BS787+15 L= 1' W= 1' D= 0.003' FOUND IN LIMITS<BR>BS807+14 L= 1.500' W= 1' D= 0.020' FOUND OUT OF LIMITS <BR>TOOL= ID: ATS2472 S/N: UNKNOWN DATE: 12/2021 DUE: 12/2022<BR>IAW SRM 51-10-02 AND SRM 53-00-53-1A-2;[02] VERIFIED SRM 53-00-53-1A-2 ALLOWABLE DAMAGE IS APPLICABLE.REMOVED CORROSION FROM ACB L/H FLOOR TO SIDEWALL SUPPORT WITH ORIGINAL THICKNESS 0.040'.BS787+6 L= 1' W= 0.900' D= 0.007' FOUND OUT OF LIMITSBS787+8 L= 1.200' W= 1' D= 0.001' FOUND IN LIMITSBS787+10 L= 1' W= 1' D= 0.005' FOUND OUT LIMITSBS787+12 L= 1.100' W= 0.900' D= 0.004' FOUND IN LIMITSBS787+15 L= 1' W= 1' D= 0.003' FOUND IN LIMITSBS807+14 L= 1.500' W= 1' D= 0.020' FOUND OUT OF LIMITSTOOL= ID: ATS2472 S/N: UNKNOWN DATE: 12/2021 DUE: 12/2022IAW SRM 51-10-02 AND SRM 53-00-53-1A-2;[03] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTS;[FABRICATION OF REPLACEMENT FLOOR TO SIDEWALL SUPPORT BS727-847 LBL 21 IS ACCOMPLISHED ON CUSTOMER CARD TTG8Q00DDBZX

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727+11; BS 727+14; BS 727+18; BS 727A+10; BS 727A+14; BS 727B+2; BS 727B+6; BS 727B+10; BS 727C+2; BS 727C+6. / [01] REMOVED DAMAGE FROM THE FOLLOWING LOCATION: BS727+11 0.7LX0.6W D:0.09; BS727+14 0.8LX0.7W D:0.03; BS727+18 0.9LX0.7W D:0.07; BS727A+10 0.6LX0.5W D:0.06; BS727A+14 0.9LX0.7W D:0.04; BS727B+2 1.2LX0.6W D:0.04; B727B+6 0.7LX0.55W D:0.09; BS727B+10 0.8LX0.6W D0.05; BS727C+2 0.7LX0.7W D:0.02; BS727C+6 0.8LX0.6W D:0.14 IAW SRM 51-10-02; SRM 53-00-53-1A-2. ORIGINAL THICKNESS IS 0.40 PART FOUND TO BE OUT OF LIMIT. SRM 53-00-53-1A-2; BAC1496-377 IS FOUND TO BE APPLICABLE FOR THIS EVALUATION. CAL TOOL INFO. ID:ATS2595 S/N F03295; EXP; 02/2023;[05] FABRICATED ; LOCATED AND DRILLED NEW AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BETWEEN BS 727+4 T0 BS 767 ; FROM BAC1496-377 7075-T62 ; LOT# 1494598-1 ; IAW SRM 51-40-05-0G-0 AND DWG 146A7502; ID:0026;REV:-; APPLIED CHEMICAL CONVERSION AMM 51-21-41-370-802; OK TO APPLY PRIMER;[06] FABRICATED ; LOCATED AND DRILLED NEW AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AND SPLICE AT RBL 21 BETWEEN BS 727+4 T0 BS 767 ; FROM BAC1496-377 7075-T62 ; LOT# 1494598-1 ; IAW SRM 51-40-05-0G-0 AND DWG 146A7502; ID:0026;REV:-; APPLIED CHEMICAL CONVERSION AMM 51-21-41-370-802; OK TO APPLY PRIMER;

Part: RAIL — CORRODED (AFT CARGO) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY RAIL AT BS 887+16 RBL 8. / [01] REMOVED CORROSION ON ACB ON RAIL BS 887+16' RBL 8 IN L=1' X W=1' X D=0.009' FROM ORIGINAL TICKNESS OF 0.063' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR 4.A. FIG 103. USED TOOL :<BR>ID:ATS601 S/N:87172291 DATE:06/2022 DUE:06/2023;[02] VERIFIED CORRECTIVE ACTION 1 COMPLETED;[03] REMOVED AFT BAY RAIL BS 887-947 RBL 8 IAW SRM 51-40-02-0G-O;[04] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS ON AFT CARGO BAY RAIL AT BS 887+16 RBL 8 IAW SRM 53-00-53-1A-2;ALLOWABLE DAMAGE 2;[05] CORRECTION FOR CORRECTIVE ACTION #4 VERIFIED SRM 53-00-53-2R-4 IS APPLICABILITY FOR ACB -RAIL FLOOR BEAM REPAIR. BETWEEN STA 887-907; RBL 8.;[06] FABRICATED ALL REPAIR PARTS FOR ACB RAIL AT BS 887 TO BS 907+ 6 RBL 8 WL 170; MATERIAL USED BAC1509-100146#7075T76511 LOT#1456074-1 EXTRUSION; SPLICE PN 53100004-001 PO#838646/1 LOCATED AND DRILLED ALL REPAIR PARTS BETWEEN BS 887- BS 907+6 IAW SRM 53-00-53-2R-4 REPAIR 4 AND SRM 51-40-05. OK TO APPLY CHEMICAL CONV. COATING AND PRIMER TO REWORKED AREA AND PARTS.[17] INSTALLED ALL REPAIR PARTS FOR ACB RAIL AND SPLICE AT BS 887 TO BS 907+ 6 RBL 8 WL 170; IAW SRM 53-00-53-2R-4 REPAIR 4 AND SRM 51-40-02 DWG 147A7500 REV:- AND DWG146A7500 REV:A;[18] VERIFIED MEASUREMENT TABLE;[19] VERIFIED CORRECTIVE ACTION #17

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 22 BS 767+11; BS 767+15. / [01] NOT ALLOWABLE DAMEGE PER SRM ; PART WILL BE REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0; LOCATED ANDDRILLED NEW FWD CARGO DOOR SHIELD AT RBL 21 ; BS 767 TO BS 794.4 IAW SRM 51-40-05-0G-0 AND DWG 146A0081; ID:0025; REV:A;[02] VERIFIED CORRECTIVE ACTION #2; MEASUREMENT FIELD VERIFIED;[03] VERIFIED PART INSTALLED;[04] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED CORRECTIVE ACTION STEP 1 AND TASK CARD COMPLETE.

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 21 BS 847+6; BS 847+11. / [01] NOT ALLOWABLE DAMEGE PER SRM ; PART WILL BE REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] NOT ALLOWABLE DAMEGE PER SRM ; PART WILL BE REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0; LOCATED ANDDRILLED NEW AFT CARGO DOOR SHIELD AT RBL 21 ; BS 847 TO BS 867 IAW SRM 51-40-05-0G-0 AND DWG 146A0081; ID:0025; REV:A;[03] VERIFIED CORRECTIVE ACTION #2; MEASUREMENT FIELD VERIFIED;[04] VERIFIED PART INSTALLED;[05] VERIFIED MEASUREMENT FIELD COMPLETE AND TASK CARD COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 887+11; BS 887+19; BS 907+2; BS 907+13; BS 927+2. / [01] SRM 53-00-53-1A-2 FOUND TO BE APPLICABLE FOR THIS EVALUATION. REMOVED DAMAGE FROM THE FOLLOWING LOCATION: BS887+11 1.2LX1.0W D:0.008; BS887+19 0.6LX0.6W D:0.005; BS905+2 1.2LX0.5W D:0.010; BS905+13 1.1LX0.6W D0.004; BS927+2 0.8LX0.7W D:0.006 IAW SRM 51-10-02; SRM 53-00-53-1A-2. ORIGINAL THICKNESS IS 0.040 PART FOUND TO BE OUT OF LIMITS. IAW SRM 51-10-02; SRM 53-00-53-1A-2. BAC1496-377 CAL TOOL INFO. ID:ATS2595 S/N F03295; EXP; 02/2023;[02] VERIFIED CORRECTIVE ACTION #1;[03] JOB WILL BE ACCOMPLISH ON CUSTMER CARD NBR: TTG8Q00DDBZ4;[04] UPDATED MEASUREMENTS;[05] UPDATED MEASUREMENTS;[06] VERIFIED CORRECTIVE ACTION #3 AND MEASUREMENT FIELD

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON AFT CARGO BAY AFT LOWER BULKHEAD SUPPORT AT BS 947 LBL 8 - RBL 20. / [01] EVALUATED DAMAGE: NO SRM LIMITS FOR THIS PART REPAIR BY REPLACEMENT IAW SRM 51-10-02 PARA # 9.;[02] REMOVED ON AFT CARGO BAY AFT LOWER BULKHEAD SUPPORT AT BS 947 LBL 8 - RBL 20 IAW SRM 51-40-02.;[03] LOCATED AND DRILLED ON AFT CARGO BAY AFT LOWER BULKHEAD SUPPORT AT BS 947 LBL 8 - RBL 20. ITEM 149A8118-29;LOT#1497302-4 ;PO#875637/4; IAW SRM 51-40-05 AND DWG 149A8118-REV:A;[04] UPDATED MEASUREMENTS;[05] PART REQUIREMENT;[06] MADE COUNTERSINK IAW SRM 51-40-08/0G1. REQUEST OK TO INSTALL;[07] COUNTERSUNK BS 947 BULKHEAD SUPPORT IAW SRM 51-40-08/0G1. REQUEST OK TO INSTALL;[08] VERIFIED CORRECTIVE ACTIONS STEP 3;6. OK TO INSTALL GIVEN.;[09] BEGAN INSTALLING LOWER BULKHEAD SUPPORT AT BS 947 IAW SRM 51-40-02; DWG 149A8110 ID:0008 REV: A AND 149A8117 ID: 0006 REV: -;[10] INSTALLED LOWER BULKHEAD SUPPORT AT BS 947 IAW SRM 51-40-02; DWG 149A8110 ID:0008 REV: A AND 149A8117 ID: 0006 REV: -;[11] VERIFIED FASTENER INSTALLATION;[12] VERIFIED CORRECTIVE ACTION 9; 10 AND MEASUREMENT TABLE

Part: ATTACH BRACKET — CORRODED (R/H WING) · airframe 58,974 hrs · 35,001 cycles

CORROSION ON R/H AFT BOOST PUMP UPPER STRAP ATTACH BRACKET. / [01] REMOVED AND REPLACED R/H AFT BOOST PUMP UPPER STRAP ATTACH BRACKET PER SOPM 20-50-01. BONDING TESTCHECKED GOOD PER SWPM 20-20-00 AND SWPM 20-20-10. CAL ID: ATS1101 SN: 48 DUE: 03/2023;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION #1

Part: SIGN — LOOSE (OVERWING CABIN) · airframe 58,854 hrs · 34,925 cycles

EMERGENCY EXIT SIGN MID CABIN FELL OFF. / [01] R+R OVERWING EMERGENCY EXIT LIGHT SIGN PER AMM SIP.

Part: GIRT BAR — OUT OF POSITION (AFT ENTRY DOOR) · airframe 58,535 hrs · 34,711 cycles

AFT ENTRY DOOR ESCAPE SLIDE GIRT FLAP NOT PROPERLY SECURED TO SHELF. / [01] PROPERLY SECURED GIRT FLAP TO SHELF AT AFT ENTRY DOOR IN REF TO BOEING AMM 25-66-01

Part: GIRT BAR — OUT OF POSITION (AFT SERVICE DOOR) · airframe 58,535 hrs · 34,711 cycles

AFT SERVICE DOOR ESCAPE SLIDE GIRT FLAP NOT PROPERLY SECURED TO SHELF. / [01] PROPERLY SECURED SLIDE GIRT FLAP TO SHELF AT AFT SERVICE DOOR IN REF TO BOEING AMM 25-66-01

Part: DOOR — CRACKED (L/H MLG) · airframe 58,535 hrs · 34,711 cycles

L/H MAIN LANDING GEAR CENTER DOOR HAS 1/2 INCH CRACK AT FWD LOWER ATTACHMENT FRAME AREA / [01] OK TO CONTINUE ON CDL 32-10-3. LEFT MLG CENTER AND INNER DOORS REMOVED REF MM 32-13-11. REF MXI CARD TTG8Q00CA4GB

Part: SKIN — CRACKED (L/H HORIZ. STAB.) · airframe 58,535 hrs · 34,711 cycles

LH HORIZONTAL STABILIZER LOWER SKIN HAS A CRACK .75 LONG LOCATED 9.875 FWD OF AFT SPAR AT STAB STA 193.90 / [01] EA 22-155-01354 ISSUED.;[02] C/W EA 22-155-01354

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,535 hrs · 34,711 cycles

EMERGENCY LIGHT BATTER PACKS FAILED AT LOCATIONS M1674; M1672; M1673 EMERGENCY LIGHT BATTER PACKS FAILED AT LOCATIONS M1674 M1672 M1673 / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS M1674; M1672; M1673 PER AMM 33-51-06 AND DRW 33500005

Part: SKIN — CRACKED (RH HOR STAB) · airframe 58,535 hrs · 34,711 cycles

RH HORIZONTAL STABILIZER LOWER SKIN IS CRACKED 1 LONG LOCATED 9.625 FWD OF AFT SPAR AT STAB STA 193.90 / [01] EA 22-155-01353 ISSUED.;[02] C/W EA 22-155-01353

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,394 hrs · 34,614 cycles

CABIN FLOOR PANEL 241AF UPPER SURFACE HAS PULLED FIBERS / [01] EVALUATED PANEL 241AF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B 737-700 SRM 53-00-50-2R-1 PAR1A. CLEAN AND PREP FOR REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3A;C;E&F. VERIFIED MATERIALS AS: BMS 8-201 (A112601); BMS 9-3 (A10273). NEED OK TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES. IAW B737-700 SRM 53-00-50-2R-1 PAR 3 K-M. AAR DIGITAL THERMOMETER 30347 150DEG 3HRS.;[04] REPAIRED AREA'S OF PULLED FIBERS ON UPPER SURFACE OF PANEL 241AF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,394 hrs · 34,614 cycles

CABIN FLOOR PANEL 241AF LOWER SURFACE HAS PULLED FIBERS / [01] EVALUATED PANEL 241AF AND FOUND AREA OF PULLED FIBERS ON LOWER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP FOR REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3A;C;E&F. VERIFIED MATERIALS AS: BMS 8-201 (A112601); BMS 9-3 (A10273). NEED OK TO BOND.;[02] VERIFIED AND OK TO BOND;[03] BONDED REPAIR PLIES. IAW B737-700 SRM 53-00-50-2R-1 PAR 3K-M. AAR DIGITAL THERMOMETER 30347 150DEG 3HRS.;[04] REPAIRED AREA OF PULLED FIBERS ON LOWER SURFACE OF PANEL 241AF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,394 hrs · 34,614 cycles

CABIN FLOOR PANEL 242BF UPPER SURFACE HAS PULLED FIBERS / [01] EVALUATED DAMAGE; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1; TAP TEST GOOD NO DELAMINATION NOTED.<BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A;C;E;F; AND J.<BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1; TABLE 201; RESIN EPOCAST50A (A112601); FIBERGLASS CLOTH BMS9-3 (A10273). <BR><BR>REQUIRES OKAY TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES IAW B737 SRM 53-00-50-2R-1 PAR # STEPS K;L; AND M. CURED AT 150 DEGREES FOR 4 HOURS; DIGITAL THERMOMETER STAAR30347; CAL DUE 4/29/22. TAP TEST GOOD.;[04] REPAIRED CABIN FLOOR PANEL 242BF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 REPAIR 1.;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,394 hrs · 34,614 cycles

CABIN FLOOR PANEL 232RF UPPER SURFACE HAS PULLED FIBERS / [01] EVALUATED AND FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1.<BR>CLEANED AND PREPPED AREA IAW SRM 53-00-50-2R-1 STEPS 3A;C;E;F.<BR>VERIFIED BOND MATERIALS AS GLASS-(A10273); RESIN-(A112601) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR; TAP TEST GOOD IAW SRM 53-00-50-2R-1 STEPS 3K;L;M. OVEN----B0-06 DUE 5-15-22;[04] REPAIRED DAMAGE TO UPPER SURFACE IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1. TAP TEST GOOD.;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,394 hrs · 34,614 cycles

CABIN FLOOR PANEL 242AF UPPER SURFACE HAS PULLED FIBERS / [01] EVALUATED AND FOUND DAMAGE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 STEPS 3A;C;E;F<BR>VERIFIED REPAIR MATERIALS AS---GLASS (A10273); RESIN (A112601) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR; TAP TEST GOOD IAW SRM 53-00-50-2R-1 STEPS 3K;L;M TOOLING--- AAR 30347 DUE 4-29-22;[04] REPAIRED DAMAGE TO UPPER SURFACE OF FLOOR BOARD IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,394 hrs · 34,614 cycles

CABIN FLOOR PANEL 232SF UPPER SURFACE HAS PULLED FIBERS / [01] EVALUATED DAMAGE; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD; NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A;C;E;F; AND J.<BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201; RESIN EPOCAST50A (A112601); FIBERGLASS CLOTH BMS9-3 (A10273).<BR><BR>REQUIRES OKAY TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS K;L; AND M. CURED AT 150 DEGREES FOR 4 HOURS DIGITAL THERMOMETER AAR30347 CAL DUE 4/29/22. TAP TEST GOOD.;[04] REPAIRED CABIN FLOOR PANEL 232SF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 REPAIR 1.;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,394 hrs · 34,614 cycles

CABIN FLOOR PANEL 231ZF UPPER SURFACE HAS PULLED FIBERS / [01] EVALUATED AND FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 STEPS 3A;C;E;F<BR>VERIFIED REPAIR MATERIALS AS--- GLASS (A10273); RESIN (A112601) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR; TAP TEST GOOD IAW SRM 53-00-50-2R-1 STEPS 3K;L;M. TOOLING---AAR30347 DUE 4-29-22;[04] REPAIRED DAMAGE TO UPPER SURFACE FLOOR BOARD IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD.;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,394 hrs · 34,614 cycles

CABIN FLOOR PANEL 231XF UPPER SURFACE HAS PULLED FIBERS / [01] EVALUATED PANEL231XF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP FOR REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3A;C;E&F.VERIFIED MATERIALS AS: BMS 8-201 (A112601); BMS 9-3 (A10273). NEED OK TO BOND.;[02] VERIFIED AND OK TO BOND;[03] BONDED REPAIR PLIES. IAW B737-700 SRM 53-00-50-2R-1 PAR 3K-M. AAR DIGITAL THERMOMETER 30347 150DEG 3HRS.;[04] REPAIRED AREA OF PULLED FIBERS ON UPPER SURFACE OF PANEL 231XF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,394 hrs · 34,614 cycles

CABIN FLOOR PANEL 241BF UPPER SURFACE HAS PULLED FIBERS / [01] EVALUATED PANEL241BF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-2R-1 PAR 3A;C;E&F. VERIFIED MATERIALS AS: BMS 8-201 (A112601); BMS 9-3 (A10273). NEED OK TO BOND.;[02] VERIFIED AND OK TO BOND;[03] BONDED REPAIR PLIES. IAW B737-700 SRM 53-00-50-2R-1 PAR 3 K-M. AAR DIGITAL THERMOMETER 30347 150DEG 3HRS.;[04] REPAIRED AREA OF PULLED FIBERS ON UPPER SURFACE OF PANEL 241 BF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[05] VERIFIED STEPS 3-4

Part: ANGLE — CRACKED (CENTER WING) · airframe 58,394 hrs · 34,614 cycles

CRACK FOUND ON UPPER ATTACH ANGLE IN L/H A/C BAY AT STA 663 LBL 8 / [01] INSTALLED EWIZ PROTECTION IAW AMM 20-60-07-913-801.;[02] RECEIVED -1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE FABRICATED ON BACKSHOP W/O# 43543-5000-0002 AND 43543-5000-0001 IAW SRM 57-10-10-2R-5.

Part: FLOOR PANEL — DETERIORATED (FWD CARGO) · airframe 58,394 hrs · 34,614 cycles

FWD CARGO FLOOR PANEL 120CF HAS DETERIORATED REPAIR / [01] REMOVED FWD PIT FLOOR PANEL 120CF; IAW AMM 25-52-10-000-801.;[02] VERIFIED MATERIAL FOR REPLACEMENT FLOOR PANEL 120CF AS A90RG1W ; IAW AMM 25-52-01-201-801. A-TAG # A118133.;[03] VERIFIED STEP 2;[04] VERIFIED STEP 1;[05] FABRICATED REPLACEMENT FLOOR PANEL 120CF; IAW AMM 25-52-01-201-801. NEED OK TO INSTALL.;[06] VERIFIED STEP 5. OK TO INSTALL;[07] INSTALLED REPLACEMENT FLOOR PANEL 120CF; IAW AMM 25-52-10-400-801.;[08] VERIFIED STEP 7 AUDIT C/W

Part: STRUCTURE — WORN (CENTER WING) · airframe 58,394 hrs · 34,614 cycles

192DR OUTBD LATCH PAD ON WING TO BODY STRUCTURE IS WORN THROUGH STRUCTURE AND CRACKED RUB STRIP BELOW / [01] REMOVED 192DR SEAL AND SEAL RETAINER PER B737 SRM 57-0-13-2R-3 STEP 4.D.;[02] VERIFIED MATERIAL FOR -1 STRAP; -4 FILLER TO BE 7075-T6 CLAD .125' ATAG A82806 PER B737 SRM 57-10-13-2R-3 TABLE 201 AND 202;[03] VERIFIED ITEMS 1 AND 2;[04] VERIFIED ITEM 2 AS RII;[05] VERIFIED OUT OF LIMITS WITH 100% MATERIAL LOSS PER B737 SRM 57-10-13-1A-2;[06] REMOVED DAMAGED PORTION PER B737 SRM 57-10-13-2R-3 STEP 4.E.;[07] VERIFIED STEPS 5-6;[08] LOCATED AND DRILLED AND FABRICATED -1 STRAP AND -4 FILLER PER B737 SRM 57-10-13-2R-3 STEP 4.I. THRU 4.M.;[09] VERIFIED STEP 8.<BR>OK TO TREAT AND PRIME REPAIR PARTS.[20] INSTALLED NEW RUB STRIP AND SEAL AT 192DR OUTBD I/A/W SRM 51-40-02-OG-0;[21] RUB STRIP A TAG WN14803 AND SEAL A101850;[22] C/W;[23] VERIFIED STEPS 20 & 21

Part: PANEL — CRACKED (BELLY) · airframe 58,394 hrs · 34,614 cycles

FUSELAGE FAIRING 191AL; AFT SUPPORT FRAME IS CRACKED; O/B OF STR 19L; VIEWED FROM AFT SIDE / [01] REMOVED SUPPORT FRAME IAW ARM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW FAIRING SUPPORT FRAME PN: 116A3118U9 A-TAG: A123107 IAW DWG 116A3110 REV. B;[03] VERIFIED STEP 2 IS COMPLETE;[04] VERIFIED STEPS 1-3;[05] OK GIVEN TO INSTALL REPAIR PARTS;[06] INSTALLED NEW SUPPORT FRAME IAW SRM 51-40-02-0G-0 AND DWG 116A3110 REV. B;[07] APPLIED CIC TO NEW ANGLE AND DISTURBED SURFACES IN AREA IAW AMM 51-21-91-620-802;[08] VERIFIED STEPS 6 AND 7;[09] VERIFIED STEPS 6; 7 AND 8; JOB COMPLETE; AUDIT C/W

Part: LIGHT — LOOSE · airframe 58,032 hrs · 34,403 cycles

MID CABIN OVERHEAD EXIT SIGN LOOSE / [01] RESECURED EXIT SIGN IAW AMM 33-51-03

Part: ACCESS PANEL — FAILED (LH WING) · airframe 57,976 hrs · 34,368 cycles

FUEL LEAK LEFT WING / [01] REMOVED AND REPLACED L/H WING FUEL TANK ACCESS PANEL (532HB) IAW AMM 28-11-11

Part: SIGN — DISLODGED (CABIN) · airframe 57,073 hrs · 33,828 cycles

SUPPLEMENTAL INFORMATION: MID CABIN EXIT SIGNDISLODGED DURING BOARDING. ; / [01] REINSTALLED EXIT SIGN REF 33-51-01

Part: NONE — DELAMINATED (L/H WING) · airframe 56,832 hrs · 33,682 cycles

SUPPLEMENTAL INFORMATION: LEFT WING O\B AFT FLAP I\B LOWER CORNER DELAMINATED APPROX 6'X7'. ; / [01] R&R LH AFT FLAP REF 27-51-22

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,779 hrs · 33,061 cycles

L/H EMERGENCY EXIT DOOR LIGHT OUT ; / RE-LAMPED REF AMM 33-21-00; C/W

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 54,954 hrs · 32,590 cycles

AFT CARGO COMPARTMENT FLOOR BOARD JUST FWD OF DOOR CRACKED. / REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR BOARD JUST FWD OF DOOR PER SRM 51-40-10

Part: FLASHLIGHT — FAILED (CABIN) · airframe 54,954 hrs · 32,590 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01675. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION M01675 PER AMM 33-51-06.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,236 hrs · 32,171 cycles

FWD ENTRY, LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW MISSING. REMOVED & REPLACED DIRECTIONAL LIGHT LENS AT FWD ENTRY DOOR, REF AMM 33-51-01.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,236 hrs · 32,171 cycles

LEFT OVERWING DOOR LOWER LENS FOR EMERGENCY EXIT LIGHT MISSSING DIRECTIONAL ARROW. REPLACED LEFT OVERWING EMERGENCY EXIT LENS, REF AMM 33-51-01.

Part: RIB — CRACKED (HORIZOTNAL STAB) · airframe 54,053 hrs · 32,067 cycles

CRACK INSPAR RIB STAB STA 129.50 LOWER CHORD AT REAR SPAR POSITION LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB STAB STA 129.50 LOWER CHORD AT REAR SPAR POSITION LT HORIZONTAL STAB IAW ENGINEERING AUTHORIZATION EA NO.20-155-01598 REV.1 FOR FOLLOW UP REQUIREMENTS SEE TLD T078989 AND AEROMAN EA #55-0592-20 REV 0.

Part: SUPPORT ANGLE — CRACKED (BS 867 S26-27L) · airframe 54,053 hrs · 32,067 cycles

CRACK ANGLE-SUPPORT LOCATED BS 867 BETWEEN STR 26L AND STR27L AFT CARGO COMPARTMENT / REPLACED ANGLE-SUPPORT LOCATED BS 867 BETWEEN STR 26L AND STR 27L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 SHEET 16 REV.-

Part: SUPPORT — CORRODED (BS 807) · airframe 54,053 hrs · 32,067 cycles

CORROSION SUPPORT ZEE LOCATED BS 727D TO BS 807 STR 25L AND WL162.1 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED ON STA 727 TO STA 847 AT LEVEL ON STR 25L IAW B737-700 SRM 51-40-02 AND DRAWING #146A7500 REV.A AND SRM 53-00-53-2R-6 REPAIR 6.

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 54,053 hrs · 32,067 cycles

CORROSION CHANNEL BETWEEN BS 492.5 TO BS 500A AND RBL 24;STR 26R FWD CARGO COMPARTMENT; WL 157 / REPLACED CHANNEL BETWEEN BS 492.5 TO BS 500A AND RBL 24 STR 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 143A0080 REV.-

Part: STRINGER — CRACKED (BS 540) · airframe 54,053 hrs · 32,067 cycles

CRACK STRINGER 25L BS 540 FWD CARGO COMPARTMENT (1 EA). PERFORMED REPAIR STRINGER 25L BS 500D TO BS 540 IAW SRM B737-700 53-00-03-2R-1 REPAIR 1 FIGURE 206; SRM B737-700 51-40-02 AND AMM B737-700 33-42-02-960-802.

Part: SUPPORT — CRACKED (BS 747-767 S25R) · airframe 54,053 hrs · 32,067 cycles

CRACK SUPPORT ZEE BETWEEN BS 747 TO BS 767 AND STR 25R AFT CARGO COMPARTMENT / REPLACED SUPPORT ZEE LOC BTW BS 727 TO BS 767 AND STR 25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 146A7502 REV.-

Part: SUPPORT ANGLE — CRACKED (BS 500B S26L) · airframe 54,053 hrs · 32,067 cycles

CRACK ANGLE - SUPPORT BS 500B AND STR 26L FWD CARGO COMPARTMENT(1 EA) / REPLACED ANGLE-SUPPORT LOCATED AT BS 500B AND STR 26L FWD CARGO COMPARTMENT IAW SRM 737-700 51-10-02 ITEM 9 AND DRAWING 143A7505

Part: SUPPORT ANGLE — CRACKED (BS 500C S26L) · airframe 54,053 hrs · 32,067 cycles

CRACK ANGLE - SUPPORT BS 500C AND STR 26L FWD CARGO COMPARTMENT(1 EA) / REPLACED ANGLE-SUPPORT LOCATED AT BS 500C AND STR 26L FWD CARGO COMPARTMENT IAW SRM 737-700 51-10-02 ITEM 9 AND DRAWING 143AT505

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 54,053 hrs · 32,067 cycles

CRACK GUSSET BS 500D AND STR 19R FWD CARGO COMPARTMENT (1EA) / REPLACED GUSSET BS500D AND STR 19R FWD CARGO COMPARTMENT (1EA) IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG #143A7902 REV:-

Part: SUPPORT ANGLE — CRACKED (BS 400 S26L) · airframe 54,053 hrs · 32,067 cycles

CRACK ANGLE - SUPPORT BS 400 AND STR 26L FWD CARGO COMPARTMENT (1EA) / REPLACED ANGLE-SUPPORT BS 400 AND STR 26L FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 AND DWG 143A7505 REV.B

Part: SUPPORT PLATE — CRACKED (BS 540) · airframe 54,053 hrs · 32,067 cycles

CRACK FLOOR SUPPORT PLATE LOCATED BS540 BETWEEN LBL24.5 TO RBL45 CENTER SECTION (3EA) / REPLACED FLOOR SUPPORT PLATE LOCATED BS540 BTW LBL 24.5 TO RBL45 CENTER SECTION (3EA) IAW SRM B737-700 51-40-02 SRM 51-10-02 PARAGRAPH 9 AND DRAWING # 143A0060 SHEET 36 REV A

Part: SUPPORT ANGLE — CRACKED (BS 685-706) · airframe 54,053 hrs · 32,067 cycles

CRACK SUPPORT ANGLE LOCATED BETWEEN BS685 TO BS706 AND BL0 CENTER SECTION (2EA). REPLACED SUPPORT ANGLE LOC BETWEEN BS 685 TO BS 706 AND BL0 CENTER SECTION (2EA) IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG #273A9110 REV A.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 54,053 hrs · 32,067 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT / REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975. REPAIR 1 ITEM 1;2;3;4 AB(2)(4)

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,053 hrs · 32,067 cycles

CRACK INSPAR RIB LOCATED STAB STA 129.50 AND 26 INCHES FROM FRONT SPAR LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON IN SPAR RIB LOCATED STA 129.50 AND 26 INCHES FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4.

Part: RIB — CRACKED (HORIZOTNAL STAB) · airframe 54,053 hrs · 32,067 cycles

CRACK LEADING EDGE RIB ACCESS PANEL 331B LE ST 170.34 AT LT HORIZONTAL STABILIZER. REPLACED RIB LOC LEADING EDGE ACCESS PANEL 331B LE 170.34 AT LT HORIZONTAL STABILIZER IAW B737- 700 SRM 51-40-02; 51-10-02 AND DWG 186A1001 REV.B.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,053 hrs · 32,067 cycles

CRACK INSPAR RIB LOCATED STAB STA 92.7 AND 11 INCHES FROM FRONT SPAR LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED AT STAB STA 92.7 AND 11 INCHES FROM FRONT SPAR LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10- 09-2R-5 REPAIR 5.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,053 hrs · 32,067 cycles

CRACK LEADING EDGE RIB ACCESS PANEL 331B LE STA 291.21 AT LT HORIZONTAL STABILIZER. REPLACED RIB LOC LEADING EDGE ACCESS PANEL 331B LE STA 292.21 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 186A1001 REV.B.

Part: LIGHT — CRACKED (CABIN) · airframe 54,053 hrs · 32,067 cycles

CRACK FLOOR PHOTOLUMINESCENT STRIP RT SIDE AT PASSENGER CABIN (5EA). REPLACED FLOOR PHOTOLUMINESCENT STRIP RT SIDE AT PASSENGER CABIN IAW AMM 33-51-15- 400-802.

Part: LIGHT — CRACKED (CABIN) · airframe 54,053 hrs · 32,067 cycles

CRACK FLOOR PHOTOLUMINESCENT STRIP LT SIDE AT PASSENGER CABIN (5EA). REPLACED FLOOR PHOTOLUMINESCENT STRIP LT SIDE AT PASSENGER CABIN IAW AMM 33-51-15-400-802.

Part: STOP FITTING — CRACKED (R1 DOOR) · airframe 53,054 hrs · 31,409 cycles

R1 DOOR LOWER AFT STOP FITTING CRACKED. / R&R DOOR ASSEMBLY IAW AMM.

Part: LENS — DETACHED (KEMERGENCY LIGHT) · airframe 52,898 hrs · 31,307 cycles

EXIT SIGN AT CEILING BY OVERWING EXIT BECAME DETACHED. / REATTACHED LIGHTS LENS IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,647 hrs · 30,491 cycles

EXTERNAL EMERGENCY LIGHTS RT SIDE BEHIND FLAP AND AFT DOOR INOP. RELAMPED EMERGENCY LIGHTS PER AMM.

Part: LIGHT — INOPERATIVE (EXRTERIOR) · airframe 51,014 hrs · 30,071 cycles

L2 EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED REF AMM 33-51-04.

Part: LIGHT — INOPERATIVE (ROW 17) · airframe 50,754 hrs · 29,912 cycles

L/H EMERGENCY EXIT LIGHT INOP AT ROW 17. R&R LIGHT PER MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,821 hrs · 29,338 cycles

STA. 540 CENTER RT. FLOOR BOARD INTERCOSTAL IS CRACKED / REMOVED AND REPLACED CENTER RT FLOOR BOARD INTERCOSTAL ASSY AT STA 540 IAW SRM 51-40-02

Part: COVER — CRACKED (CABIN) · airframe 48,821 hrs · 28,709 cycles

RT EMERGENCY EXIT LOWER RED PULL STRAP COMPARTMENT COVER CRACKED. R&R COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,582 hrs · 28,570 cycles

LT EMERGENCY STOW BIN LIGHT INOP AT SEAT ROW 24. R&R BULB IAW AMM.

Part: SUPPORT BRACKET — CRACKED (MAIN CABIN) · airframe 48,582 hrs · 28,570 cycles

BRACKET SUPPORT BROKEN STA 867 STR 1-2R. / REMOVED AND REPLACED BRACKET STA 867 STR 1-2 CABIN IAW SRM 51-40-02-0G-0 VERIFIED P/N 287A4015-9 IAW BOEING DWG 146A7901 RECV - ATAG A35851

Part: BEAM — CRACKED (R1 DOOR) · airframe 48,582 hrs · 28,570 cycles

R1 DOOR BEAM NR 4 FOUND CRACKED. R&R NR 4 BEAM IAW SRM & DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 48,582 hrs · 28,570 cycles

R1 DOOR BEAM NR 5 FOUND CRACKED. R&R NR 5 BEAM IAW DWG.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 48,582 hrs · 28,570 cycles

FORWARD CARGO DOOR CUTOUT AFT THRESHOLD CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 48,582 hrs · 28,570 cycles

LT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 31. REPAIRED WEB IAW EA.

Part: BRACKET — CRACKED (LT WING) · airframe 48,582 hrs · 28,570 cycles

LT WING TRAILING EDGE Z BRACKET CRACKED AT WS 156.25. R&R "Z" BRACKET IAW SRM & DWG.

Part: SEAL — CRACKED (RT WING) · airframe 48,582 hrs · 28,570 cycles

DOT 43; RH WING T/E WS 253.00 WEB SEAL RETAINER CRACKED / REMOVED WEB SEAL RETAINER; RH WING T/E WS 253.00; DRILLED REPLACEMENT WEB SEAL RETAINER; INSTALLED WEB SEAL RETAINER; I/A/W SRM 51-40-02-0G-0 STEP 4; SRM 51-40-05-0G-0 FIG 3; SRM 51-40-02 STEP 4

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 48,582 hrs · 28,570 cycles

AFT CARGO DOOR CUTOUT FWD CORNER THRESHOLD HAS 2 EACH CRACKS / WELD REPAIR ACCOMPLISHED UNDER BACK SHOP WORK ORDER 38368-8300-0001 IAW SOUTHWEST EA NO: 1-A53-2076 REF: 11

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 48,582 hrs · 28,570 cycles

FORWARD CARGO DOOR CUTOUT FORWARD THRESHOLD CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: SEAL — CRACKED (LT WING) · airframe 48,582 hrs · 28,570 cycles

DOT 33; LH WING T/E WS 253; WEB SEAL RETAINER CRACKED (MARKED) / REMOVED WEB SEAL RETAINER. LOCATED AND DRILLED NEW WEB SEAL RETAINER AND INSTALLED IAW BOEING 737-700 SRM 51-40-05-0G-0 AND SRM 51-40-02-0G-0.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 48,582 hrs · 28,570 cycles

AFT CARGO DOOR CUTOUT AFT CORNER THRESHOLD HAS 1 EACH CRACK / WELD REPAIR ACCOMPLISHED UNDER BACK SHOP W/O 38368-8300-0002 IAW SOUTHWEST EA NO. 1-A53-2076 REV: 11.

Part: PLATE — BROKEN (L/H WING) · airframe 48,582 hrs · 28,570 cycles

DOT 31; LH WING T/E WS 253 WIGGLE PLATE; RIVETS BROKE OFF AND PULLED THROUGH / REMOVED AND REPLACED DAMAGE L/H WING T/W WS 253 WIGGLE PLATE WITH A NEW P/N 115A2781-13 (ST7570132) A TAG #WN9872. IAW SRM 57-40-02-0G-0; DWG #115A2001 REV- DWG #115A2714 REV-

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 48,582 hrs · 28,570 cycles

TRAILING EDGE PANEL 551FB; ATTACH ANGLE IS CRACKED AT FWD EDGE OF PANEL; 26' FROM O/B END. / REMOVED AND INSTALLED NEW ATTACH ANGLE TO PANEL 551 FB I.A.W B737-700 SRM 51-40-02-0G-0

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 48,025 hrs · 28,211 cycles

L/H HORIZONTAL STAB. UPPER FWD. SLIDING SEAL IS CRACKED / REMOVED AND REPLACED L/H HORIZONTAL STAB. UPPER FWD. SLIDING SEAL PER AMM. 53-31-31

Part: SKIN — CRACKED (LEFT WING) · airframe 47,657 hrs · 27,958 cycles

L/H WING LEADING EDGE SKIN ABOVE KRUEGER FLAPS HAD A COUNTERSINK CRAKC INDICATION DURING NDT PART 6 53-30-00 PROCEDURE 3 INSPECTION ON THE 9TH HOLE FORWARD OFTH SKIN'S OUTBOARD/AFT CORNER. / REPAIR TO BE ACCOMPLISHED ON EA 1-757-15266 PART AND DOCUMENTED ON DEFECT NUMBER D216461

Part: GUARD — BROKEN (COCKPIT) · airframe 47,249 hrs · 27,699 cycles

P5 OVERHEAD PANEL EMERGENCY EXIT LIGHT ARMING SWITCH GUARD ON BROKEN. R&R SWITCH GUARD IAW SOPM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 46,109 hrs · 26,978 cycles

FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY INOP. R&R BATTERY IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 45,695 hrs · 26,712 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: HYDRAULIC LINE — DAMAGED (NLG WW) · airframe 45,333 hrs · 26,481 cycles

DIVERSION/DECLARED EMERGENCY, SUSPECTED BIRD STRIKE ON TAKEOFF. HYDRAULIC QUANTITY LOSS IN-FLIGHT. INSTALLED HYDRAULIC LINE PER AMM.

Part: STRUCTURE — BROKEN (EMERGENCY LIGHT) · airframe 42,747 hrs · 24,891 cycles

AFT EMERGENCY EXIT LIGHT BASE BROKEN. R & R BASE ASSEMBLY IAW AMM.

Part: STRIP — DAMAGED (CABIN) · airframe 42,687 hrs · 24,857 cycles

RT EMERGENCY FLOOR TRACK GLOW STRIP DAMAGED AT ROW 1. R&R STRIP PER AMM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 42,133 hrs · 24,557 cycles

LT HORIZONTAL STABILIZER RIB CRACKED AT STA 120.30, STIFFENER 2ND ONE AFT FROM FRONT SPAR. REPAIRED STIFFENER PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 42,133 hrs · 24,557 cycles

LT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.70, AT STIFFENER 2ND ONE AFT FROM FRONT SPAR. REPAIRED RIB PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

FLOOR SUPPORT CRACKED AT BS 540, BETWEEN RBL 0 TO RBL 25. R&R SUPPORT PER SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

AFT CARGO BAY STRAP CORRODED AT BS 804, RBL 19. R&R STRAP IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 42,133 hrs · 24,557 cycles

RT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT STA 92.70 AT THE 1ST, 2ND, AND 3RD VERTICAL STIFFENERS LOWER RADIUS. REPAIRED RIB IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

AFT CARGO BAY DOOR SUB THRESHOLD CORRODED. R&R THRESHOLD IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

LT FLOOR TO SIDEWALL SUPPORT ZEE CORRODED BETWEEN BS 400 TO BS 500D. R&R ZEE IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 492 TO BS 500A. R&R SHIELD IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

FORWARD CARGO BAY FRAME SIDEWALL SUPPORT CORRODED AT BS 440, BETWEEN STR 18R TO STR 25R. REPAIRED SUPPORT PER ER AND EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

FORWARD CARGO BAY AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED BETWEEN STR 25L TO STR 25R. R&R ANGLE IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 420 TO BS 440. R&R SHIELD IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

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

Part: SHIELD — CORRODED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 794. R&R SHIELD IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

RT FLOOR TO SIDEWALL SUPPORT ZEE CORRODED BETWEEN BS 500A TO BS 500D. R&R ZEE IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

FORWARD CARGO BAY DOOR SUBTHRESHOLD WEB CORRODED. R&R WEB IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LT. R&R SUPPORT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

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

Part: BEAM — CRACKED (R1 DOOR) · airframe 42,133 hrs · 24,557 cycles

R1 DOOR FORWARD STUB BEAM CRACKED AT BS 294.5, WL 208. R&R STUB BEAM IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 32. R&R INTERCOSTAL IAW DWG AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294.5, BL 0. R&R INTERCOSTAL IAW DWG AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

FRAME CRACKED AT BS 380, STR 86. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,133 hrs · 24,557 cycles

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

Part: WIRE HARNESS — FAULTY (NR 2 ENGINE) · airframe 42,066 hrs · 24,522 cycles

NR 2 ENGINE AT FL410, EGT SURGED TO 810 DEGREE. RAN SURGE QRC/QRH AND HAD TO RUN NR 2 AT IDLE TO MAINTAIN EGT 500 DEGREE. DID NOT SHUT DOWN NR 2. USED ENGINE NORMALLY AT 10,000 MSL. NO VIBRATION NO N1/N2 OR OIL ISSUES. JUST ERRATIC EGT UNTIL LOWER ALTITUDE. NR 2 THRUST REVERSER NOT USED. R & R THE NR 2 ENGINE J10 HARNESS IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 41,765 hrs · 24,353 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1672. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 41,765 hrs · 24,353 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1668. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 41,765 hrs · 24,353 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1673. R & R THE BATTERY IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 41,765 hrs · 24,353 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1670. R & R BATTERY PACK IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 41,765 hrs · 24,353 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1675. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 41,765 hrs · 24,353 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1674. R & R THE BATTERY IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 41,765 hrs · 24,353 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1669. R & R THE BATTERY PACK IAW AMM.

Part: OVERHEAT SYS — MALFUNCTIONED (WING TO BODY) · airframe 41,511 hrs · 24,195 cycles

RIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. DIVERTED. R & R THE WING TO BODY OVERHEAT UNIT IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,505 hrs · 23,009 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 38,725 hrs · 22,573 cycles

RIGHT WING SIDEWALL EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,680 hrs · 22,547 cycles

LEFT DOOR EMER EXIT LIGHT INOPERATIVE. REPAIRED LIGHT IAW MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 37,764 hrs · 22,000 cycles

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

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 37,268 hrs · 21,711 cycles

THE RIGHT OVERWING EXIT LIGHT FOUND INOPERATIVE. R & R THE LIGHT ASSY IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 35,510 hrs · 20,692 cycles

LEFT WING OTBD AFT FLAP LOWER INBD CORNER DELAMINATED. R & R AFT FLAP IAW MM.

Part: PLATE — LOOSE (LT WING) · airframe 35,510 hrs · 20,692 cycles

LEFT WING WAFFLE PLATE LOOSE AFT OF REAR SPAR AT ORSS 261. R & R WAFFLE PLATE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

LEFT LOWER BULKHEAD SKIN CHORD CRACKED AT BS 540, STRINGER 22L FROM FWD FASTENER 2 ROWS AT 3 & 9 O'CLOCK POSITION. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

LEFT LOWER BULKHEAD SKIN CHORD CRACKED AT BS 540, STRINGER 22L FROM AFT HOLE AT 6 O'CLOCK POSITION. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

LEFT LOWER BULKHEAD SKIN CHORD CRACKED AT BS 540, STRINGER 22L FROM AFT FASTENER 2 ROWS. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,510 hrs · 20,692 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 124.50, 20 INCHES REAR SPAR. REPAIRED SKIN IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

OUTBOARD FWD FLANGE FWD HOLE CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

OUTBOARD FWD FLANGE AFT HOLE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

OUTBOARD FWD FLANGE FWD HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

INBOARD FWD FLANGE AFT HOLE CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

OUTBOARD FWD FLANGE FWD HOLE CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

OUTBOARD FWD FLANGE AFT HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,510 hrs · 20,692 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 138.70, 16 INCHES FROM FRONT SPAR. REPAIRED SKIN IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

LEFT NR 3 FLIGHT DECK WINDOW E - F POST CRACKED ON HOLE NR 8. REPAIRED WINDOW POST IAW ACO.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,510 hrs · 20,692 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 138.70, 9 INCHES FROM FRONT SPAR. REPAIRED SKIN IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

INBOARD FORWARD FLANGE FORWARD HOLE CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE PER EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

OUTBOARD FWD FLANGE FWD HOLE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

OUTBOARD FWD FLANGE FWD HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

FORWARD INBD FLANGE AFT HOLE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

INBOARD FWD FLANGE FWD HOLE CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

INBOARD FWD FLANGE AFT HOLE CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,510 hrs · 20,692 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 184.70, 10 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,510 hrs · 20,692 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 101.90, 20 INCHES FWD OF AFT SPAR. REPAIRED SKIN IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,510 hrs · 20,692 cycles

INBOARD FWD FLANGE AFT HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: TAB — DAMAGED (RT ELEVATOR) · airframe 35,165 hrs · 20,488 cycles

RIGHT ELEVATOR TAB DAMAGED AT MIDDLE OF TE. R & R TAB IAW AMM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 34,731 hrs · 20,224 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,812 hrs · 19,140 cycles

FWD ENTRY EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACKS IAW AMM.

Part: BRACKET — CRACKED (LT WING) · airframe 32,812 hrs · 19,140 cycles

LT WING UPPER TE PANEL ANGLE BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,812 hrs · 19,140 cycles

AFT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACKS IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,812 hrs · 19,140 cycles

MID CABIN EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACKS IAW AMM.

Part: FITTING — LOOSE (L1 DOOR) · airframe 32,311 hrs · 18,841 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP ASSEMBLY LOOSE. R & R CLIP ASSEMBLY IAW SIP.

Part: SLIDING WINDOW — CRACKED (COCKPIT) · airframe 31,288 hrs · 18,240 cycles

FIRST OFFICER`S SLIDING WINDOW ARCED & CRACKED. R&R WINDOW IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 29,419 hrs · 17,155 cycles

R2 DOOR SLIDE LOWER FLAP OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 29,419 hrs · 17,155 cycles

R1 DOOR SLIDE LOWER FLAP OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 29,359 hrs · 17,120 cycles

FORWARD ENTRY EXIT SIGN COVER FELL OFF. REPLACED LIGHT PER MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 28,707 hrs · 16,738 cycles

VERTICAL PANEL ATTACH BEAM LOWER ANGLE STRAP CRACKED AT STA 867, STR 26L. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,707 hrs · 16,738 cycles

EMERGENCY EXIT LIGHT ON AFT LAV IS DAMAGED. REMOVED AND REPLACED AFT LAV EMERGENCY EXIT LIGHT, OPERATION TEST GOOD IAW AMM 33-51-01-960-802.

Part: ISOLATOR — BROKEN (EMERGENCY EXIT) · airframe 28,707 hrs · 16,738 cycles

LEFT EMERGENCY EXIT HAS A BROKEN ISOLATOR. REMOVED BROKEN ISOLATOR FROM LEFT EMERGENCY EXIT IAW SRM 51-40-02-0G-0, INSTALLED NEW ISOLATOR, A-TAG #A25727, IAW SRM 51-40-02-0G-0 AND BOEING DWG 144A8103 REV B.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,707 hrs · 16,738 cycles

STA 321 LBL 12 FLOORBOARD BREAK CRACKED AT FASTENER HOLE. REMOVED AND REPLACED STA 321 LBL 12 FLOORBOARD BREAK/INTERCOSTAL IAW SRM 51-40-02, SRM 51-40-05, AMM 51-21-91, AND DWG 140N4500.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,707 hrs · 16,738 cycles

STA 360 LBL 12 INTERCOSTAL CRACKED AT FASTENER HOLE. REMOVED INTERCOSTAL AT STA 344-360 LBL 12 AND DRILL UP NEW INTERCOSTAL. INSTALLED ALSO DINOL NEW INTERCOSTAL IAW SRM 51-40-02, SRM 51-40-05, AMM 51-21-91 AND DWG 141A5506.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,707 hrs · 16,738 cycles

INTERCOSTAL CRACKED AT BS 354, BL 0. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND BOEING DWG.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 28,707 hrs · 16,738 cycles

PASSENGER CABIN WET AREA FLOORBOARD CRACKED. REPAIRED FLOORBOARD IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,707 hrs · 16,738 cycles

STA 321 LBL 46 INTERCOSTAL CRACKED AT FASTENER HOLE. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW ONE IAW B737-700 SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 LOCATED ATTACH HOLE FOR FLOORBOARD AND INTERCOSTAL HOLES IAW SRM 51-40-05-0G-0.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,707 hrs · 16,738 cycles

STA 307 BL 0 INTERCOSTAL CRACKED AT FASTENER HOLE. REMOVED INTERCOSTAL AT 5TA 294-312 BL 0. DRILLED UP NEW INTERCOSTAL AND INSTALLED. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-40-02, SRM 51-40-05 AMM 51-21-91.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,707 hrs · 16,738 cycles

STA 304 RBL 15 INTERCOSTAL CRACKED AT 2 EA FASTENER HOLES. REMOVED AND REPLACED INTERCOSTAL AT STA 304 RBL 15 IAW SRM 51-40-05, AMM 51-21-91 AND DWG 141A5410.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,707 hrs · 16,738 cycles

RIGHT HORIZ STAB LOWER IN-SPAR SKIN CRACKED IN SKIN O/B OF RIB. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,707 hrs · 16,738 cycles

LEFT HORIZ STAB LOWER IN-SPAR SKIN CRACKED I/B SIDE OF RIB TO TRAILING EDGE OF PANEL. REMOVED AND REPLACED SKIN IAW MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,707 hrs · 16,738 cycles

RIGHT HORIZ STAB LOWER IN-SPAR SKIN CRACKED I/B SIDE OF RIB TRAILING EDGE OF PANEL. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,707 hrs · 16,738 cycles

RIGHT HORIZ STAB LOWER IN-SPAR SKIN CRACKED 16.125" FROM TRAILING EDGE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,707 hrs · 16,738 cycles

LEFT HORIZ STAB LOWER IN-SPAR SKIN CRACK I/B OF RIB TRAILING EDGE OF PANEL. REPAIRED SKIN IAW SRM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 28,707 hrs · 16,738 cycles

FORWARD CARGO PIT OPENING FORWARD CORNER SCUFF PLATE PLATE IS CRACKED. REMOVED AND ROUTED TO BACK SHOP TO WELD RACK IN SCUFF PLATE. REWORK AND WELDING COMPLETED IAW EA 1-A53-2076 REV 10.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,707 hrs · 16,738 cycles

RIGHT HORIZ STAB LOWER IN-SPAR SKIN CRACKED I/B SIDE OF 157.10 RIB FROM TRAILING EDGE OF PANEL. REMOVED AND REPLACED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,707 hrs · 16,738 cycles

RIGHT HORIZ STAB LOWER IN-SPAR SKIN, I/B SIDE OF RIB 111.10, 19.312" TO 20.312" SKIN PANEL CRACKED. REMOVED AND REPLACED SKIN IAW MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,707 hrs · 16,738 cycles

LEFT HORIZ STAB LOWER IN-SPAR SKIN CRACK I/B OF RIB TRAILING EDGE OF PANEL. REMOVED AND REPLACED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,707 hrs · 16,738 cycles

RIGHT HORIZ STAB LOWER IN-SPAR SKIN CRACKED I/B SIDE OF RIB FROM TRAILING EDGE OF PANEL. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,707 hrs · 16,738 cycles

LEFT HORIZ STAB LOWER IN-SPAR SKIN CRACK O/B OF RIB. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,707 hrs · 16,738 cycles

LEFT HORIZ STAB LOWER IN-SPAR SKIN CRACK I/B OF RIB TRAILING EDGE OF PANEL. REMOVED AND REPLACED SKIN IAW SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 28,510 hrs · 16,630 cycles

LEFT WING T/E VERTICAL BULB SEAL RETAINER CRACKED OUTBOARD OF NR 3 FLAP TRACK. REMOVED AND REPLACED BRACKET PER MM AND SRM 51-40-02.

Part: COVER — OUT OF POSITION (CABIN) · airframe 27,498 hrs · 16,062 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER PLATE FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 27,331 hrs · 15,960 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: VALVE — FAILED (FUEL SYSTEM) · airframe 28,831 hrs · 19,811 cycles

FUEL CROSS FEED VALVE INOP. REMOVED AND REPLACED FUEL CROSS FEED VALVE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 25,242 hrs · 14,750 cycles

LT EEPLS COVER CRACKED AT ROW 20. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 25,162 hrs · 14,700 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS MISSING AT ROW 18. INSTALLED LENS PER MM.

Part: GASPER FAN — FAULTY (CARGO BAY) · airframe 22,258 hrs · 12,983 cycles

DIVERSION - DURING CRUISE, SMELLED WHAT APPEARED TO BE ELECTRICAL SMOKE / FUMES IN COCKPIT AND CABIN. NEVER SAW SMOKE. SMELLED SEEMED TO DISSIPATE AFTER GASPER/RECIRC OFF. REMOVED AND REPLACED GASPER FAN PER MM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 22,179 hrs · 12,931 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX FUEL TANK STIFFENER CRACKED AT BS 549, RBL 6. REMOVED AND REPLACED STIFFENER PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,169 hrs · 12,925 cycles

DURING SCHEDULED 6Y CHECK, FOUND BULKHEAD CRACKED AT BS 663, RBL 39 HOLE NR 7 DOWN 6 INCHES FROM TOP. REPAIRED BULKHEAD PER EA.

Part: WEB — CRACKED (CENTER WING BOX) · airframe 22,169 hrs · 12,925 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX WEB CRACKED AT BS 663, LBL 43. REPAIRED WEB PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,169 hrs · 12,925 cycles

DURING SCHEDULED 6Y CHECK, FOUND BULKHEAD CRACKED AT BS 663, RBL 39 HOLE NR 6 DOWN 5 INCHES FROM TOP. REPAIRED BULKHEAD PER EA.

Part: WEB — CRACKED (CENTER WING BOX) · airframe 22,169 hrs · 12,925 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB PER EA.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 22,169 hrs · 12,925 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX FUEL TANK STIFFENER CRACKED AT BS 549, RBL 14. REMOVED AND REPLACED STIFFENER EPR SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 22,169 hrs · 12,925 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX FUEL TANK STIFFENER CRACKED AT BS 549, LBL 32. REMOVED AND REPLACED STIFFENER EPR SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 22,169 hrs · 12,925 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX FUEL TANK STIFFENER CRACKED AT BS 549, LBL 14. REMOVED AND REPLACED STIFFENER EPR SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 22,169 hrs · 12,925 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX FUEL TANK STIFFENER CRACKED AT BS 549, LBL 5. REMOVED AND REPLACED STIFFENER EPR SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 22,169 hrs · 12,925 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX FUEL TANK STIFFENER CRACKED AT BS 549, RBL 32. REMOVED AND REPLACED STIFFENER EPR SRM.

Part: COVER — MISSING (CABIN) · airframe 22,137 hrs · 12,903 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: COVER — MISSING (EXIT SIGN) · airframe 21,282 hrs · 12,386 cycles

AFT GALLEY EMERGENCY EXIT SIGN COVER MISSING. REMOVED AND REPLACED SIGN PER MM.

Part: LENS — MISSING (CABIN) · airframe 21,291 hrs · 12,392 cycles

FWD EEPLS LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 19,546 hrs · 11,416 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: BRACKET — LOOSE (L1 DOOR) · airframe 19,546 hrs · 11,416 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW BRACKET LOOSE. SECURED BRACKET PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 19,546 hrs · 11,416 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 19,508 hrs · 11,389 cycles

FWD SECTION EEPLS DAMAGED. REMOVED AND REPLACED EEPLS ASSY PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 17,315 hrs · 10,055 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER MM.

Part: CAP — MISSING (CABIN) · airframe 17,315 hrs · 10,055 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS END CAP MISSING AT ROW 1. REMOVED AND REPLACED END CAP PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 16,295 hrs · 9,458 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 16,133 hrs · 9,352 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 14,986 hrs · 8,674 cycles

DURING SCHEDULED HC2 CHECK , FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 111. REPAIRED SKIN PER SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 14,986 hrs · 8,674 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY LIGHT STRIP CRACKED. REMOVED AND REPLACED EMERGENCY LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 14,986 hrs · 8,674 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 EMERGENCY EXIT DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 13,735 hrs · 7,945 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 13,014 hrs · 5,701 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 13,014 hrs · 5,701 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — LOOSE (CABIN) · airframe 12,514 hrs · 7,191 cycles

EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 12,383 hrs · 7,110 cycles

EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 12,374 hrs · 7,104 cycles

EEPLS LIGHT ASSY LOOSE AT ROW 1 ABC. SECURED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,643 hrs · 6,685 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 10,798 hrs · 6,176 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 9,992 hrs · 5,708 cycles

EEPLS COVER MISSING AT 1 ABC. INSTALLED COVER PER MM.

Part: CAP — LOOSE (CABIN) · airframe 9,937 hrs · 5,681 cycles

DURING SCHEDULED 1/2DHC2 CHECK, FOUND EEPLS END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,666 hrs · 5,534 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 2 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 8,789 hrs · 4,989 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 3 ABC. INSTALLED COVER PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 8,635 hrs · 4,905 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,785 hrs · 3,841 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 1,055 hrs · 600 cycles

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