N490WN

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,792 hrs · 38,139 cycles

LEFT SIDE (CAPTAINS SIDE) ROW 1 AND 4 BIN EMERGENCY AISLE EXIT LIGHTS DO NOT ILL LEFT SIDE (CAPTAINS SIDE) ROW 1 AND 4 BIN EMERGENCY AISLE EXIT LIGHTS DO NOT ILLUMINATE<[01] REMOVED AND REPLACED FWD GALLEY LEFT SIDE BATTERY PACK IAW AMM 33-51-06; EMERGENCY LIGHTS OPS CHECK GOOD.

Part: SLIDE — OUT OF LIMITS (ZN 800 DOOR) · airframe 63,581 hrs · 38,008 cycles

AFT SERVICE DOOR SLIDE NOT IN GREEN<[01] REMOVED + REPLACED AFT SERVICE SLIDE PACK IAW M/M 25-66-01 + MT#725-61-06-AS

Part: FUSE — INOPERATIVE (ZN 200 FUS TOP) · airframe 60,453 hrs · 35,959 cycles

R OVERWING EXIT EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED POWER SUPPLY FUSES; BATTERY PACK AND BATTERY CHARGER ASSY PER AMM 33-51-06 NO HELP.;[02] DISCONNECTED R OVER WING EMERGENCY EXIT SIGN; CLEANED CORROSION ; RECONNECTED SIGN. OPS CHECK GOOD REF MM 33-51-01.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 60,453 hrs · 35,959 cycles

R OVERWING EXIT EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED POWER SUPPLY FUSES; BATTERY PACK AND BATTERY CHARGER ASSY PER AMM 33-51-06 NO HELP.;[02] DISCONNECTED R OVER WING EMERGENCY EXIT SIGN; CLEANED CORROSION ; RECONNECTED SIGN. OPS CHECK GOOD REF MM 33-51-01.

Part: CHARGER — INOPERATIVE (ZN 200 FUS TOP) · airframe 60,453 hrs · 35,959 cycles

R OVERWING EXIT EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED POWER SUPPLY FUSES; BATTERY PACK AND BATTERY CHARGER ASSY PER AMM 33-51-06 NO HELP.;[02] DISCONNECTED R OVER WING EMERGENCY EXIT SIGN; CLEANED CORROSION ; RECONNECTED SIGN. OPS CHECK GOOD REF MM 33-51-01.

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 59,880 hrs · 35,571 cycles

RH EXIT DOOR UPPER AND LOWER AFT EMERGENCY LIGHTS INOP / [01] REPLACED DAMAGED FUSE ON BATTERY CHARGER M1669 AND PERFORMED GOOD TEST PER AMM 33-51-06-690-804.<BR>-COMPLETED STEP 1.;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.<BR>VERIFIED STEP 1.

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 59,880 hrs · 35,571 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1673 ARE INOP / [01] REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK M1673 AND PERFORMED GOOD TEST PER AMM 33-51-06-960-805.;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.

Part: FLOOR PANEL — DAMAGED (CABIN FLOOR) · airframe 59,880 hrs · 35,571 cycles

PASSENGER CABIN FLOOR PANEL 241ABF HAS 3 EACH INSERTS THAT DOES NOT ALIGN WITH HOLES IN STRUCTURE=R/H SIDE; AFT INBOARD AFT 3 HOLES / REMOVED DAMAGE FROM UPPER SURFACE MEASURING 13'X3' APPLIED BMS5-28 TY19 LOT#AK2DP3091K POTTING COMPOUND TO (3EA) FASTENER HOLES; CURED POTTING UNDER HEAT LAMP USING THERMOMETER ID:ATS2208 DUE:10/2022; SANDED POTTING FLUSH; AND CLEANED IAW SRM 53-00-50-2R-1 PAR.3 G-J;RELOCATION OF INSERT HOLES REQUIRES REPAIR TO BOTH SKINS AND CORE REPAIR TO BE ACCOMPLISHED PER SRM 53-00-50-2R-6 REMOVED POTTING COMPOUND FROM INSERT HOLES; FABRICATED CORE PLUGS FROM BMS8-124 TYPE 5 GRADE 9 LOT#1287137 AND UPPER SURFACE REPAIR PLIES FROM BMS9-3 H2 LOT#1493221 INSTALLED CORE PLUGS USING BMS5-28 TYPE 19 POTTING LOT#AK2DP3091K AND REPAIR PLIES USING BMS8-201 TYPE 4 LOT#AK2CP8139K; VACUUM BAGGED CURED; UNBAGGED AND SANDED REPAIR FLUSH WITH INITIAL SURFACE; CLEANED REPAIR AREA AND FABRICATED REPAIR PLIES FOR LOWER SURFACE FROM BMS9-3 H2 LOT#1493221-1; OK TO INSTALL IAW SRM 53-00-50-2R-6 PARA 3I-K;[16] ITEM #15 USED THERMOMETER ATS2208 CAL DUE DATE 10/2022;INSTALLED REPAIR PLIES USING BMS8-201 TYPE 4 LOT#AK2CP8139K; VACUUM BAGGED;CURED REPAIR PLIES UNDER HEAT LAMP USING THERMOMETER ID:ATS2208 DUE:10/2022; REMOVED VACUUM BAG INSTALLED (3EA) THROUGH INSERTS USING BMS5-107 CL1 LOT#AK1KP9159K; CURED INSERTS UNDER HEAT LAMP USING THERMOMETER ID:ATS2208 DUE:10/2022 IAW SRM 53-00-50-2R-6 PAR.3 N & BOEING DWG 147A5810-88

Part: FLOOR PANEL — MISALIGNED (FUSELAGE) · airframe 59,880 hrs · 35,571 cycles

DUE TO REPAIR OF BS 986 FLOORBEAM; AT SPLICE LOCATION;PASSENGER CABIN FLOOR PANEL 242VF HAS 2 EACH INSERTS THAT DOES NOT ALIGN WITH HOLES IN STRUCTURE= FWD EDGE OF PANEL-MARKED / [01] IDENTIFIED PANEL 242VF IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6<BR><BR>DAMAGED AREA EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR.4 E(2)<BR><BR>DAMAGE IS REPAIRABLE IAW SRM 53-00-50-2R-1<BR><BR>REMOVED (3EA) THROUGH INSERTS TO FACILITATE REPAIR<BR>REMOVED DAMAGE FROM UPPER SURFACE MEASURING 15'X3'; CLEANED; WITH NO CONTAMINATION NOTED IAW SRM 53-00-50-2R-1 PAR.3 A-F 08] RELOCATION OF INSERT HOLES REQUIRES REPAIR TO BOTH SKINS AND CORE REPAIR TO BE ACCOMPLISHED PER SRM 53-00-50-2R-6 <BR><BR>REMOVED POTTING COMPOUND FROM INSERT HOLES; FABRICATED CORE PLUGS FROM BMS8-124 TYPE 5 GRADE 9 LOT#1287137 AND UPPER SURFACE REPAIR PLIES FROM BMS9-3 H2 LOT#1493221-1; OK TO INSTALL IAW SRM 53-00-50-2R-6 PARA 3C-G;[13] CURED; UNBAGGED AND SANDED REPAIR FLUSH WITH INITIAL SURFACE; CLEANED REPAIR AREA AND FABRICATED REPAIR PLIES FOR LOWER SURFACE FROM BMS9-3 H2 LOT#1493221-1; OK TO INSTALL IAW SRM 53-00-50-2R-6 PARA 3I-K<BR><BR>USED THERMOMETER ATS2208 CAL DUE DATE 10/2022;[16] INSTALLED REPAIR PLIES USING BMS8-201 TYPE 4 LOT#AK2CP8139K; VACUUM BAGGED; CHECKED FOR LEAKS; LEAK CHECKED GOOD USING VACUUM GAUGE ATS2107 CAL DUE DATE 09/2022 IAW SRM 53-00-50-2R-6 PARA 3K-L;

Part: FLOOR PANEL — OUT OF POSITION (FUSELAGE) · airframe 59,880 hrs · 35,571 cycles

PASSENGER CABIN FLOOR PANEL 241AAF HAS 1 EACH INSERT THAT DOES NOT ALIGN WITH HOLE IN STRUCTURE=L/H SIDE; AFT OUTBOARD CORNER HOLE / [01] IDENTIFIED FLOOR PANEL 241AAF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6. FLOOR PANEL PROVIDED FROM STOCK WAS BAD. THE FLOOR PANEL HAS 1 INSERT THAT DOES NOT ALIGN WITH THE STRUCTURE. FLOOR PANEL REQUIRES REPLACEMENT AND CAN BE FABRICATED IAW SRM 53-00-50-2R-0 PARAGRAPH 1.A AND PARAGRAPH 4.<BR><BR>FABRICATED REPLACEMENT FLOOR PANEL USING BMS 4-17 TY6 LOT# 1486491-1 AND INSTALLED INSERTS USING BMS5-107 LOT# AK1KP9159K AND CURED INSERTS USING THERMOMETER ID: ATS2208 CAL DUE: 10/2022. IAW SRM 53-00-50-2R-1 PARAGRAPH 4.A(1) AND 5.S(1); AND BAC DWG 147A5810 ID:008.;[02] CORRECTION TO ITEM #1 'IAW SRM 53-00-50-2R-1 PARAGRAPH 4.A(1) AND 5.S(1) TO SAY 'IAW SRM 53-00-50-2R-0 PARAGRAPH 4.A(1) AND 5.S(1)';[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2;[04] ATTACHED INSERT CURE SHEET TO THIS FAULT RECORD.;[05] FINAL INSPECTION. JOB COMPLETE PER SRM 53-00-50-2R-1 AND BAC DWG 147A5810 ID:008.

Part: PANEL — DELAMINATED (RH WING) · airframe 59,880 hrs · 35,571 cycles

R/W FUELING PANEL 621GB HAS DELAMINATIONS TO INNER SURFACE (MARKED) / [01] IDENTIFIED PANEL IAW SRM 57-41-01-0I-4 FIG 1; DRAWING 116A8500 PL SHT 15; DRAWING 116A8520 & 116A8501; AND AIPC 57-40-00-51 ITEM 100. DAMAGE IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.D (5)(B)1). DAMAGE IS TO BE REPAIRED IAW SRM 51-70-05-2R-1 AS GIVEN IAW SRM 57-41-01-2R-1 PARA 4.B(1) TABLE 201. 350 DEGREE PREPREG REPAIR. REMOVED DAMAGE TO INNER SURFACE AND TAPER SANDED REPAIR AREAS AT (5EA) LOCATIONS ALL IAW SRM 51-70-05-2R-1 PARA 4.A & 4.B.;[02] VALIDATED APPLICABILITY OF REPAIR TO BE COMPLETED IAW SRM 51-70-05-2R-1.;[03] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 1 AND 2.;[04] FABRICATED REPAIR PLIES FROM BMS 8-139ST1581 LOT#1491914-1 AND ADHESIVE BMS 5-154GR5 LOT#1493149-1; INSTALLED; VACUUM BAGGED; LEAK CHECK GOOD WITH VACUUM GAUGE ID:ATS2545 CAL DUE 08/2022 IAW SRM 51-70-05-2R-1 PARA 4C-D.<BR>REPAIR NEEDS CURE;[05] CURED REPAIR WITH HOTBONDER ID:ATS883 CAL DUE 10/2022; UNBAGGED AND LIGHTLY SANDED IAW SRM 51-70-05-2R-1 PARA 4E;G.;[06] VERIFIED CORRECTIVE ACTION ITEMS 4 AND 5. UT INSPECTED REPAIR PER NDTM PART 4; 51-00-02. NO DISBONDS NOTED.<BR>CAL ID: ATS2342 S/N: 190848504 DUE: 07/2023;[07] R/W FUELING PANEL 621GB DELAMINATION'S TO THE INNER SURFACE WERE REPAIRED IAW SRM 51-70-05-2R-1.;[08] FINAL INSPECTION. JOB COMPLETE PER SRM 51-70-05-2R-1.

Part: WIRE — BROKEN (AFT FUSELAGE) · airframe 59,880 hrs · 35,571 cycles

BROKEN WIRE AT AFT PASSENGER CABIN BS947+5 S-2R. MARKED. / [01] REPAIRED WIRE W3058-0147-22 WITH SPLICE IAW SWPM 20-10-13 AND SWPM 20-30-12; AS WELL AS WDM 23-42-11. TOOLING: ID: ATS1543 DUE: 10/2022;[02] PERFORMED GOOD CONTINUITY CHECK OF W3058-0147-22 IAW WDM 23-42-11.<BR>CAL TOOL: ATS1499 DUE 02/2023;[03] VERIFIED CORRECTIVE ACTION #1; #2.;[04] PERFORMED GOOD TEST OF EMERGENCY EXIT LOCATOR SIGN L1223 PER AMM 33-51-00-710-801.;[05] VERIFIED CORRECTIVE ACTION 4 AND MEASUREMENT TABLE.

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

FWD CARGO BAY L/H BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT AT BS 460-480 LBL 23 IS CRACKED / [01] VERIFIED APPLICABILITY FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT;PER SRM 51-10-02 PARA#9.;[02] REMOVED FWD CARGO BAY L/H BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT AT BS 460-480 LBL 23 WL 156 IAW SRM 51-40-02;[03] LOCATED AND DRILLED ; FWD CARGO BAY L/H BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT AT BS 460-480 LBL 23 WL 156 IAW SEM 51-40-02 AND DWG143A7505 REV:-.OK TO INSTALL;[04] CORRECTION STEP 3 # LOCATED AND DRILLED ; FWD CARGO BAY L/H BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT AT BS 460-480 LBL 23 WL 156 P/N 143A7510-13 LOT# 1487893-2 PO#863594/2 IAW SRM 51-40-05 AND DWG143A7505 REV:-.OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION #4 .OK TO INSTALL GIVEN;[06] VERIFIED MEASUREMENT TABLE;[07] INSTALLED FWD CARGO BAY L/H NEW BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT AT BS 460-480 LBL 23 WL 156 P/N 143A7510-13 LOT# 1487893-2 PO#863594/2 IAW SRM 51-40-02 AND DWG143A7505 REV:-.;[08] VERIFIED CORRECTIVE ACTION 7;[09] VERIFIED MEASUREMENT TABLE

Part: WEB — CRACKED (RH WING) · airframe 59,880 hrs · 35,571 cycles

RT WING T/E SEAL WEB TO DEFLECTION CONTROL RIB IS CRACKED / [01] FOUND NO APPLICABLE SRM REPAIR FOR CRACKED RT WING T/E SEAL WEB TO DEFLECTION CONTROL RIB ANGLE; THEREFORE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9. REMOVED AND REPLACED CRACKED ANGLE PER SRM 51-40-02-0G-0 PARAGRAPH 4. VERIFIED FASTENER CALLOUT PER AIPC 57-42-51-02 ITEM NO. 16.;[02] CORRECTIVE ACTION 1 SHOULD READ: FOUND NO APPLICABLE SRM REPAIR FOR CRACKED RT WING T/E SEAL WEB TO DEFLECTION CONTROL RIB; THEREFORE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9. REMOVED AND REPLACED CRACKED WEB PER SRM 51-40-02-0G-0 PARAGRAPH 4. VERIFIED FASTENER CALLOUT PER AIPC 57-50-00-36 ITEM NO. 240 AND 235.;[03] VERIFIED CORRECTIVE ACTIONS STEP 1;2.

Part: FLOOR PANEL — DAMAGED (CABIN FLOOR) · airframe 59,880 hrs · 35,571 cycles

AFT CABIN FLOOR PANEL 242UF HAS 2 RIPPED OUT INSERTS ALONG THE AFT EDGE. (MARKED) / OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B REMOVED DAMAGE TO 2 FACESHEETS AND CORE AT 2EA INSERT HOLES ON AFT EDGE OF PANEL AND CLEANED REPAIR AREA. FABRICATED CORE PLUGS FROM BMS8-124 CLASS 4 TYPE 5 GRADE 9 LOT#1287137 AND LOWER SURFACE REPAIR PLIES FROM BMS9-3 H2 LOT#1493221-1; INSTALLED CORE PLUGS USING BMS5-28 TYPE 19 LOT#AK2KP3091K AND REPAIR PLIES USING BMS8-201 TYPE 4 LOT#1496781-1; VACUUM BAGGED; CHECKED FOR LEAKS; LEAK CHECKED GOOD USING VACUUM GAUGE ATS2107 CAL DUE DATE 09/2022 AND SET FOR CURE FABRICATED REPAIR PLIES FROM BMS9-3 H2 STYLE 1581 LOT#1493221-1; OK TO INSTALL IAW SRM 53-00-50-2R-6 PARA 3K;[08] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 6 AND 7. OKAY TO INSTALL REPAIR PLIES PER SRM 53-00-50-2R-6.;[09] INSTALLED REPAIR PLIES USING BMS8-201 TYPE 4 LOT#1496781-1; VACUUM BAGGED; CHECKED FOR LEAKS; LEAK CHECKED GOOD USING VACUUM GAUAGE ATS2107 CAL DUE DATE 09/2022 IAW SRM 53-00-50-2R-6 PARA 3K-L;[10] INSPECTED AND VERIFIED CORRECTIVE ACTION 14. 5X5 LEAK CHECK PASSED PER SRM 53-00-50-2R-6.;[11] CURED REPAIR PLIES USING HEAT LAMP CURE IAW SRM 53-00-50-2R-1 PARA 3.M (1); LOCATING AND INSTALLATION OF INSERTS ACCOMPLISHED ON TTG8Q00DUH5R;[14] VERIFIED CORRECTIVE ACTION #11; #12; #13

Part: ACCESS PANEL — CORRODED (AFT ENTRY DOOR) · airframe 59,880 hrs · 35,571 cycles

AFT ENTRY DOOR LOWER HINGE ACCESS PANEL 834DZ HAS CORROSION AT INNER SURFACE LOWER EDGE; 9' FROM AFT EDGE. / [01] RECEIVED NEW AFT ENTRY DOOR LOWER HINGE ACCESS PANEL 834DZ; TO BE INSTALLED ON TASK CARD TTG8Q00CULFB;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] UPDATED MEASUREMENT TABLE;[04] VERIFIED MEASUREMENTS

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 59,880 hrs · 35,571 cycles

EMERGENCY EXIT BATTERY CHARGER AT M1669 WON'T CHARGE BATTERY / [01] REPLACED EMERGENCY EXIT BATTERY CHARGER AT M1669 PER AMM 33-51-06-960-806; STEP 5.E.(4).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] COMPLETED STEP 1.;[04] VERIFIED STEP 1 COMPLETE.

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON WEB AT AFT CARGO BAY BS787+11 RBL20. / REMOVED CORROSION ON WEB AT AFT CARGO BAY BS 787+11 RBL 20 IAW SRM 51-10-02 MEASURES: L= 10' W= 3' REQUIRES NDT FOR REMAINING THICKNESS;[03] UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2.<BR>REMAINING MATERIAL THICKNESS IS 0.049' ADJACENT TO 0.056'. <BR>EQUIP USED: -EPOCH 650 ID: ATS2031 CAL DUE: 03/23;[04] EVALUATE DAMAGE: ORIGINAL THICKNESS IS 0.056' PER SRM 53-60-15-01-1 IDENTIFICATION; MAX MAT LOSS AREA IS L= 10' W= 3' XD= .007' REMAINING THICKNESS= 0.049' FOUND TO BE OUT LIMITS; REWORKED AREAS IAW SRM 53-60-15-1A-1 ALLOWABLE DAMAGE;[05] VERIFIED CORRECTIVE ACTION 4.;[06] REMOVED ON WEB AT AFT CARGO BAY BS787 TO 847 RBL20 IAW SRM 51-40-02-0G-0;[07] RECIVED NEW WEB ITEM 146A8123-10 LOT 1484898-1 LOCATED AND DRILLED NEW WEB AT BS 787 TO 847 RBL 20; IAW 737-700 SRM 51-40-05-0G-0 DWG 146A8121-;[08] OK TO INSTALL;[09] VERIFIED CORRECTIVE ACTION ITEM 6-8; OK TO INSTALL. MEASUREMENT FILED PART NUMBER DOESN'T MATCH PART RECEIVED AND THIS IS NOT A MAJOR REPAIR.;[10] CORRECTIVED MEASUREMENT 14; 22;[11] PART NUMBER FIELD ITEM 14 STILL INCORRECT;[12] CORRECTIVED MEASUREMENT ITEM 14;[13] INSTALLED NEW WEB AT BS 787 TO 847 RBL 20 WL160 . IAW 737-700 SRM 51-40-02-0G-0; DWG 146A8121 AND DWG 146A8120 .

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON WEB AT AFT CARGO BAY BS807+4 RBL20. / [01] CORRECTED STEPS 1 & 2.;[02] REMOVED CORROSION ON WEB AT AFT CARGO BAY BS 807+4 RBL 20 IAW SRM 51-10-02 MEASURES: L=1' W=1' <BR><BR> REQUIRES NDT FOR REMAINING THICKNESS;[03] UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2. REMAINING MATERIAL THICKNESS IS 0.052' ADJACENT TO 0.056'. <BR>EQUIP USED: -EPOCH 650 ID: ATS2031 CAL DUE: 03/23;[04] EVALUATE DAMAGE: ORIGINAL THICKNESS IS 0.056' PER SRM 53-60-15-01-1 IDENTIFICATION; MAX MAT LOSS AREA IS L= 1' W= 1' XD= .007' REMAINING THICKNESS= 0.049' FOUND TO BE OUT LIMITS; REWORKED AREAS IAW SRM 53-60-15-1A-1 ALLOWABLE DAMAGE;[05] THIS TARJET ACCOMPLISH WITH CARD TTG8Q00DR65P;[06] CORRECTED; THIS FAULT WILL BE ACCOMPLISHED ON CARD TTG8Q00DR65P;[07] VERIFIED STEPS 1 AND 2; CORRECTIVE ACTION 6 AND VERIFIED MEASUREMENT TABLE.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON FLOORBEAM AT AFT CABIN BS986 RBL40 - RBL43. / CUT AND REMOVED THE DAMAGED FLANGES OF THE UPPER CHORD OF THE FLOOR BEAM FROM L/H END TO R/H END IAW SRM 53-70-51-2R-4 REPAIR 4 STEP 4B; INSTALLED BACR15CE8AD DOUBLE FLUSH RIVET TO PLUG THE INITIAL TOOLING HOLE AND MICROSHAVED THE RIVET PLUSH IAW SRM 53-70-51-2R-4 REPAIR 4 STEP 4E(2);(3);(4) FLAP PEEN THE CUT EDGE WITH 200% COVERAGE IAW SRM 53-70-51-2R-4 REPAIR 4 STEP 4 D;CUT ON THE TOP FORWARD OF THE INTERCOSTAL TO REMOVE THE MATERIAL THAT IS IN THE REPAIR AREA IAW SRM 53-70-51-2R-4 REAPR 4 STEP 4F(3);FLAP PEEN THE CUT EDGE WITH 200% COVERAGE IAW SRM 53-70-51-2R-4 REPAIR 4 STEP 4F(5)PERFORMED SHOT PEEN 4 EA -8 CORNER FITTINGS IAW SRM 53-70-51-2R-4 REPAIR 4 STEP 4G(3);(A);[29] VERIFIED CORRECTIVE ACTIONS #27 AND #28 VERIFIED MEASUREMENT TABLE;[30] LOCATED AND DRILLED NEW CLIPS PN#147A5615 (2EA) & PN#147A5615-6 (2EA) AND FABRICATED 4 EA STRUCTURAL FILLERS FROM 7075T6#0.090' CLAD LOT# 1482311-1. TREATED IAW SRM 53-70-51-2R-4 REPAIR 4 AND IAW EA#22-153-02234-WIP1. OK TO PRIME;[31] VERIFIED CORRECTIVE ACTION #30 OK TO PRIME GIVEN;[32] FABRICATED -1 T-CHORD FROM BAC1505-101474#7050T76511 LOT# 1482297-1; -2 (2EA) ANGLES FROM BAC1490-2811#7075T6 LOT# 1491932-1; -3 (2EA) ANGLES FROM BAC1490-2900#7075T6 LOT# 1495938-1 AND -4 (2EA) STRAPS FROM 7075T6#0.080' LOT# 1379745-1. TREATED IAW SRM 53-70-51-2R-4 REPAIR 4 AND IAW EA# 22-153-02234-WIP1. OK TO PRIME.;[33] LOCATED AND DRILLED NEW -7 L

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02 STEP#9. REMOVED GUSSET CRACKED AT BS500D;STR 19L;WL 193 AT FWD CARGO BAY;IAW SRM 51-40-02. LOCATED AND DRILLED NEW GUSSET WITH P/N 143A9481-6;LOT#1480476-3;IAW SRM 51-40-05 AND DWG#143A7902.OK TO INSTALL.;[02] VERIFIED CORRECTIVE ACTION 1 OK TO INSTALL GIVEN.;[03] INSTALLED NEW GUSSET AT BS 500D;STR 19L;WL193 AT FWD CARGO BAY;IAW SRM51-40-02 AND DWG#143A7902.ALL MAINTENANCE ACTIONS ARE COMPLETE REQUIRE FINAL BUY OFF.;[04] INSPECTION COMPLETE;[05] INSPECTION COMPLETE; VERIFIED MEASUREMENT TABLE

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON BS 986 FLOORBEAM; RBL 35; WL 208 / [01] REMOVED CORROSION FROM PASSENGER CABIN FLOORBEAM BS 986 RBL 35; WL 208 IN AREA OF 1.5' X 1'X 0.09' DEEP ORIGINAL MATERIAL THICKNESS 0.150' FOUND TO BE IN LIMIT IAW SRM 53-70-51-1A-1 DET. 4H; FIG 103-C TOOLS USED MICROMETER ID: ATS1671; S/N:65093024; DUE10/2022;[02] REMOVED CORROSION FROM PASSENGER CABIN FLOORBEAM BS 986 RBL 35; WL 208 IN AREA OF 1.5' X 1'X 0.09' DEEP ORIGINAL MATERIAL THICKNESS 0.150' FOUND TO BE OUT OF LIMIT IAW SRM 53-70-51-1A-1 DET. 4H; FIG 103-C<BR>TOOLS USED MICROMETER ID: ATS1671; S/N:65093024; DUE10/2022;[03] VERIFIED APPLICABILITY OF SRM 53-70-51-01-1 FOR IDENTIFICATION AND SRM 53-70-51-1A-1 FOR ALLOWABLE LIMIT;[04] VERIFIED CORRECTIVE ACTION 2 AND 3 COMPLETED AND VERIFIED OUT OF LIMITS;[05] 'REFER TO FAULT TTG8Q00DQKNA WHERE EA 22-153-02234 WAS ADDED AS A SUBTASK. 'FAULT RESOLVED ON OTHER FAULT' REPAIR REFERENCE IS SELECTED.;[06] VERIFIED CORRECTIVE ACTION 5;[07] VERIFIED MEASUREMENTS.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON BS 986 FLOORBEAM LBL 44; WL 208 / [01] REMOVED CORROSION FROM PASSENGER CABIN FLOORBEAM BS 986 LBL 44; WL 208 IN AREA OF 1' X 1'X 0.110' DEEP ORIGINAL MATERIAL THICKNESS 0.150' FOUND TO BE IN LIMIT IAW SRM 53-70-51-1A-1 DET. 4H; FIG 103-C<BR>TOOLS USED MICROMETER ID: ATS1671; S/N:65093024; DUE10/2022;[02] REMOVED CORROSION FROM PASSENGER CABIN FLOOR BEAM BS 986 LBL 44; WL 208 IN AREA OF 1' X 1'X 0.110' DEEP ORIGINAL MATERIAL THICKNESS 0.150' FOUND TO BE OUT OF LIMIT IAW SRM 53-70-51-1A-1 DET. 4H; FIG 103-C TOOLS USED MICROMETER ID: ATS1671; S/N:65093024; DUE10/2022;[03] VERIFIED APPLICABILITY OF SRM 53-70-51-01-1 FOR IDENTIFICATION AND SRM 53-70-51-1A-1 FOR ALLOWABLE LIMIT;[04] VERIFIED CORRECTIVE ACTION 2 AND 3 COMPLETED AND VERIFIED OUT OF LIMITS;[05] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-70-51-2R-4 (REPAIR 4) AND EA 22-153-02234;[06] VERIFIED ITEM 5 CORRECTIVE ACTIONS.<BR>VERIFIED MEASUREMENTS.

Part: CHANNEL — CORRODED (CABIN FLOOR) · airframe 59,880 hrs · 35,571 cycles

AFT R/H MOPSILL HAS CORROSION BS 957-986; RBL 47-50; WL 208 / [01] REMOVED CORROSION ON PASSENGER CABIN MOP SEAL AT RBL 47-50 BS 957- BS 986 W.L 208.1 P/N 147A8540-8;AREA OT=0.080;RT=0.068 ;L=30.000'W=1.200'' ;X=0.012;FOUND TO BE OUT LIMITS I.A.W SRM 53-70-15-1A-1FOR ALLOWABLE DAMAGE AND SRM 53-70-15-0I-1 FOR IDENTIFICATION AND IT WILL REPAIRABLE BY REPLACEMENT I.A.W 51-10-02-0G PAR 9C .<BR>TOOL USED ID ATS1671; S/N:65093024; DATE: 01/2023;[02] REMOVED AFT SERVICE DOOR MOP SILL AT RBL 47-50 BS 957- BS 986 W.L 208.1 P/N 147A8540-8; I.A.W SRM 51-40-02-0G-0;[03] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.;[04] RECIVED NEW MOP SEAL ITEM 7530246; LOCATED AND DRILLED NEW MOP SEAL AT RBL 47-50 BS 897 TO 1016 W.L 208.1 ; IAW 737-700 SRM 51-40-05-0G-0 DWG 147A8501 OK TO INTALL.;[05] VERIFIED CORECTIVE ACTION 4.;[06] INSTALLED NEW R/H MOPSILL AT BS 910 TO 1016; LBL 47-50 WL 208 IAW SRM 51-40-02-0G-0; DWG 147A8501; 147A0000 CARD IS COMPLETED;[07] CORRECTED ITEM 6 : INSTALLED NEW R/H MOPSILL AT BS 910 TO 1016; LBL 47-50 WL 208 IAW SRM 51-40-02-0G-0; DWG 147A8501 REV:C 147A0000 CARD IS COMPLETED;[08] UPDATED PART USED;[09] VERIFIED CORRECTIVE ACTION #7 AND MEASUREMENT FIELD;[10] VERIFIED CORRECTIVE ACTION #7 AND MEASUREMENT FIELD

Part: FLOOR PANEL — CRACKED (CABIN FLOOR) · airframe 59,880 hrs · 35,571 cycles

AFT CABIN FLOOR PANEL 241ADF AFT O/B CORNER IS CRACKED. / [01] IDENTIFIED FLOOR PANEL 241ADF IAW SRM 53-00-50-0I-1 TABLE 6 FIG 6DAMAGED NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4 DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-6 REMOVED ALL DAMAGE TO AFT O/B OF PANEL AND CLEANED REPAIR AREA IAW SRM 53-00-50-2R-6 PARA 3C-EFABRICATED CORE PLUG FROM BMS8-124 TYV GR5 CL4 LOT# 1287137 AND FABRICATED REPAIR PLIES FOR UPPER SURFACE USING BMS9-3 ST1581 LOT# 149322-1. OKAY TO INSTALL CORE PLUG AND UPPER SURFACE PLIES IAW SRM 53-00-50-2R-6 PARAGRAPH 3.F.G(1)INSTALLED CORE PLUG USING BMS5-28 TY19 LOT# AK2DP3091K AND INSTALLED REPAIR PLIES ON LOWER SURFACE USING BMS8-201 TYIII LOT#AK2CP8139K AND VACUUM BAGGED; LEAK CHECKED VACUUM BAG GOOD USING VACUUM GAUGE ID: 11543 CAL DUE: 08/2022 AND SET TO CURE IAW SRM 53-00-50-2R-6 PAR. 3.K(1)L.(1).;[07] CORRECTION FOR ITEM 6: 'IAW SRM 53-00-50-2R-6 PAR. 3.K(1)L.(1).' TO SAY 'IAW SRM 53-00-50-2R-6 PAR. 3.G(1)H(1).';[08] RII VERIFIED CORRECTIVE ACTION ITEM 6-7.;CURED REPAIR PLIES AND CORE PLUG ON THE UPPER SURFACE USING THERMOMETER ID: ATS2209 CAL DUE: 10/2021; AND VACUUM GAUGE ID: 11543 CAL DUE: 08/2022 AND REMOVED VACUUM BAG AND TRIMMED REPAIR EDGES; AND SANDED CORE PLUG TO CONTOUR IAW SRM 53-00-50-2R-6 PARAGRAPH 3.I(1). FABICATED LOWER SURFACE REPAIR PLIES FROM BMS 9-3 H2 LOT#1493221-1; INSTALLED REPAIR PLIES USING BMS8-201 TYPE 4 LOT#1482288-1; COMPLETED SUCCESSFUL CURE

Part: SIDEWALL SUPPORT — CORRODED (FWD CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS420 RBL23. / [01] REMOVED SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS420 RBL23 IAW 51-40-02;[02] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT CARGO BAY BS400-BS420 RBL 23 AT DISCREPANCY AREA BS 420 L=1.500' W=0.800' D= 0.017 ORIGINAL THCHNESS 0.040' REMAINING MAT 0.023' MAT LOSS 0.017' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 USED TOOL ID ATS 1672 DUE 03/2023 VERIFIED SRM APPLICABILITY AND OUT OF LIMITS PER SRM 53-00-53-1A-2 STEP 4.A 2;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLE.;[04] FABRICATED ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS.400-420 FROM BAC1496-444#7075T62 LOT#1490548 IAW SRM 51-40-05 AND DWG 143A7501 OK APPLIED A CHEMICAL CONVERSION COATING;[05] OK TO PRIME;[06] VERIFIED CORRECTIVE ACTIONS 4 AND 5. OK TO PRIME GIVEN.;[07] APPLIED PRIME AT FABRICATED ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS.400-420 IAW SOPM 20-41-02;[08] VERIFIED CORRECTIVE ACTION ITEM 7.;[09] ALL STEPS ARE COMPLETE;[10] SIDEWALL SUPPORT WILL BE INSTALLED WITH AD COSTUMER CARD; 5330-E-16461-NG; ALL STEPS ARE COMPLETE;[11] VERIFIED CORRECTIVE ACTION 10.

Part: TENSION TIE — CORRODED (AFT WET AREA) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON TENSION STRAP AT AFT WET AREA RBL3 BS1026; BS1029. / [01] CORROSION ON TENSION STRAP AT AFT WET AREA RBL3 BS1026; BS1029 WITH NEXT DIMENSION L=3.00'' W=0.800 X= 0.010 OT=0.050 RT=0.040 WL 208 P/N 147A5744-1 WITH NEXT TOOL DEPTH GAGE ID:ATS2678 S/N:UNKNOWN DATE:04/2022 DUE:04/2023; FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G PAR 9C;[02] VERIFIED CORRECTIVE ACTION 1 COMPLETED AND VERIFIED OUT OF LIMITS;[03] REMOVED TENSION STRAP AT BS 989 TO 1029 RBL 11 WL 208 PER SRM 51-10-02.-;[04] RECIVED NEW TENSION STRAP ITEM 147A5744-1 LOT 1482052-6; LOCATED AND DRILLED NEW TENSION STRAP AT BS 989 TO 1029 RBL 11 WL 208; IAW 737-700 SRM 51-40-05-0G-0 DWG 147A5730 OK TO INTALL.;[05] RECIVED NEW TENSION STRAP ITEM 147A5744-1 LOT 1482052-6; LOCATED AND DRILLED NEW TENSION STRAP AT BS 989 TO 1029 RBL 3 WL 208; IAW 737-700 SRM 51-40-05-0G-0 DWG 147A5730 OK TO INTALL;[06] VERIFIED CORRECTIVE ACTION STEP 5. VERIFIED OK TO INSTALL.;[07] INSTALLED NEW TENSION STRAP AT BS 989 TO 1029 RBL 3 WL 208; IAW 737-700 SRM 51-40-02-0G-0; DWG 147A5600.;[08] REJECTION TO ITEM 7 IS AT STEP 1.;[09] CORRECTED ITEM 7: INSTALLED NEW TENSION STRAP AT BS 989 TO 1029 RBL 3 WL 208; IAW 737-700 SRM 51-40-02-0G-0; DWG 147A5600. REV:A; AND STEP 3 IS COMPLETED;[10] ITEM 9; CORRECTED STEP 1;[11] VERIFIED ITEMS 9;10 CORRECTIVE ACTIONS. <BR>VERIFIED STEP 1;[12] VERIFIED MEASUREMENT FIEL

Part: TENSION TIE — CORRODED (AFT WET AREA) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON TENSION STRAP AT AFT WET AREA LBL3 BS1016; BS1026. / [01] PARTIAL STEP 1 AND 2.;[02] VERIFIED CORRECTIVE ACTION 1 AND 2 PARTIAL AND VERIFIED OUT OF LIMITS;[03] REMOVED TENSION STRAP AT BS 989 TO 1026 RBL 11 WL 208 PER SRM 51-10-02.-;[04] RECIVED NEW TENSION STRAP P/N 147A5620-3; LOCATED AND DRILLED NEW TENSION STRAP AT BS 989 TO 1029 LBL 3 WL 208; IAW 737-700 SRM 51-40-05-0G-0 DWG 147A5600 OK TO INTALL.;[05] VERIFIED CORRECTIVE ACTION STEP 4. VERIFIED OK TO INSTALL.;[06] INSTALLED NEW TENSION STRAP AT BS 989 TO 1029 LBL 3 WL 208; IAW 737-700 . IAW 737-700 SRM 51-40-02-0G-0; DWG 147A5600.;[07] INSTALLED NEW TENSION STRAP AT BS 989 TO 1029 LBL 3 WL 208. IAW 737-700 SRM 51-40-02-0G-0; DWG 147A5600.;[08] REJECTION TO ITEM 7 AT STEP 3.;[09] INSTALLED NEW TENSION STRAP AT BS 989 TO 1029 LBL 3 WL 208. IAW 737-700 SRM 51-40-02-0G-0; DWG 147A5600 REV:H;[10] VERIFIED ITEM 9 CORRECTIVE ACTIONS.;[11] VERIFIED MEASUREMENT FIELD

Part: SIDEWALL SUPPORT — CORRODED (FWD CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY LBL23 BS400 - BS500D. / [01] REMOVED CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 23 WL 156 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.FABRICATED ; LOCATED AND DRILLED REPLACEMENT FLOOR TO SIDEWALL SUPPORT FCB BS 396 TO BS 500D LBL 23 WL 156 USING BAC1496-444#7075T62 LOT:1485395-1 IAW SRM 51-40-05-0G-0;; AND DWG 143A7501 REV: A. FABRICATED FLOOR TO SIDEWALL SUPPORT SPLICE REPAIR AT B/S BTW 480 -500 USING BAC1496-444#7075T62 LOT:1485395-1 IAW SRM 53-00-53-2R-6 AND SRM 51-40-05. APPLY CHEMICAL CONVERSION COATING AND PRIMER.;APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON FCB FLOOR TO SIDEWALL SUPPORT AT LBL 23WL 156; BS 396 TO BS 500D AND SPLICE BTW BS 480 AND BS 500 IAW SRM 51-20-01 AND AMM 51-21-72-370-804; INSTALLED SPLICE REPAIR AT SIDEWALL SUPPORT LBL 23 ; WL 156 ;BTW 480 TO 500 FCB L/H IAW SRM 53-00-53-2R-6 REPAIR 6 AND SRM 51-40-02;

Part: FLOOR SUPPORT — ELONGATED (FWD CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

FCB FLOOR SUPPORT HAS ELONGATED FASTENER HOLE BS492 RBL17 WL156. / [01] VERIFIED APPLICABILITY NO ALLOWABLE DAMAGE FOR THIS PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 PARA#9;[02] REMOVED FCB FLOOR SUPPORT HAS ELONGATED FASTENER HOLE BS492 RBL17 WL156. IAW SRM 51-40-02.;[03] FABRICATED FCB NEW FLOOR SUPPORT BS 492 RBL 17 WL 156 P/N BAC1505-100261#2024-T3511 EXTRUSION;LOT#5116161-1 PO#869316/1 IAW SRM 51-40-05 AND DWG 143A9405 REV:A.;[04] VERIFIED CORRECTIVE ACTION 1-3;[05] APPLIED CHEMICAL CONVERSION COATING AND PRIMER FCB FLOOR SUPPORT BS 492 RBL 17 WL 156 IAW SRM 51-20-01 AND AMM 51-21-72-370-804; OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION 1 OK TO INSTALL;[07] INSTALLED FCB NEW FLOOR SUPPORT BS 492 RBL 17 WL 156 IAW SRM 51-40-02 AND DWG I43A8330 REV:-;[08] VERIFIED CORRECTIVE ACTION STEP 7.;[09] TASK CARD COMPLETE.

Part: ATTACH ANGLE — CRACKED (FWD CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL25 WL155. / [01] REMOVED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL25 WL155 IAW SRM 51-40-02;[02] LOCATED AND DRILLED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL25 WL155. IAW SRM 51-40-05 AND DWG 143A7505 REV:B;OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION ITEMS 1 AND 2. OKAY TO INSTALL NEW ATTACH ANGLE GIVEN.;[04] INSTALLED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL25 WL155 IAW SRM 51-40-02 AND DWG 143A7505 REV:B;[05] VERIFIED CORRECTIVE ACTION STEP 4.;[06] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON FLOORBEAM AT AFT CABIN BS986 RBL5; LBL5. MARKED. / [01] REMOVED CORROSION FROM PASSENGER CABIN FLOOR BEAM BS 986 RBL 5; WL 208 IN AREA OF 1' X 1' X 0.08' DEEP ORIGINAL MATERIAL THICKNESS 0.150' FOUND TO BE OUT OF LIMIT IAW SRM 53-70-51-1A-1 DET. 4H; FIG 103-C TOOLS USED MICROMETER ID: ATS1671; S/N:65093024; DUE10/2022;[02] VERIFIED APPLICABILITY OF SRM 53-70-51-01-1 FOR IDENTIFICATION AND SRM 53-70-51-1A-1 FOR ALLOWABLE LIMIT;[03] PARTIALLY COMPLETED STEP 1 & 2;[04] VERIFIED CORRECTIVE ACTION 1; 2 COMPLETED AND PARTIAL FOR CORRECTIVE ACTION 3;[05] 'REFER TO FAULT TTG8Q00DQKNA WHERE EA 22-153-02234 WAS ADDED AS A SUBTASK. 'FAULT RESOLVED ON OTHER FAULT' REPAIR REFERENCE IS SELECTED.;[06] VERIFIED CORRECTIVE ACTION 5;[07] COMPLETED STEPS 1 AND 2;[08] UPDATED STEP 1AND 2 AS A PARTIAL STEP;[09] VERIFIED CORRECTIVE ACTION 5;6;7 COMPLETED

Part: CHANNEL — CORRODED (CABIN FLOOR) · airframe 59,880 hrs · 35,571 cycles

AFT L/H MOPSILL HAS CORROSION BS 947-996; LBL 45-50; WL 208 / [01] REMOVED CORROSION ON AFT SERVICE DOOR MOP SILL AT B.S. 947-996 LBL45-50 W.L 208.1 P/N 147A8540-7 ;AREA OT=0.080;RT=0.068 ;L=26.700'W=1.700'' ;X=0.012 WITH DEPTH GAGE ID:ATS2678<BR>S/N:UNKNOWN<BR>DATE:04/2022<BR>DUE:04/2023. FOUND TO BE OUT OF LIMITS I.A.W SRM 53-70-15-1A-1FOR ALLOWABLE DAMAGE AND SRM 53-70-15-0I-1 FOR IDENTIFICATION AND IT WILL REPAIRABLE BY REPLACEMENT I.A.W 51-10-02-0G PAR 9C .;[02] REMOVED AFT SERVICE DOOR MOP SILL AT B.S. 947-996 LBL45-50 W.L 208.1 P/N 147A8540-7 I.A.W SRM 51-40-02-0G-0.;[03] VERIFIED CORRECTIVE ACTION #1.;[04] RECIVED NEW MOP SEAL ITEM 147A8540-7 LOT 1497046; LOCATED AND DRILLED NEW MOP SEAL AT LBL45-50 BS 897 TO 1016 W.L 208.1 ; IAW 737-700 SRM 51-40-05-0G-0 DWG 147A8501 OK TO INTALL.;[05] VERIFIED CORRECTIVE ACTION 4; OK TO INSTALL GIVEN.;[06] VERIFIED MEASUREMENT TABLE.;[07] INSTALLED NEW L/H MOPSILL AT BS 910 TO 1016; LBL 45-50 WL 208 IAW SRM 51-40-02-0G-0; DWG 147A8501; 147A0000 CARD IS COMPLETED;[08] CORRECTED ITEM 7 : INSTALLED NEW L/H MOPSILL AT BS 910 TO 1016; LBL 45-50 WL 208 IAW SRM 51-40-02-0G-0; DWG 147A8501 REV:C; 147A0000 CARD IS COMPLETED;[09] UPDATED PART USED;[10] VERIFIED CORRECTIVE ACTION #8;[11] VERIFIED CORRECTIVE ACTION #8

Part: WEB — CORRODED (AFT CABIN) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON WEB AT AFT CABIN BS989 RBL37. / [01] CORROSION ON WEB AT AFT CABIN BS989 RBL37 WL 208 P/N 147A5744-14 WITH NEXT DIMENSION L=0.950'' W=0.800 X= 0.010 OT=0.050 RT=0.040 WITH NEXT TOOL DEPTH GAGE ID:ATS2678 S/N:UNKNOWN DATE:04/2022 DUE:04/2023; FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G PAR 9C;[02] VERIFIED CORRECTIVE ACTION 1 COMPLETED AND VERIFIED OUT OF LIMITS;[03] REMOVED WEB AT BS 989 TO 1016 RBL 11 WL 208 PER SRM 51-10-02.-;[04] RECIVED NEW WEB ITEM 147A5744-14 LOT 1485868 LOCATED AND DRILLED NEW WEB AT RBL 37 BS 989 TO 1016 WL 208.1 ; IAW 737-700 SRM 51-40-05-0G-0 DWG 147A5730.- OK TO INSTALL.-;[05] VERIFIED CORRECTIVE ACTION STEP 4. VERIFIED OK TO INSTALL.;[06] INSTALLED NEW WEB AT AFT CABIN BS 986 TO BS 1016 RBL 37 IAW SRM 51-40-02-0G-0 ADN DWG 147A5730 REV:C; CARD IS COMPLETED;[07] UPDATED PART USED;[08] VERIFIED CORRECTIVE ACTION #6 AND MEASUREMENT FIELD;[09] VERIFIED CORRECTIVE ACTION #6 AND MEASUREMENT FIELD

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767+8; BS767+12 RBL22. / [01] CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767+8; BS767+12 RBL22 ; FOUND TO BE OUT OF LIMITS DUE NO ALLOWABLE DAMAGE ON SRM ;PART WILL BE REPAIRED BY REMPLACEMENT IAW 51-10-02-0G-0 PAR 9 C;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] RECEIVED SHIELD P/N 146A8127-12 LOT: 1494181-1. LOCATED AND DRILLED NEW SHIELD IAW SRM 51-40-05-0G-0; AND DWG 146A008. THIS FAULT WILL BE ACCOMPLISHED ON AD CARD ID TTG8Q004E2GM;[04] CORRECTION STEP 3: RECEIVED SHIELD P/N 146A8127-12 LOT: 1494181-1. LOCATED AND DRILLED NEW SHIELD IAW SRM 51-40-05-0G-0; AND DWG 146A008.;[05] VERIFIED CORRECTIVE ACTIONS 3 AND 4.;[06] UPDATED MEASUREMENT FIELD; ITEM 12 CORRECTED FINAL Z AXIS STATION 2 INCREMENT TO 12'

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS914 RBL11. / [01] DAMAGE FOUND AT ACB WATER SERVICE PANEL SUPPORT ANGLE BS 914; RBL 11; FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9C;[02] REMOVED ACB SUPPORT ANGLE BEHIND WATER SERVICE PANEL BS 914 RBL 11 IAW SRM 51-4-02-0G-0;[03] RECEIVED NEW SUPPORT ANGLE P/N 147A7221Y32 LOT#1493584 LOCATED AND DRILLED AT BS 914 RBL 11 IAW SRM 51-40-05-0G-0 AND DWG#147A7221 REV-D OK TO INSTALL;[04] VERIFIED ACTION #1-3; OK TO INSTALL GIVEN;[05] INSTALLED SUPPORT ANGLE BEHIND WATER SERVICE PANEL BS 914 RBL 11 IAW SRM 51-40-02-0G-0 AND DWG#147A7221 REV-D;[06] VERIFIED CORRECTIVE ACTION STEP 5.;[07] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

Part: ATTACH ANGLE — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON ATTACH ANGLE AT AFT CARGO BAY BS807 RBL19. / [01] REMOVED ATTACH ANGLE AT AFT CARGO BAY BS807 RBL19 PER SRM 51-40-02;[02] RECEIVED; LOCATE AND DRILL ON ATTACH ANGLE AT AFT CARGO BAY BS807 RBL19 IAW 737-700 PER SRM 51-40-05 AND DWG 146A8120. OK TO INSTALL;[03] VERIFIED ITEM 2 CORRECTIVE ACTIONS. OK TO INSTALL.;[04] INSTALLED ATTACH ANGLE AT AFT CARGO BAY BS807 RBL19 IAW 737-700 PER SRM 51-40-02 AND DWG 146A8120;[05] VERIFIED CORRECTIVE ACTION #4 AND MEASUREMENT FIELD;[06] VERIFIED CORRECTIVE ACTION #4 AND MEASUREMENT FIELD

Part: FRAME — CRACKED · airframe 59,880 hrs · 35,571 cycles

BS 312 FRAME IS CRACKED AT STRINGER 5L / [01] REMOVED DAMAGE FROM FRAME BS 312 STR 5L; WL 283 IAW SRM 51-10-02-0G-0;[02] REMOVED DAMAGE FROM FRAME BS 312 STR 5L; WL 283 IAW SRM 53-10-07-2R-1 STEP 4C;[03] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 1 AND 2. HFEC INSPECTED TRIMMED EDGE OF DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND. TOOL N600 ATS1465 DUE 08/2023.;[04] ACCOMPLISHED PERMANENT REPAIR ON BS312 FRAME UPPER CHORD LBL33 S-5L AND S-6L REF. EA M-22-153-01244 TTG8Q00DVQFJ;[05] VERIFIED CORRECTIVE ACTION #4. VERIFIED MEASUREMENT TABLE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,880 hrs · 35,571 cycles

FLOOR SUPPORT IS CRACKED AT BS 284; BL 0; WL 208 / [01] VERIFIED APPLICABILITY AS PER SRM 53-10-51-1A-1 AFTER EVALUATION; DISCREPANCY WAS FOUND OUT OF LIMIT AS PER SRM 53-10-51-1A-1; STEP 4.B(1)A FIGURE 105; DETAIL A.<BR><BR>LOCATED AND DRILLED NEW INTERCOSTAL P/N: 141A5410-3; IAW SRM 51-40-02 AND DWG 141A5400;[02] VERIFIED CORRECTIVE ACTION 1; OK TO INSTALL SUPPORT.;[03] INSTALLED NEW INTERCOSTAL FLOOR SUPPORT AT BS 277 TO 294 BL 0 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A5400;[04] VERIFIED CORRECTIVE ACTION STEP 3.;[05] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

Part: ATTACH FITTING — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON FWD SHIELD ATTACH FITTING AT AFT CARGO BAY BS767 RBL23. / [01] REMOVED FWD SHIELD ATTACH FITTING AT AFT CARGO BAY BS767 RBL23.FOUND TO BE OUT LIMITS DUE NO ALLOWABLE DAMAGE ON SRM PART WILL REPLACEMENT PER SRM 51-40-02-0G-0 PARA 9C . RECEIVED NEW CLIP P /N 146A8125-39 LOT. 1484112-3 LOCATED AND DRILLED IAW SRM 51-40-05 DWG 146A1010.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; OK TO INSTALL NEW CLIP.;[03] INSTALLED ATTACH FITTING AT AFT CARGO BAY BS767 RBL23 IAW SRM 51-40-02 AND DWG 146A1010;[04] VERIFIED CORRECTIVE ACTION ITEM 3.;[05] VERIFIED MEASUREMENTS. VERIFIED FAULT COMPLETE

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON AFT SHIELD AT AFT CARGO BAY BS847 - BS867 RBL21. / [01] CORROSION ON AFT SHIELD AT AFT CARGO BAY BS847 - BS867 RBL21; FOUND TO BE OUT OF LIMITS DUE NO ALLOWABLE DAMAGE ON SRM; PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9 C.<BR><BR>RECEIVED NEW SHIELD P/N 146A8127-10 LOT:1496127-2; LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 146A0081.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] VERIFIED MEASUREMENT TABLE.;[04] CARD COMPLETE

Part: STRINGER CLIP — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS807 S-26R. / [01] REMOVED CLIP AT AFT CARGO BAY BS807 S-26R FOUND TO BE OUT LIMITS DUE NO ALLOWABLE DAMAGE ON SRM PART WILL REPLACEMENT PER SRM 51-40-02-0G-0 PARA 9C . RECEIVED NEW CLIP P /N 146A1010-27 LOT. 1487498. LOCATED AND DRILLED IAW SRM 51-40-05 DWG 146A1263.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; OK TO INSTALL NEW CLIP. MEASUREMENT FIELD RBL NEED VERIFIED.;[03] UPDATE MEASUREMENTS ITEM 2;4;[04] INSTALLED NEW CLIP P /N 146A1010-27 LOT. 1487498 I.A.W SRM 51-40-02-0G-0 AND DWG 146A1263.;[05] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 4.;[06] VERIFIED MEASUREMENT FIELDS ARE ACCURATE & COMPLETE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON FLOOR SUPPORT BS 309; LBL 12; WL 208 / [01] REMOVED CORROSION FROM INTERCOSTAL BS 309 LBL 12 WL 208 IN REA OF 1'X0.05'X0.491' DEEP FOUND TO BE OUT OF LIMIT IAW SRM 53-10-51-1A-1 DET.4E FIG 105-C <BR>TOOLS USED MICROMETER ID:ATS1617; S/N:65093024; DUE 10/2022;[02] INSPECTED AND VERIFIED CORRECTIVE ACTION 1.;[03] REMOVED FLOOR SUPPORT INTERCOSTAL AT BS 294.5 TO BS 312 LBL 12 WL 208 IAW SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW INTERCOSTAL FLOOR SUPPORT AT BS 294.5 TO BS 312 LBL 12 WL 208 IAW SRM 51-40-05-0G-0 AND DWG 141A5600; OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION 4; OK TO INSTALL GIVEN.;[06] REINSTALLED NEW INTERCOSTAL FLOOR SUPPORT AT BS 294.5 TO BS 312 LBL 12 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A5600 CARD IS COMPLETED.;[07] VERIFIED CORRECTIVE ACTION STEP 6.;[08] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS887+2; BS927+17 RBL21. / [01] VERIFIED APPLICABILITY OF SRM 53-60-53-01-2 FOR IDENTIFICATION AND SRM 53-60-15-1A-1 FOR ALLOWABLE DAMAGE;[02] CORRECTION STEP 1: VERIFIED APPLICABILITY OF SRM 53-70-53-01-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.;[03] VERIFIED PATIAL STEPS 1 AND 2 AND CORRECTIVE ACTION 2.;[04] FABRICATED; LOCATED AND DRILLED FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 887 TO BS 927 RBL; ITEM BAC1496-377 LOT. 1484618-1 IAW SRM 51-40-02-0G-0 DWG 147A7501 OK TO TREATMENT AND PRIMER IAW SRM 51-21-0G-0 AND SOPOM 20-41-02;[05] CORRECTIVE ACTION STEP 4: REFERNCE CORRECT IAW SRM 51-40-05 FOR LOCATED AND DRILLED;[06] VERIFIED CORRECTIVE ACTIONS #4 AND #5<BR> OK TO TREATMENT AND PRIME GIVEN;[07] UPDATED MEASUREMENTS ON TABLE ITEM 22: MINOR REPAIR;[08] VERIFIED CORRECTIVE ACTION #7;[09] APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01 AND AMM 51-21-72-370-804.;[10] VERIFIED CORRECTIVE ACTION #9;[11] REINSTALLED SPLICE ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BTW BS 883 TO 891 RBL 21 WL 156 IAW SRM 51-40-02 AND DWG 146A7501 REV:A.;[12] VERIFIED CORRECTIVE ACTION #11 AND MEASUREMENT FIELD;[13] VERIFIED CORRECTIVE ACTION #11 AND MEASUREMENT FIELD

Part: INTERCOSTAL — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS827+18 RBL6. / [01] REMOVED CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS827+18 RBL6 AT DISCREPANCY AREA BS.827+18 L=2.000' W=2.000' D= 0.023' ORIGINAL THCKNESS 0.045' REMAINING MAT 0.022 MAT LOSS 0.023 FONUD TO BE OUT OF LIMITS IAW SRM SRM 53-60-15-1A-1 USED TOOL ATS ID 1672 DUE 03/2023 VERIFIED SRM APPLICABILITY AND OUT OF LIMITS PER SRM 53-60-15-1A-1 STEP 4.C 2;[02] REMOVED INTERCOSTAL AT AFT CARGO BAY BS 827 TO 847 RBL6 IAW SRM 51-40-02;FORMED INTERCOSTAL; AT AFT CARGO BAY BS 827+18 RBL 16 WITH MATERIAL ( 7075 T0 # .045' ) LOT .1480084-1 IAW SRM 51-30-01-0G-0 DWG 146A8131;[05] VERIFIED CORRECTIVE ACTION STEP 4.;[06] LOCATED AND DRILL FORMED INTERCOSTAL; AT AFT CARGO BAY BS 827+18 RBL 16 WITH MATERIAL ( 7075 T0 # .045' ) LOT .1480084-1 IAW SRM 51-30-01-0G-0 DWG 146A8131 APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON FORMED INTERCOSTAL ; AT AFT CARGO BAY IAW SRM 53-60-15-1A-1;ALLOWABLE DAMAG 2 STEP 2B;C OK TO INTALL.;[09] VERIFIED ACTION #8; OK TO INSTALL GIVEN;[10] INSTALLED NEW INTERCOSTAL AT ACB BS27 - BS847; RBL16; WL154 PER DWG 146A8130 AND SRM 51-40-02-0G-0;[11] INSTALLED NEW INTERCOSTAL AT AFT CARGO BAY BS827 - BS847; RBL16; WL154 PER DWG 146A8130 AND SRM 51-40-02-0G-0;[12] UPDATED MEASUREMENT TABLE=PART NUMBER;[13] CORRECTION TO ACTION ITEM 8=APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON FORMED INTERCOSTAL ; AT AFT CARGO BAY IAW AMM 51-21-72-370-804 AND AMM 51-21-41-370-802 ;

Part: THRESHOLD WEB — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS796 - 827+3 RBL27. / [01] REMOVED CORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS796 - 827+3 RBL27 AT DISCREPANCY AREAS BS.827+3 FOUND TO BE OUT LIMITS L=1.700' W=0.600' D=0.020' REMAINING MAT 0.025 MAT LOSS 0.020' IAW SRM 53-60-15-1A-1 USED TOOL ID ATS1672 DUE 03/2023;[02] VERIFIED CORRECTIVE ACTION ITEM 1; MEASUREMENT FIELDS N/A'S INCORRECT.;[03] CORRECTION:MEASUSUREMENT 23-24;[04] RECIVED NEW SUBTHRESHOLD WEB ITEM 14146A8123-25 LOT1498664-1 LOCATED AND DRILLED NEW SUBTHRESHOLD WEB AT AFT CARGO BAY BS787 - 847 RBL27 ; IAW SRM 51-40-05-0G-0 DWG 146A8340 OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION ITEM 3-4; MEASUREMENT FIELD STILL INCORRECT; BUT OK TO INSTALL NEW PART.;[06] CORRECTIVED:MEASUREMENT ITEM #22;[07] MEASUREMENT FIELD 18 REMAINING THICKNESS IS .025' NOT .020'; ITEM 22 IS INCORRECT; THIS IS A 'MINOR' REPAIR NOT 'MAJOR'.;[08] CORRECTED MEASUREMENTS;[09] THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q004E2GM.-;[10] THIS PIECE WILL BE INSTALLED WITH THE CARD TTG8Q004E2GM;[11] INSTALLED ON CORRECTIVE ACTIONS 10;[12] VERIFIED MEASUREMENT TABLE AND CORRECTIVE ACTIONS INDICATING THE AFT CARGO BAY SUB THRESHOLD WILL BE INSTALLED ON FAULT# TTG8Q004E2GM

Part: FLOOR PANEL — PULLED (FWD FUSELAGE) · airframe 59,880 hrs · 35,571 cycles

FWD CABIN FLOOR PANEL 222DF HAS PULLED THROUGH INSERTS / [01] IDENTIFIED FWD CABIN FLOOR PANEL 222DF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2. 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 13 EACH INSERTS TO FACILITATE REPAIRS; REMOVED DAMAGED SKINS/CORE ON 2 EACH LOWER SURFACE OUTBOARD EDGE; AND CLEANED REPAIR AREA IAW SRM 53-00-50-2R-1 PARA 3.A-F.;[05] POTTING COMPOUND CURED SURFACE SANDED & CLEANED IAW SRM 53-00-50-2R-1 PARA 3 STEPS H; I; & J . PER GENERAL REPAIR SECTION 53-00-50-2R-0 ELEVATED TEMPERATURE CURE TABLE 203 PAGE 2 REF CAL TOOL THERMOMETER ID ATS1776 SN 34910031WS CAL DUE 08/2022 .;[06] USING BMS9-3 STYLE 1581 GLASS LOT 149322-1 & BMS8-201 TYPE III RESIN LOT AK2CP8139K FABRICATED & APPLIED REPAIR PLIES IAW SRM 53-00-50-2R-1 PARA 3 . K . (1) STEPS (A)-(C). OK TO LAY UP .;[07] VERIFIED CORRECTIVE ACTIONS 5 AND 6<BR><BR>OK TO LAY UP REPAIR PLIES;[08] LAID UP THE REPAIR VACUUM BAGGED ;LEAK CHECKED & SET TO CURE IAW SRM 53-00-50-2R-1 PARA 3 . L. STEPS (A)-(C).;[09] VERIFIED CORRECTIVE ACTION 8;[10] CURED THE REPAIR PLIES IAW SRM 53-00-50-2R-1 PARA 3 . M. (1) STEPS A & B.;[11] CALIBRATED TOOLS USED CORRECTIVE ACTION 10: THERMOMETER ID ATS1777<BR>SN 3491002WS CAL DUE 08/2022 . VACUUM GAGE ID ATS2438 SN UNK CAL DUE 03/2023.

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727+19 - BS767 RBL21. / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727+19 - BS767 RBL21. AT DISCREPANCY AREA BS.767 L=1;0' W=0.900';D=0.015' ORIG THICKNESS 0.040' REMAINING MAT 0.025' MAT LOSS 0.015' FOUN TO BE OUT LIMITS IAW 53-00-53-1A-2 USED TOOL ID ATS 1672 DUE 03/2023 VERIFIED APPLICABILITY OF SRM 53-60-53-01-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE;[02] VERIFIED DAMAGE WAS OUT OF LIMITS PER SRM 53-00-53-1A-2.<BR>CONFIRMED APPLICABILITY OF SRM 53-60-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.<BR>VERIFIED MEASUREMENT TABLE HAS BEEN COMPLETED.;[03] LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT (ZEE) P/N 146A7502-51 LOT: 1484607-1 IAW SRM 51-40-05 AND DWG 146A7502.;[04] VERIFIED CORRECTIVE ACTION STEP 3.;[05] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS867+9 RBL21. / [01] VERIFIED APPLICABILITY OF SRM 53-60-53-01-2 FOR IDENTIFICATION AND SRM 53-60-15-1A-1 FOR ALLOWABLE DAMAGE;[02] SRM FOR ALLOWABLE DAMAGE 53-00-53-1A-2;[03] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS867+9 EVALUATED AS FOLLOW: L=2' W=0.750' D=0.030; ORIGINAL THICKNESS 0.040' PER BAC1496-377. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4A (2) FIG 103 DETAIL D.<BR>USED TOOL ID ATS2739 S/N A22004232<BR>DUE 04/2023;[04] VERIFIED CORRECTIVE ACTIONS 1-3.;[05] FABRICATED; LOCATED AND DRILLED FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 867 TO BS 887 RBL 21; ITEM BAC1496-377 LOT. 1484618-1 IAW SRM 51-40-02-0G-0 DWG 146A7500. OK TO TREATMENT AND PRIMER IAW SRM 51-20-01-0G-0 AND SOPOM 20-41-02;[06] CORRECTIVE ACTION STEP 5: REFERNCE CORRECT IAW SRM 51-40-05 FOR LOCATED AND DRILLED;[07] VERIFIED CORRECTIVE ACTIONS #5 AND #6 OK TO TREATMENT AND PRIME GIVEN;[08] UPDATED MEASUREMENTS ON TABLE ITEM 22: MINOR REPAIR;[09] VERIFIED MEASUREMENT TABLE;[10] APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01 AND AMM 51-21-72-370-804.;[11] VERIFIED CORRECTIVE ACTION #10;[12] REINSTALLED SPLICE ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BTW BS 883 TO BS 891 RBL 21 WL 156 IAW SRM 51-40-02 AND DWG 146A7501 REV A.;[13] VERIFIED CORRECTIVE ACTION #12;[14] VERIFIED CORRECTIVE ACTION #12

Part: RAIL — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON RAIL AT AFT CARGO BAY BS767+6 LBL12. / [01] CORRODED SPLICE REPAIR ; ON UPPER FLANGE AT A JOGGLE; LOCATED AT AFT CARGO BAY BS 767 + 6 LBL12 NOT HAVE ENTRIES IN SRM BY ALLOWABLE DAMAGE MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 ITEM 9.C.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED SPLICE REPAIR LOCATED AT A JOGGLE AT AFT CARGO BAY BS 767 + 6 LBL12 IAW SRM 51-40-02. RECEIVED REPAIR CHANNEL WITH P/N: 53100004-001; LOT: 1469421; LOCATED AND DRILLED IAW. SRM 51-40-05-0G-0; SRM 53-00-53-2R-2 REPAIR 2 PARAG. 4.I.(5).& DWG# 53100004. OK TO INSTALL;[04] VERIFIED ITEM 3 CORRECTIVE ACTIONS. OK TO INSTALL.;[05] INSTALLED ACB FLOOR RAIL SPLICE ANGLE AT JOGGLE BS 767 + 6 LBL.12 IAW SRM 53-00-53-2R-2 REPAIR 2;[06] VERIFIED CORRECTIVE ACTION ITEM 5.;[07] VERIFIED MEASUREMENTS. FAULT COMPLETE.

Part: TRACK — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON TRACK AT AFT CARGO BAY RBL13 BS727+10 - BS727B; BS727D; BS787; BS787+12. / [01] REMOVED MULTIPLE CORROSION AREAS ON THE TIE DOWN TRACK FROM BS 727+10 - BS787+12 RBL 13 IAW SRM 51-10-02. MAX. MATERIAL REMOVED IN AREA OF 1.3'X0.9'X0.04'DEPTH FROM AN ORIGINAL THICHNESS 0'071' . REMIANING THICHNESS 0.031' ( OR 56% MATERIAL REMOVED) WHICH IS OUT OF LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2. THE STRUCTURAL ITEM WILL BE REPAIRED BY REPLACEMENT FROM BS 727+4 - BS 867 PER SRM 53-00-53-2R-3 REPAIR 3 AND PER DWG#146A7500 ON CUSTOMER CARD# 727855 FUSELAGE 5170 OR TTG8Q00DQ58Z;[02] CORRECTIVE ITEM 1 ABOVE. SHOULD BE ON CUSTOMER CARD# 727855 FUSELAGE 5174 OR TTG8Q00DQ58Z;[03] VERIFIED AFT CARGO TIE-DOWN TRACK AT RBL13 WILL BE REPLACED ON FAULT #TTG8Q00DQ58Z- NO FURTHER ACTION REQUIRED.

Part: TIE DOWN — CRACKED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CRACKED TRACK AT AFT CARGO BAY BS727E RBL13. / [01] CARGO TIE DOWN TRACK CRACKED AT BS 727 E RBL 13 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2. THE STRUCTURAL ITEM TO BE REPAIRED BY REPLACEMENT PER SRM 53-00-53-2R-3 REPAIR 3 AND PER DWG#146A7500;[02] VERIFIED CORRECTIVE ACTION 1.;[03] LOCATED AND DRILLED NEW CARGO TIE DOWN TRACK (KIT# 654A0004-1350) AND SPLILCE ANGLE PN# 146A7506-20; PO# 863815 FROM BS 727+4 TO BS 887 RBL 13.8 IAW SRM 51-40-05; IAW SRM 53-00-53-2R-3 REPAIR 3 AND IAW DWG# 146A7500.... OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTION 3. OK TO INSTALL TIE-DOWN TRACK.;[05] INSTALLED CARGO TIE DOWN TRACK FROM BS 727+4 TO BS 887 RBL 13.8 IAW SRM 51-40-05; IAW SRM 53-00-53-2R-3 REPAIR 3 AND IAW DWG# 146A7500;[06] VERIFIED CORRECTIVE ACTION 5.;[07] WORKSCOPE COMPLETE.

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 59,880 hrs · 35,571 cycles

FWD CABIN FLOOR PANEL 221BF IS BROKEN ON THE AFT O/B END / [01] IDENTIFIED FLOOR PANEL 221BF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. DAMAGE IS REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>REMOVED DAMAGED INSERTS; AND INSERTS IN THE REPAIR AREA IAW SRM 53-00-50-2R-1 PARAGRAPH 3.B<BR><BR>REMOVED A 2.5' X 17.5' AREA OF DELAMINATED CRACKED LOWER SKIN ONLY; AND REMOVED LOOSE PIECES OF CORE; AND CLEANED AREA. NO CONTAMINATION NOTED. OKAY TO APPLY POTTING TO EXPOSED CORE CELLS IAW SRM 53-00-50-2R-1 PARAGRAPH 3A.C-F.;FABRICATED REPAIR PLIES USING BMS9-3 ST1581 LOT#1493221-1 ALL IAW SRM 53-00-50-2R-1 PAR.3 H-K(1)(A)08] INSTALLED REPAIR PLIES WITH BMS8-201 LOT#AK2CP8139K AND VACUUM BAGGED; LEAK CHECKED GOOD USING VACUUM GAUGE ID:ATS2107 CAL DUE 09/2022 AND SET REPAIR TO CURE IAW SRM 53-00-50-2R-1 PARAGRAPH 3.K(1)(B-C)L(1).;[10] CURED REPAIR PLIES USING THERMOMETER ID: ATS2208 CAL DUE: 10/2022. REMOVED VACUUM BAG AND TRIMMED REPAIR EDGES AND CLEANED IAW SRM 53-00-50-2R-1 PARAGRAPH M(1).[13] INSTALLED ALL PREVIOUSLY REMOVED INSERTS USING BMS5-107 LOT# AK1KP9159K IAW SRM 53-00-50-2R-1 PARAGRAPH 3.N; AND FOR INSERT IDENTIFICATION BAC DWG 141A5810 ID:0056.[15] FWD CABIN FLOOR PANEL 221BF WITH DAMAGE AT THE AFT O/B END WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BAC DWG 141A5810 ID:0056.

Part: CHANNEL — CORRODED (FWD SERVICE DOOR) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON FSD MOPSILL AT BS 312-315; 324; AND 333 RBL 59; WL 208 / [01] PARTIAL STEP 1-3.;[02] COMPLETED STEPS 1; 2 AND 3. VERIFIED CORROSION REMOVAL AND OUT OF LIMITS.;[03] REMOVED MOPSILL AT BS 260 TO BS 360 RBL 59 WL 208 IAW SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW MOPSILL AT BS 260 TO BS 360 RBL 59 WL 208 IAW SRM 51-40-05-0G-0 AND DWG 141A8310; OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION 4; OK TO INSTALL GIVEN.;[06] INSTALLED NEW MOPSILL FROM BS 260 TO BS 360 RBL 59 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A8310; CARD IS COMPLETED;[07] VERIFIED MEASUREMENT TABLE.;[08] VERIFIED CORRECTIVE ACTION 6.;[09] VERIFIED TASK CARD COMPLETE.

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS918 RBL11. / [01] DAMAGE FOUND AT ACB WATER SERVICE PANEL SUPPORT ANGLE BS 918; RBL 11; FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9C;[02] REMOVED ACB SUPPORT ANGLE BEHIND WATER SERVICE PANEL BS 918 RBL 11 IAW SRM 51-4-02-0G-0;[03] RECEIVED NEW SUPPORT ANGLE P/N 147A7221Y32 LOT#1493584 LOCATED AND DRILLED AT BS 918; RBL 11 IAW SRM 51-40-05-0G-0 AND DWG#147A7221 REV-D OK TO INSTALL;[04] VERIFIED ACTION #1-3; OK TO INSTALL GIVEN;[05] INSTALLED SUPPORT ANGLE BEHIND WATER SERVICE PANEL BS 918 RBL 11 IAW SRM 51-40-02-0G-0 AND DWG#147A7221 REV-D;[06] VERIFIED CORRECTIVE ACTION STEP 5;[07] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

Part: STRINGER CLIP — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS767 S-26R. / [01] CORROSION ON CLIP AT AFT CARGO BAY BS767 S-26R FOUND TO BE OUT LIMITS DUE NO ALLOWABLE DAMAGE ON SRM PART WILL REPLACEMENT PER SRM 51-40-02-0G-0 PARA 9C;[02] REMOVED CLIP AT AFT CARGO BAY BS767 S-26R P/N 146A1010-90 I.A.W SRM 51-40-02-0G-0.;[03] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 1.;[04] FABRICATED ; DRILLED AND APPLIED CHEMICAL CONVERSION COATING ON NEW CLIP AT AFT CARGO BAY BS767 S-26R P/N 146A1010-90 WITH NEXT MATERIAL BAC1493-856#7075T62 LOT 5062963-1 I.A.W SRM 51-40-05-0G-0 ;SRM 51-20-01-0G-0 AND DWG 146A1010 AND OK TO PRIME.;[05] VERIFIED ACTION #4; OK TO PRIME GIVEN;[06] APPLIED OF BMS 10-11; TYPE I PRIMER TO THE SURFACE OF THE REWORKED AREA. REFER TO SOPM 20-41-02. AND OK TO INSTALL.;[07] VERIFIED ACTION #6; OK TO INSTALL GIVEN;[08] INSTALLED NEW CLIP AT AFT CARGO BAY BS767 S-26R I.A.W SRM 51-40-02-0G-0 AND DWG 146A1261.;[09] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 8.;[10] VERIFIED MEASUREMENT FIELDS ARE ACCURATE & COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY LBL21 BS727B+10; BS727C+10; BS727C+14; BS727D+6; BS727E+2; BS727E+10; BS747 - BS787. / REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY LBL 21 BS 727B+10 REMOVED CORROSION EVALUATED AS FOLLOW L=1' W=0.750' D=0.010'; ORIGINAL THICKNESS 0.040' PER BAC 1496-377 ; BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 4A FIG 103 DETAIL D. TOOL USED ID ATS 1672<BR>S/N 65092939 DUE 03/2023;[05] CORRECTION STEP 2: FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS847 PREVIOUSLY REMOVED BY AD ID:TTG8Q004E2GMFABRICATED; LOCATED AND DRILLED REPLACEMENT FLOOR TO SIDEWALL SUPPORT ACB BS727 TO BS847 LBL 21 USING BAC1496-377 #7075T62 LOT:1494598-1 IAW SRM 51-40-05-0G-0 AND DWG 146A7502.FABRICATED FLOOR TO SIDEWALL SUPPORT SPLICE REPAIR AT BS BTW 727E - 747 USING BAC1496-377#7075 T62 LOT:1494598-1 IAW SRM 53-00-53-2R-6 AND SRM 51-40-05. APPLY CHEMICAL CONVERSION COATING AND PRIMER;[07] VERIFIED SIDEWALL SUPPORT ZEE CHANNEL AT BS 727 TO BS 847 LBL 21 IS BEING REPLACED AND INCORPORATING THE SPLICE REPAIR FROM SRM 53-00-53-2R-6INSTALLED SPLICE REPAIR AT SIDEWALL SUPPORT LBL 21 BTW BS 727E TO BS747 ACB L/H IAW SRM 53-00-53-2R-6 AND SRM 51-40-02. INSTALLATION FLOOR TO SIDEWALL SUPPORT WILL BE ACCOMPLISHED WITH THE CUSTOMER CARD # TTG8Q004E2GM

Part: RAIL — CORRODED (AFT CARGO FLOOR) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON RAIL AT AFT CARGO BAY BS727D+6; BS767+6 LBL3. / [01] [1]REMOVED (2EA) NUTS PLATE FOR ACCESS IAW SRM 51-40-02. REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS 727D+ 6 LBL 3 IAW SRM 51-10-02-0G-0 MEASURE: L= 2.' X W= .8' X D= 0.003' REWORKED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53-1A-2 [2]CORRODED SPLICE REPAIR ; ON UPPER FLANGE AT A JOGGLE; LOCATED AT AFT CARGO BAY BS 767 + 6 LBL3. NOT HAVE ENTRIES ALLOWABLE DAMAGE IN SRM MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 ITEM 9.C.;[03] REMOVED SPLICE REPAIR LOCATED AT A JOGGLE AT AFT CARGO BAY BS 767 + 6 LBL.3 IAW SRM 51-40-02. RECEIVED REPAIR CHANNEL WITH P/N: 53100004-001; LOT: 1469421; [05] INSTALLED ACB FLOOR RAIL SPLICE ANGLE AT JOGGLE BS 767 + 6 LBL.3 IAW SRM 53-00-53-2R-2 REPAIR 2;;[11] [2]CORRODED SPLICE REPAIR ; ON UPPER FLANGE AT A JOGGLE; LOCATED AT AFT CARGO BAY BS 767 + 6 LBL3. NOT HAVE ENTRIES ALLOWABLE DAMAGE IN SRM MUST BE REPAIR BY REPLACEMENT IAW SRM 53-00-53-2R-2 REPAIR 2 PARAG. 4.I.(5).;[12] THE ITEM#1 STEP[2] WAS EDITED AND CORRECTED BY ITEM 11; THE STRUCTURAL REPAIR WAS DONE WITH SRM 53-00-53-2R-2 REPAIR 2 AND NOT SRM 51-10-02 [14] VERIFIED CORROSION AT BS727D+6 LBL3 WAS IN LIMITS AND REWORK AREA WAS RETORED IN STEP 1. VERIFIED CORROSION AT BS767+6 LBL3 WAS OUT OF LIMITS AND REPAIRED PER SRM 53-00-53-2R-2 REPAIR 2.

Part: RAIL — CORRODED (AFT CARGO FLOOR) · airframe 59,880 hrs · 35,571 cycles

CORROSION ON RAIL AT AFT CARGO BAY BS727C+7; BS767+6 LBL8. / [01] [1]REMOVED (1EA) NUTS PLATE FOR ACCESS IAW SRM 51-40-02. REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS 727C+ 7 LBL 8 IAW SRM 51-10-02-0G-0 MEASURE: L= 1.5' X W= .9' X D= 0.003' REWORKED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 PARAG. 4.A.(2) DETAIL E (B-B) FIG.103 SHEET 3.<BR> USED TOOL: DEPTH GAGE :<BR> ID: ATS1738.<BR> S/N: UNKNOWN.<BR> DUE DATE:09/2022. OK TO TREAT AND PRIME.<BR>[2]CORRODED SPLICE REPAIR ; ON UPPER FLANGE AT A JOGGLE; LOCATED AT AFT CARGO BAY BS 767 + 6 LBL3. NOT HAVE ENTRIES ALLOWABLE DAMAGE IN SRM MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 ITEM 9.C.;[03] REMOVED SPLICE REPAIR LOCATED AT A JOGGLE AT AFT CARGO BAY BS 767 + 6 LBL.8 IAW SRM 51-40-02. RECEIVED REPAIR CHANNEL WITH P/N: 53100004-001; LOT: 1469421; INSTALLED ACB FLOOR RAIL SPLICE ANGLE AT JOGGLE BS 767 + 6 LBL.8 IAW SRM 53-00-53-2R-2 REPAIR 2;[06] STEP #(1) THE STRUCTURAL REPAIR WAS DONE WITH SRM 53-00-53-2R-2 REPAIR 2 AND NOT SRM 51-10-02<BR>THE ITEMS #5;6;7. COMPLETED. ALL MAINTENANCE ACTION ARE COMPLETED REQUEST FINAL BUYOFF.;[11] VERIFIED RII INSPECTION REQUIREMENTS WERE MET.;[12] VERIFIED CORROSION AT BS727C+7 LBL8 WAS REWORKED WITHIN LIMITS AND RESTORED PER SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 PARAG. 4.A.(2) DETAIL E (B-B) FIG.103 SHEET 3 . VERIFIED CORROSION AT BS767+6 LBL8 HAD NO ALLOWABLE LIMITS AND WAS REPAIRED PER SRM 53-00-53-2R-2 REPAIR 2. WORKSCOPE COMPLETE.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 59,880 hrs · 35,571 cycles

PANEL 193CL HAS A DELAMINATED DENT ON THE EXTERNAL SKIN / [01] IDENTIFIED PANEL 193CL MATERIAL ACCORDING TO SRM 53-40-70-0I-4; FIG. 2; TABLE 2; ITEM 9. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1; PARA'S 2.D AND 4.A.(6); AND FIG. 102. AREAS TO BE REPAIRED ACCORDING TO SRM 51-70-05-2R-2; AS REQUIRED BY SRM 53-40-70-2R-1; PARA'S 2; 4.B.(1); AND TABLE 201. STRIPPED SURFACE FINISHES IN REPAIR AREA; REMOVED DELAMINATED PLIES TO A REGULAR SHAPE; TAP TESTED AREAS (NO DISBONDS NOTED); REMOVED CONTAMINANTS FROM REPAIR AREA; ALL ACCORDING TO SRM 51-70-05-2R-2; PARA'S 4.A THRU 4.C.[04] APPLIED BMS 5-28; TY 7 POTTING COMPOUND TO EXPOSED CORE (LOT# AK1AP8072K); CURED APPLIED POTTING COMPOUND; SANDED POTTING COMPOUND FLUSH WITH THE SURROUNDING AREAS; CLEANED ALL REPAIR AREAS; THEN FABRICATED REPAIR PLIES FROM BMS 8-79; ST 1581 FIBERGLASS (LOT# 1495932-1); AND BMS 5-129; GR 05 ADHESIVE (LOT# 1494556-1); ALL ACCORDING TO SRM 51-70-05-2R-2; PARA. 4.D.; AND SRM 51-70-05;2R-11; PARA'S 4.A THRU 4.D. REQUEST OK TO LAYUP.13] ACCOMPLISHED UT POST REPAIR INSPECTION OF REPAIR AREA NO DISBONDS NOTED IAW 737 NDTM PART 4; 51-00-02 TOOL# ATS843 CAL. DUE 06/2023.

Part: PANEL — DELAMINATED (RH WING) · airframe 59,880 hrs · 35,571 cycles

RT WING L/E PANEL 621NB HAS DELAMINATION AT BOTH L/E CORNERS / REMOVED DAMAGE FROM BOTH SIDES OF PANEL MEASURING 5.5'X2.4; 4.5'X4.5'; 4'X2'; AND 4.5X2'; RE-CLEANED; WITH NO CONTAMINATION NOTED IAW SRM 51-70-05-2R-6 PAR.4 A-D;[02] VALIDATED APPLICABILITY OF REPAIR TO BE COMPLETED IAW SRM 51-70-05-2R-6. FABRICATED REPAIR PLIES USING BMS5-129TY2 GR05 LOT#1497185-1; BMS8-79CL3ST1581 LOT#1490485-1; AND BMS8-79CL3ST120 LOT#1493863-1 IAW SRM 51-70-05-2R-6 PAR.4 E; INSTALLED REPAIR PLIES AND VACUUM BAGGED IAW SRM 51-70-05-2R-6 PARA 4.E&F.CURED REPAIR PLIES USING HOT BONDER ID:ATS532 DUE:06/2023; REMOVED VACUUM BAG MATERIALS; LIGHTLY SANDED FLUSH; AND CLEANED AREA OF REPAIR IAW SRM 51-70-05-2R-6 PAR.4 F-G;[08] VERIFIED CORRECTIVE ACTIONS 4-7FABRICATED ALUMINUM FOIL PLY USING BMS 8-289 LOT#1484605-1 INSTALLED AND CURED USING BMS 5-128 LOT#JH1LAR7523. VACUUM BAGGED; LEAK CHECK GOOD USING VACUUM GAUGE ID:E11543 DUE:09/2022 AND THERMOMETER ID:ATS2208 DUE:10/2022 IAW SRM 51-70-14-2R-3 PARA 4.A.3-7 & 11 (A-J).;[12] UNBAGGED ALUMINUM FOIL REPAIR; AND TRIMMED EXCESS MATERIAL IAW SRM 51-70-14-2R-3 PAR.4 A(11)(L)APPLIED FINAL FINISH IAW AMM 51-21-71-370-801 PAR.3 D(1-4;7A); AMM 51-21-99-300-802 PAR.3 C(1); AND SRM 51-70-05-2R-6 PAR.4 RT WING L/E PANEL 621NB WITH DELAMINATION AT BOTH L/E CORNERS HAS BEEN REPAIRED IAW SRM 51-70-05-2R-6

Part: SKIN — CRACKED (LH HOR STAB) · airframe 59,880 hrs · 35,571 cycles

LH HORIZONTAL STABILIZER LWR SKIN HAS 1/2' CRACK AT STA 193.9 18' FROM FWD EDGE. / TRIMMED OUT THE DAMAGED PART OF THE SKIN AT DISCREPANCY AREA; CUT OUT DIMENSIONS 1.7' X 1.0' IAW SRM 55-10-01-2R-11;[03] HFEC REQUEST AT THE EDGES OF THE CUT OUT AND OPEN HOLES TO ENSURE NO CRACKS EXIST.;[04] HFEC INSPECTED THE TRIMMED EDGE OF THE DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND. TOOL N600 ATS2353 DUE 01/2023.;[05] VERIFIED CORRECTIVE ACTION 2 DAMAGE REMOVAL;[06] HFEC REQUEST AT OPEN HOLES TO ENSURE NO CRACKS EXIST.;[07] HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16. NO CRACKS NOTED. EQUIP USED: -NORTEC 600 ID: ATS2353 CAL DUE: 01/23 -MINIMITE ID: IS000934 CAL DUE: 08/22;[08] FABRICATED REPAIR PARTS (1)- DOUBLER 2024 T3 CLAD 0.080' LOT# 1466259-1 AND (2)- FILLER 2024 T3 CLAD 0.063' LOT# 1497220-1 APPLIED CHEMICAL CONVERSION COATING IAW SRM 55-10-01-2R-11 OK TO PRIME.;[09] VERIFIED ITEM 8 CORRECTIVE ACTIONS.;[10] APPLIED PRIMER TO REPAIR PARTS AND COMMON AREA IAW SRM 55-10-01-2R-11 OK TO INSTALL.;[11] VERIFIED ITEM 10 CORRECTIVE ACTIONS. OK TO INSTALL.;[12] INSTALLED REPAIR PARTS AT LH HORIZONTAL STABILIZER LWR SKIN AT STA 193.9 IAW SRM 55-10-01-2R-11;REVIEWED MXI FOLLOW ON CATEGORY B DEFERRAL REQUIREMENTS IS ESTABLISHED

Part: SUPPORT BRACKET — CRACKED · airframe 59,880 hrs · 35,571 cycles

CRACK ON L/H DUCT SUPPORT BRACKET AT BS 540+2 LBL 7.(ACCESS FROM 192CL. MARKED) / [01] REMOVED & REPLACED BRACKET ASSY P/N 212A1116-1; LOT: 1486702-1; LOCATED AT LEFT ECS BAY BTW. BS.540.4 WL 165.98 LBL 8 IAW SRM 51-40-02-0G-0; DWG#212A1110 REV:C;[02] VERIFIED CORRECTIVE ACTION 1.;[03] VERIFIED MEASUREMENT TABLE; WORKSCOPE COMPLETE.

Part: WEB — CRACKED (RH WING) · airframe 59,880 hrs · 35,571 cycles

CRACK ON R/H SEAL WEB TO DEFLECTION CONTROL RIB O/B BRACKET ATTACH ANGLE.(MARKED) / [01] FOUND NO APPLICABLE SRM REPAIR FOR CRACKED RT WING T/E SEAL WEB TO DEFLECTION CONTROL RIB ATTACH ANGLE; THEREFORE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9. REMOVED AND REPLACED CRACKED ANGLE PER SRM 51-40-02-0G-0 PARAGRAPH 4. VERIFIED FASTENER CALLOUT PER AIPC 57-42-51-02 ITEM NO. 16.;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.

Part: SUPPORT ANGLE — CRACKED (LH WING) · airframe 59,880 hrs · 35,571 cycles

LEFT WING UPPER T/E PANEL SEAL SUPPORT ANGLE IS CRACKED AT RSS 270 / [01] FOUND NO APPLICABLE SRM REPAIR FOR CRACKED LT WING T/E UPPER PANEL SEAL SUPPORT ANGLE AT RSS 270; THEREFORE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9. REMOVED AND REPLACED CRACKED ANGLE PER SRM 51-40-02-0G-0 PARAGRAPH 4. VERIFIED INSTALLATION FASTENER CALLOUT PER AIPC 57-50-00-25 ITEM 199.;[02] VERIFIED CORRECTIVE ACTIONS STEP 1. VERIFIED MEASUREMENTS TABLE.

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 59,880 hrs · 35,571 cycles

FWD SERVICE DOOR #4 BEAM HAS CRACK IN INSPECTION AREA AS DEFINED IN TASK 52-41-EG-SWA-001 FIG 1. / [01] FWD SERVICE DOOR #4 BEAM WAS REPLACED ON WORK ORDER: 551501; CUSTOMER RO# P3723631-1 WHICH IS ATTACHED DIGITALLY TO IMAGES ON THIS NRC.;[02] VERIFIED

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,880 hrs · 35,571 cycles

FSD CUTOUT; FWD FRAME; UPPER HINGE BOX FTG CRACKED (MARKED) / [01] CUTOUT CRACK FROM UPPER HINGE BOX FITTING IN THE FWD FRAME OF THE FSD CUTOUT. DAMAGE REMOVAL AREA MEASURES .1' X .4'. DAMAGE REMOVED PER SRM 51-10-02-0G-0.;[02] AFTER DVI; CRACK NOTED ON INBOARD SURFACE AT DAMAGE REMOVAL/CUT OUT AREA.;[03] CUTOUT ADDITIONAL MATERIAL FROM BLEND AREA ON UPPER HINGE BOX FITTING IN THE FWD FRAME OF FSD CUTOUT PER SRM 51-10-02-0G-0. DAMAGE REMOVAL AREA NOW MEASURES: .5' X .7'.;[04] VERIFIED CORRECTIVE ACTION 3.;[05] HFEC INSPECTED CUTOUT AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23. NO CRACKS NOTED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23;[06] REPAIRED UPPER HINGE BOX FITTING PER EA 22-153-02281;[07] REPAIRED UPPER HINGE BOX FITTING PER EA 22-153-02281

Part: LIGHT — INOPERATIVE · airframe 59,444 hrs · 35,291 cycles

EMERGENCY LIGHT ROW 6 RIGHT SIDE INOP. / [01] RELAMPED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 6 RIGHT SIDE PER AMM 33-51-03. OPS CK GOOD

Part: SLIDE — LOW (FWD ENTRY DOOR) · airframe 59,167 hrs · 35,119 cycles

FWD ENTRY DOOR SLIDE PRESSURE LOW / [01] REPLACED SLIDE PER AMM 25-66-01 AND MT 725-61-06

Part: LIGHT — LOOSE (L2 DOOR) · airframe 58,781 hrs · 34,869 cycles

EMERGENCY EXIT LIGHT COVER FELL OFF; NEAR AFT F/A JUMPSEAT / [01] R&R?D L2 DOOR EMERGENCY EXIT DESIGNATOR LIGHT ASSY AND OPS CHECKED GOOD IN REF TO M/M 33-51-01

Part: SUPPORT FRAME — CRACKED (WING) · airframe 58,772 hrs · 34,863 cycles

1.30' CRACK IN WING-TO-BODY FAIRING SUPPORT FRAME AT BS 500D; RBR 60; WL 192; MARKED IN BLACK. / [01] REMOVED R/H WTB PANEL 195AR AND 191AR IAW B737 AMM 53-51-21-000-803<BR><BR>REMOVED LOWER FAIRING SUPPORT AT STA 500D RBR60 WL 192 FOR PANELS 191AR AND 191FR IAW B737 SRM 51-40-02-0G-0<BR><BR>REMOVED MIDDLE FAIRING SUPPORT AT STA 500D RBR60 WL 192 FOR PANELS 191AR AND 195AR IAW B737 SRM 51-40-02-0G-0;[02] VERIFIED P/N 116A3118-10; ATAG BT2623 IAW B737 BOEING DRAWING 116A3110 REV -;[03] LOCATED AND DRILLED NEW P/N 116A3118-10 IAW B737 BOEING DRAWING 116A3110 REV - AND B737 SRM 51-40-05-0G-0 FIG 4; 5 AND 8;[04] INSPECTION CW STEPS 1;2 AND 3;[05] OK TO INSTALL;[06] BEGAN INSTALLING NEW SUPPORT FRAME IAW B737 BOEING DRAWING 116A3110 REV - AND B737 SRM 51-40-02-0G-0;[07] INSPECTION CW STEP 6;[08] FINISHED INSTALLING NEW SUPPORT FRAME IAW SRM 51-40-02-0G-0 AND DWG116AR3110 REV -. NEED OK TO INSTALL WTB PANEL 191AR AND 195 AR.;[09] VERIFIED STEP 8 AND OK TO INSTALL ACCESS PANELS;[10] INSTALLED WTB PANEL 191 AR AND 195 AR IAW AMM 53-51-21-400-803.;[11] VERIFIED ITEM 10.<BR>AUDITED.

Part: WEB — CRACKED (R/H WING) · airframe 58,772 hrs · 34,863 cycles

RIGHT WING TRAILING; WBL 201.90; FIXED TRAILING EDGE PANEL SUPPORT WEB CRACKED AT LOWER FASTENER HOLE. DOT 234/11 / [01] REMOVED CRACKED PANEL SUPPORT WEB IAW SRM 51-40-02-0G-0.;[02] VERIFY NEW PART AS PART NUMBER 115A2982-10 A-TAG: A64812 IAW IPC 57-50-00-25.;[03] VERIFIED STEP 1;2;[04] LOCATED;DRILLED AND INSTALLED NEW SUPPORT WEB IAW SRM 51-40-05-0G-0;SRM 51-40-02-0G-0 AND IPC 57-50-00-25.;[05] VERIFIED STEP 4<BR>C/W

Part: FLAP — DELAMINATED (R/H WING) · airframe 58,772 hrs · 34,863 cycles

RH OUTBD AFT FLAP INBD CORNER DELAMINATED / [01] EVALUATED R/H OUTBD AFT FLAP INBD CORNER AND FOUND AREA OF DELAMINATION OF 5'X6'.FOUND TO BE REPAIRABLE. IAW B737-700 SRM 57-53-01-2R-4 PAR1A REV 75. REMOVED DAMAGED SKIN FOR REPAIR. NO DAMAGE TO CORE. CLEAN AND PREP FOR REPAIR. IAW B737-700 SRM 51-70-10-2R-0. PAR 6;7;8&9. REV75. APPLIED BO-GEL AND ADHESIVE PRIMER. IAW B737-700 SRM 51-70-10-2R-0 PAR 14&15.(A111068);(A45722). NEED OK TO BOND.;[02] VERIFIED PRIMER THICKNESS IAW SRM 51-70-10-2R-0. FOUND TO BE IN LIMITS. TOOL#21860; DUE 22SEP22.;[03] OK TO INSTALL REPAIR;[04] BONDED REPAIR DOUBLER'S. IAW B737-700 SRM 51-70-10-2R-0 PAR 18;20&21. TAP TEST GOOD.(A80169) 7075-T6-.025.(A54056) 7075-T6-.020.(A68274) FILM ADHESIVE. NEED OK TO APPLY DECORATIVE FINISH.;[05] VERIFIED ITEM 4; OK TO PRIME AND PAINT;[06] APPLIED DECORATIVE FINISH. IAW B737 AMM 51-21-99-300-801 REV 76 (A79762);(A99201).;[07] REPAIRED AREA OF DELAMINATION ON RIGHT WING O/B AFT FLAP INBD CORNER. IAW B737-700 SRM 57-53-01-2R-4; SRM 51-70-10-2R-4; SRM 51-70-10-2R-0; AMM 51-21-99-300-801.;[08] VERIFIED STEP 6;7<BR>C/W

Part: SKIN — DELAMINATED (LH WING TE FLAP) · airframe 58,772 hrs · 34,863 cycles

LH OUTBD AFT FLAP INBD CORNER LOWER SKIN DELAMINATED / [01] REMOVED LH OUTBOARD AFT FLAP ASSEMBLY IAW AMM 27-51-22-000-801.;[02] OK TO INSTALL NEW LH OTBD AFT FLAP;[03] INSTALLED NEW LH OUTBOARD AFT FLAP ASSEMBLY IAW AMM 27-51-22-400-801 STEPS 3.F.(1) THRU 3.F.(5)(G). TW #AAR39120 DUE 05/07/2022. ADJUSTMENT CHECK REQUIRED.;[04] VERIFIED STEP 3;[05] COMPLETED INSTALLATION OF LH OUTBOARD AFT FLAP ASSEMBLY IAW AMM 27-51-22-400-801 STEPS 3.G.(1) THRU 3.H.(2). ADJUSTMENT CHECK GOOD. ALL RIG PINS REMOVED.;[06] VERIFIED STEP 5;[07] C/W

Part: SKIN — ELONGATED (R/H WING) · airframe 58,772 hrs · 34,863 cycles

RIGHT WING TRAILING EDGE PANEL 651GB INBOARD FASTENER HOLES ELONGATED IN COMPOSITE SKIN. DOT 234/12. / [01] WORK ACCOMPLISHED ON NON-ROUTINE TTG8Q00B1K45 (43253/6000/0023)

Part: SHIELD — CRACKED (#2 PYLON) · airframe 58,772 hrs · 34,863 cycles

NO.2 PYLON STRUT FAIRING INTERNAL SUPPORT RIB NO. 5 (CASTING)PN 313A2752-2 CRACKED AT FASTENER HOLES. DOT 234/05. / [01] DISPLACED INBD AND OUTBD BLADE SEALS FOR F.O.M IAW ARM 51-40-02-0G-0;[02] REMOVED AFT FITTING MOUNT FOR F.O.M IAW ARM 51-40-02-0G-0;[03] REMOVED LOWER HEAT SHIELD PLATE FOR F.O.M IAW ARM 51-40-02-0G-0;[04] REMOVED LOWER EDGE PLATE FOR F.O.M IAW ARM 51-40-02-0G-0;[05] REMOVED #2 PYLON STRUT FAIRING INTERNAL CRACKED SUPPORT RIB IAW SRM 51-40-02-0G-0;[06] VERIFIED NEW SUPPORT RIB P/N 7540234 MPN 313A2752Y2 ATAG WN8021 IAW BOEING DWG 313A2752 REV A;[07] STARTED LOCATEING AND DRILLING NEW SUPPORT RIB IAW BOEING DWG 313A2752 REV A;[08] CERTIFIED STEP 6;[09] VERIFIED STEPS 1 THRU 8;[10] COMPLETED LOCATING AND DRILLING OF NEW SUPPORT RIB FOR #2 PYLON IAW SRM 51-40-05-0G-O ALSO SRM 51-40-02-0G-0 ;BOEING DRW 313A2752 REV:A;[11] INSPECTION CW STEP 10;[12] APPLIED ONE COAT OF TYPE III PRIMER ON NEW SUPPORT RIB IAW BOEING DWG 313A2752-2;[13] INSPECTION CW STEP 12;[14] OK TO INSTALL RIB;[15] STARTED INSTALLING RIB IAW BOEING DWG 313A2752 REV A SRM 51-40-02-0G-0;[16] VERIFIED STEP 15;[17] OK TO CLOSE INBD SIDE PNL OF #2 PYLON;[18] STEP 17 OK TO CLOSE GRANTED;[19] OK TO INSTALL LOWER HEAT SHIELD PLATE AND AFT FITTING MOUNT ON TO #2 PYLON;[20] STEP 19 OK TO CLOSE GRANTED;[21] INSTALLED INBD SIDE PNL ; LOWER HEAT SHIELD PLATE;AND AFT FITTING IAW SRM 51-40-02-0G-0 ALSO BOEING DWG 313A2400 REV A;

Part: FITTING — ELONGATED (R/H WING) · airframe 58,772 hrs · 34,863 cycles

RIGHT WING TRAILING EDGE PANEL 651GB FORWARD ADJUSTMENT ROD UPPER CLEVIS ATTACH POINT TEE FITTING HOLE ELONGATED. DOT 234/11 / [01] REMOVED AND REPLACED ELONGATED TEE FITTING WITH PN 115A2350-1 ATAG# A117187 IAW BOEING DWG 115A5300 SHT 6 REV- AND SRM 51-40-02-0G-0.;[02] VERIFIED TASK COMPLETE<BR><BR>AUDIT COMPLETE

Part: ANGLE — CRACKED (CENTER WING) · airframe 58,772 hrs · 34,863 cycles

CRACK FOUND IN A/C BAY UPPER ATTACH ANGLE AT STA 663 RBL 8 / [01] REMOVED FASTNERS AND CUT OUT DAMAGED PORTION OF ANGLE AS SHOWN IN SRM 57-10-10-2R FIG. 202.;[02] PREFORMED A DVI OF REPAIR AREA. NO DEFECTS NOTED IAW SRM 57-10-10-2R.;[03] MATERIAL VERIFIED FOR -1 REPLACEMENT ANGLE FABED IN BACK SHOP ON W/O 43255-6000-0002 AND -2 SPLICE ANGLE FABED ON BACK SHOP W/O 43255-6000-0001 IAW SRM 57-10-10-2R TABLE 201.;[04] VERIFIEF STEPS1;2;3[10] BEGAN INSTALLING -1 AND -2 REPAIR PARTS. FASTENERS COMMON TO THE FUEL TANK INSTALLED AND CAP SEALED INSIDE THE TANK I/A/W B737 SRM 57-10-10-2R-5 REPAIR 5.;[11] INSPECTION CW STEP 10;[12] COMPLETED INSTALLING -1 AND -2 REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5.;[13] CAP SEALED; AND FILLET SEALED REPAIR AND APPLIED CIC TO REPAIR AREA AS REQUIRED IAW SRM 57-10-10-2R-5 REPAIR 5 STEPS 4L- 4O.;[14] INSPECTION CW STEPS 12 AND 13.;[15] RII REQUIREMENTS C/W;[16] AUDIT CW

Part: LENS — LOOSE (CABIN) · airframe 58,285 hrs · 34,564 cycles

SUPPLEMENTAL INFORMATION: ILLUMINATED EXIT SIGN AT RIGHT OVER WING EXIT FELL OFF ; / [01] REINSTALLED EXIT SIGN LENS PER SIP

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 58,160 hrs · 34,487 cycles

SUPPLEMENTAL INFORMATION: RT HORZ. STAB; UPPER FWD SLIDER CRACKED ; RT HORZ. STA; PPER FWD SLIDER CRACKED / [01] REMOVED AND REPLACED RT HORN STAB UPPER SLIDE SEAL REF MM 53-31-31

Part: SLIDE — LOW (L1 DOOR) · airframe 57,879 hrs · 34,307 cycles

ESCAPE SLIDE AT DOOR 1L PRESSURE INDICATING BELOW GREEN BAND ; ESCAPE SLIDE AT DOOR 1R PRESSURE INDICATING BELOW GREEN BAND. / [01] REMOVED AND REPLACED R-! ESCAPE SLIDE PER MT 725-61-06-FS

Part: PANEL — ELONGATED (FUSELAGE) · airframe 57,696 hrs · 34,199 cycles

SUPPLEMENTAL INFORMATION: SEVERAL ELONGATED HOLES ON PANEL 193B ; / [01] REMOVED AND REPLACED WORN 193B PANEL PER AMM 53-21-21.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 57,567 hrs · 34,127 cycles

AFT SERVICE DOOR ECAPE SLIDE FELL OUT OF BUSTLE. ; / [01] REINSTALLED AFT SERVICE DOOR SLIDE PER MT 725-61-06.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 56,400 hrs · 33,441 cycles

LEFT FWD ENTRY SLIDE CAME LOOSE IN ITS CONTAINER ; / RESCURED SLIDE IN CONTAINER PER MT 725-61-06

Part: INTERCOSTAL — CRACKED (BS 500-500A) · airframe 54,635 hrs · 32,397 cycles

CRACK WEB - INTERCOSTAL BS500 TO BS500A STR 26L AT FWD CARGO COMPARTMENT (1 EA) / REPLACED WEB-INTERCOSTAL BS 500D TO BS 500D STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG # 143A7505 REV -

Part: INTERCOSTAL — CORRODED (BS 867-887) · airframe 54,635 hrs · 32,397 cycles

CORROSION WEB - INTERCOSTAL LOC BTW BS 867 TO BS 887 AND BTW S-26L TO 27L AT AFT CARGO COMPARTMENT WL 156.5 / AS DOCUMENTED ON NRC L174465. DETAILED DAMAGE REMOVAL INSPECTION NAD REPAIR INSTRUCTION WERE ACCOMPLISHED PER EA 20-153-013-24.

Part: SEAT TRACK — DETERIORATED (COCKPIT) · airframe 54,635 hrs · 32,397 cycles

DETERIORATED SEAT TRACK FIRST OFFICER SEAT AFT POSITIONS INBORD AND OUTBORD AT COCKPIT (2 EA) / REPLACED SEAT TRACK FIRST OFFICER SEAT AFT POSITIONS INBOARD AND OUTBOARD AT COCKPIT IAW B737-700 AMM 25-11-11-400-801

Part: SEAT TRACK — DETERIORATED (COCKPIT) · airframe 54,635 hrs · 32,397 cycles

DETERIORATED SEAT TRACK CAPTAIN SEAT AFT POSITIONS INBORD AND OUTBORD AT COCKPIT (2 EA) / REPLACED SEAT TRACK CAPTAIN SEAT AFT POSITION INBOARD AND OUTBOARD AT COCKPIT (2EA) IAW B737-700 AMM 25-11-11-400-801

Part: WEB — CORRODED (BS 787-807) · airframe 54,635 hrs · 32,397 cycles

CORROSION BILGE AREA ON WEB LOCATED BTW BS 787 TO BS 807 STR 27R AND RBL3.00 AT AFT CARGO COMPARTMENT WL 156.5 / REPLACED WEB LOCATED BETWEEN BS 787 TO BS 807 STR 27R AND RBL 3.00 WL 156.5 AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 PARAGRAPH 9 AND DRAWING #146A8130 SHEET 12 REV. B

Part: WEB — CORRODED (BS 767-787) · airframe 54,635 hrs · 32,397 cycles

CORROSION FLOOR STRUCTURE WEB LOCATED BTW BS 767 TO BS 787 AT LEVEL OFSTR 25R AND RBL 21.00 AT AFT CARGO COMPARTMENT WL 156.5 / REPLACED WEB LOCATED BETWEEN BST 767 TO BST 787 AT LEVEL OF STR 25 RH AND RBL 21.00 AT AFT CARGO COMPARTMENT WL 156.5 IAW SRM B737-700 51-10-02; 51-40-02 AND DRAWING #146A0081 REV.

Part: SUPPORT — CRACKED (BS 727-847) · airframe 54,635 hrs · 32,397 cycles

CRACK SUPPORT ZEE LOCATED BTW BS727 TO BS847 AT LEVEL STR25L AND LBL 21.00 AFT CARGO COMPARTMENT / REPLACED SUPPORT ZEE LOCATED BTW B727 TO BS847 AT LEVEL STR25L AND LBL 21.00 AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02;53-00-53-2R-6 REPAIR 6 AND DWG'S 146A7502 REV A 140N4500

Part: CHANNEL — CORRODED (BS 420-440) · airframe 54,635 hrs · 32,397 cycles

CORROSION CHANNEL SIDEPLATE LOCATED BETWEEN BS420 TO BS440; RBL21 AND WL156.5 AT FWD CARGO COMPARTMENT WL 156.5 / REPLACED CHANNEL SIDE PLATE LOC BTW BS420 TO BS440 RBL21 AND WL156.59 AT FWD CARGO COMPARTMENT WL156.5 IAW B737-700 SRM 51-10-02-0G-0 AND DRAWING #143A0080 REV

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 54,635 hrs · 32,397 cycles

CORROSION CHANNEL SIDEPLATE LOCATED BETWEEN BS492.4 TO BS500A; RBL21 AND WL156.5 AT FWD CARGO COMPARTMENT WL 156.5 / REPLACED CHANNEL SIDEPLATE LOC BTW BS492.4 TO BS500A; RBL21 AND WL156.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 AND DWG 146A0081-9 REV C

Part: SUPPORT ANGLE — CRACKED (BS 500B) · airframe 54,635 hrs · 32,397 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS500B AFT FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED ANGLE- SUPPORT LOC. ON BS500B AFT FACE AND STR.26L FWD CARGO COMPARTMENT IAW SRM B737-700 51-40-02 DWG #143A7505 REV.B

Part: SUPPORT ANGLE — CRACKED (BS 460) · airframe 54,635 hrs · 32,397 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS460 AFT FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED ANGLE SUPPORT LOC ON BS 460 AFT FACE AND SW 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 DWG #143A7505 REV A

Part: SUPPORT ANGLE — CRACKED (BS 480) · airframe 54,635 hrs · 32,397 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS480 FWD FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED ANGLE-SUPPORT ; AND FASTENERS LOC. BS480 FWD FACE AND STR.26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 DWG#143A7505 REV.-

Part: SUPPORT ANGLE — CRACKED (BS 500C) · airframe 54,635 hrs · 32,397 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS500C FWD FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED ANGLE - SUPPORT LOC ON BS500C FWD FACE AND STR.26L FWD CARGO COMP IAW B737-700 SRM 51-40-02 AND DWG #143A7505 REV.-

Part: STRAP — CORRODED (BS 430) · airframe 54,635 hrs · 32,397 cycles

CORROSION STRAP LOCATED BETWEEN BS430; RBL21 TO LBL21 AND WL 156.5 AT FWD CARGO COMPARTMENT WL 156.5 / REPLACED STRAP LOC BTW BS430;RBL21 TO LBL21 AND WL 156.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02

Part: SUPPORT ANGLE — CRACKED (BS 500A) · airframe 54,635 hrs · 32,397 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS500A FWD FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED SUPPORT ANGLE LOC ON BS 500A FWD FACE AND STR26L FWD CARGO COMPART IAW B737-700 SRM 51-40-02 DWG #143A7502-159 REV A

Part: SUPPORT ANGLE — CRACKED (BS 500B) · airframe 54,635 hrs · 32,397 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS500B FWD FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED NAGLE-SUPPORT LOC ON VS500B FWD FACE STR STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 DWG # 143A7505 REV B

Part: SUPPORT ANGLE — CRACKED (BS 500B) · airframe 54,635 hrs · 32,397 cycles

CRACKED SUPPORT ANGLE BS 500B FWD FACE AND STRINGER 26R FWD CARGO COMPARTMENT. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 1143A7505, REV B.

Part: CARGO TRACK — CRACKED (BS 747) · airframe 54,635 hrs · 32,397 cycles

CRACKED CARGO TRACK BS 747, STRINGER 26R AND RBL 13.84 IN THE AFT CARGO COMPARTMENT. PERFORMED A REPAIR TO THE CARGO TRACK IAW SRM 53-0053-2R-3, REPAIR 3, ALTERNATIVE 1-2, AND DRAWING 146A7500, REV.A.

Part: SUPPORT ANGLE — CRACKED (BS 500C) · airframe 54,635 hrs · 32,397 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS500C AFT FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED ANGLE - SUPPORT LOC. ON BS500C AFT FACE STR.26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-42-02 DWG #143A7505 REV.A

Part: STRAP — CORRODED (BS 767-787) · airframe 54,635 hrs · 32,397 cycles

CORROSION STRAP LOC BST 768 TO 787 AT AFT CARGO COMPARTMENT (1 EA) WL 156.5 AND BTW STR 25LH TO STR 25RH / REPLACED STRAP LOC BTW BS 768 TO BS787 WL156.5 AND BTW STR 25LH TO STR 25RH AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 AND DRAWING #146A9401 REV D

Part: CARGO TRACK — CRACKED (BS 767) · airframe 54,635 hrs · 32,397 cycles

CRACKED CARGO TRACK, BS 767, RBL 13.84 IN THE AFT CARGO COMPARTAMENT. PERFORMED A REPAIR TO THE CARGO TRACK LOCATED BETWEEN BS 727E TO 787, RBL 13.84 IAW SRM 53-00-53-2R-3, REPAIR 3, ALTERNATIVE 1-2, AND DRAWING 146A7500, REV AL

Part: SEAT TRACK — GOUGED (BS 520) · airframe 54,635 hrs · 32,397 cycles

GOUGE SEAT TRACK BS 520, LBL 24.75 AT PASSENGER CABIN. PERFORMED REPAIR SEAT TRACK BETWEEN BS 500C TO BS 520 LBL 24.75 AT PASSENGER CABIN IAW SRM 53-00-52-2R-4, REPAIR 4.

Part: STRINGER — CRACKED (BS 896) · airframe 54,635 hrs · 32,397 cycles

CRACKED STRINGER 25L, BS 896 IN THE AFT CARGO COMPARTMENT. REPAIRED THE STRINGER BETWEEN BS 896 TO 907 +10 IAW SRM 53-00-03-2R-1, REPAIR 1. PERMANENT REPAIR.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 54,635 hrs · 32,397 cycles

GOUGE SEAT TRACK STA 520 AT LBL 45.5 AT PASSENGER CABIN / PERFORMED REPAIR SEAT TRACK BETWEEN BS 500C TO BS 520 LBL 45.5 AT PASSENGER CABIN IAW SRM B737-700 53-00-52-2R-4 REPAIR 4

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 54,635 hrs · 32,397 cycles

CRACK GUSSET LOCATED ON BS500D AND STR19 LH FWD CARGO COMPARTMENT / REPLACED GUSSET LOC; BS500D AND STR.19LH FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DWG 143A7902

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 54,635 hrs · 32,397 cycles

CRACK GUSSET LOCATED ON BS500D AND STR19 RH FWD CARGO COMPARTMENT / REPLACED GUSSET LOC BS 500D AND STR19RH FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DWG 143A7902

Part: LIGHT — DETERIORATED (CABIN) · airframe 54,635 hrs · 32,397 cycles

DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT RH SIDE (5EA) AT PASSENGER CABIN (5 EA) / REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT RH SIDE AT PASSENGER CABIN IAW DWG 33500007

Part: LIGHT — DETERIORATED (CABIN) · airframe 54,635 hrs · 32,397 cycles

DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT LT SIDE (5 EA) AT PASSENGER CABIN (5EA) / REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT LT SIDE AT PASSENGER CABIN IAW DWG 33500007

Part: SCUFF PLATE — CRACKED (CARGO BAY) · airframe 54,635 hrs · 32,397 cycles

CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT (1EA) / REPAIRED BY WELDS AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30- 15-2R-1; REPAIR 1 PARAGRAPH 4.B STEP (4) AND BAC 5975

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 54,635 hrs · 32,397 cycles

CRACK FLOOR PANEL 120AF AT FWD CARGO COMPARTMENT (1 EA) / FABRICATED NEW FLOOR PANEL 120AF AT FWD CARGO COMPARTMENT (1EA) WITH NEW PANEL FABRICATED FROM 0.090' CONOLITE PO 2016 552348 IAW B737-700 AMM 25-52-01-201-801 AND DWG 453A161D SHEET 3 REV D

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,635 hrs · 32,397 cycles

CRACK LEADING EDGE RIB ACCESS PANEL 331B LOC. LE STA 78.29 AT LT HORIZONTAL STABILIZER (1 EA) / REPLACED LEADING EDGE RIB ON ACCESS PANEL 331B LOC. LE STA 78.29 AT LT HORIZONTAL STABILIZER(1EA)IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 186A1001 REV A

Part: RIB — CRACKED (HORIZONTA STAB) · airframe 54,635 hrs · 32,397 cycles

CRACK LEADING EDGE RIB ACCESS PANEL 331B LOC. LE STA 105.26 AT LT HORIZONTAL STABILIZER (1 EA) / REPLACED RIB AND FASTENER LOC.STA 105.26 AT LT HORIZONTAL STABILIZER(1EA)IAW B737-700 SRM 51-40- 02;51-10-02 ITEM 9 AND DWG 186A1304 REV

Part: RING — MISSING (L1 DOOR GIRT BAR) · airframe 52,526 hrs · 31,074 cycles

L1 DOOR SLIDE GIRT BAR RETAINING RING MISSING. / INSTALLED RING PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,529 hrs · 30,427 cycles

EMERGENCY LIGHT JUST BEHIND FWD SERVICE DOOR INOP. RELAMPED IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 49,515 hrs · 29,191 cycles

RT OVERWING EXIT EMERGENCY LIGHT FAILED CAPACITY CHECK. R&R BATTERY PACK PER AMM.

Part: CHARGER — FAULTY (CABIN) · airframe 48,881 hrs · 28,759 cycles

LT EMERGENCY LIGHTS IN COCKPIT GALLEY FAULTY BETWEEN ROW 1 TO ROW 3. R&R CHARGER PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,881 hrs · 28,759 cycles

LT EMERGENCY LIGHTS IN COCKPIT GALLEY FAULTY BETWEEN ROW 1 TO ROW 3. R&R BATTERY PACK PER AMM.

Part: WEB — CRACKED (RT WING) · airframe 48,798 hrs · 28,703 cycles

R/H DEFLECTION RIB PANEL WEB ANGLE CRACKED AT ORSS 271 / REMOVED DAMAGED WEB ANGLE + INSTALLED NEW WEB ANGLE PO# 699694 PER BOEING DWG 115A2930 + SRM 51-40-02-0G-0

Part: BRACKET — CRACKED (LT WING) · airframe 48,798 hrs · 28,703 cycles

LT WING UPPER PANEL BETWEEN NR 5 AND NR 6 SPOILER WEB OUTBOARD ANGLE BRACKET CRACKED. REMOVED BRACKET IAW SRM & DWG.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 48,798 hrs · 28,703 cycles

EXIT INDICATOR LIGHT L1188 CONNECTOR D0366 DAMAGED. R&R CONNECTOR IAW WDM & AMM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 48,798 hrs · 28,703 cycles

AFT CARGO COMPARTMENT FWD CORNER SCUFF PLATE IS CRACKED / REMOVED AND REPLACED AFT CARGO COMPARTMENT FWD CORNER SCUFF PLATE IAW B737 A.M.M- 53-11-02. SCUFF PLATE TO BE INSTALED ON ITEM 753-721-10-01.

Part: PRESSURE PANEL — DEFECTIVE (RT MLG WW) · airframe 48,798 hrs · 28,703 cycles

RT WHEEL WELL VERTICAL PRESSURE WEB DEFECTIVE AT RBL 25+9. REPAIRED WEB IAW SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 48,798 hrs · 28,703 cycles

AFT CARGO COMPARTMENT AFT CORNER SCUFF PLATE IS CRACKED / REMOVED AND REPLACED AFT CARGO COMPARTMENT AFT CORNER SCUFF PLATE IAW B737 A.M.M 53-11-02. SCUFF PLATE TO BE INSTALLED ON ITEM 753-721-10-01.

Part: DOUBLER — BROKEN (FWD FUSELAGE) · airframe 48,798 hrs · 28,703 cycles

EXTERNAL POWER DOOR CUTOUT LOWER AFT CORNER BROKEN / REMOVED DAMAGE AT EXTERNAL POWER DOOR CUTOUT LOWER AFT CORNER IAW SRM 53-10-15-2R-4; TREATED AREA IAW AMM 51-21-41-370-802; PRIMED AREA IAW AMM 51-21-72-370-804. 81146U 8/30/18

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,309 hrs · 28,394 cycles

L1 DOOR OF FIRST TWO CABIN EMERGENCY LIGHTS INOP. R&R BATTERY PACK IAW AMM.

Part: RETAINER — BROKEN (R1 GIRT BAR) · airframe 47,310 hrs · 27,761 cycles

R1 DOOR SLIDE GIRT BAR QUICK ATTACH COUPLER BROKEN. INSTALLED A NEW GIRT BAR RETAINER IAW AMM.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR SLIDE) · airframe 47,198 hrs · 27,690 cycles

R1 DOOR SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED THE GIRT BAR IAW MM.

Part: LENS — DISTORTED (CABIN) · airframe 46,489 hrs · 27,263 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS DISTORTED. R&R LENS PER AMM.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 46,297 hrs · 27,139 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF POSITON. REPOSITIONED GIRT BAR IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 45,408 hrs · 26,575 cycles

MID CABIN OH EXIT SIGN HOUSING BROKEN. R&R SIGN PER MM.

Part: SKIN — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FASTENER HOLE AT HORIZ STAB STA 170.30 AFT OF SKIN L/E (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; AND BOEING DRWG# 002A0001

Part: SKIN — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FADTENER HOLE AT HORIZ STAB STA 129.50 APPROX 34' AFT OF SKIN L/E (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; CCO 55-10-0014; AND BOEING DRWG 002A0001

Part: SKIN — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FASTNER HOLE AT HORIZ STAB STA 109.10 APPOX 43.5' AFT OF SKIN L\E (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; CCO 55-10-0014; AND BOEING DRWG #002A0001.

Part: SUPPORT ANGLE — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FASTENER HOLE AT HORIZ STAB STA 138.70 APPROX 30' AFT OF SKIN L/E (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; CCO 55- 10-0014; AND BOEING DRWG #002A0001.

Part: SKIN — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FASTENER HOLE AT HORIZ STAB STA 166.30 APPROX 34' AFT OF SKIN L/E (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; CCO 55-10-0014; AND BOEING DRWG# 002A0001

Part: SKIN — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FASTENER HOLE AT HORIZ STAB STA 149.50 REAR SPAR (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; CCO 55-10-0014; AND BOEING DRWG# 002A0001

Part: SKIN — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FASTENER HOLE AT HORIZ STAB STA 129.50 APPOX 33' AFT OF SKIN L\E (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; CCO 55-10-0014; AND BOEING DRWG #002A0001.

Part: SKIN — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FASTNER HOLE AT HORIZ STAB STA 130.50 APPROX 1' AFT OF SKIN L\E (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; CCO 55-10-0014; AND BOEING DRAWING #002A0001.

Part: SKIN — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FASTENER HOLE AT HORIZ STAB STA 157.10 APPROX 7' AFT OF SKIN L/E (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; CCO 55-10-0014; AND BOEING DRWG #002A0001

Part: SKIN — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FASTENER HOLE AT HORIZ STAB STA 166.30 APPROX 26.5' AFT OF SKIN L/E (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; CCO 55-10-0014; AND BOEING DRWG #002A0001

Part: SKIN — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FASTENER HOLE AT HORIZ STAB STA 147.90 APPROX 6' AFT OF SKIN L/E (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; CCO 55-10-0014; AND BOEING DRWG #002A001

Part: SKIN — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FASTENER HOLE AT HORIZ STAB STA 166.30 APPROX 36' AFT OF SKIN L/E (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; CCO 55-10-0014; AND BOEING DRWG# 002A0001

Part: SKIN — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FASTENER HOLE AT HORIZ STAB STA 160.10 AT FWD SPAR (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; CCO 55-10-0014; AND BOEING DRWG# 002A0001.

Part: SKIN — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FASTENER HOLE AT HORIZ STAB STA 157.10 APPROX 29.5' AFT OF SKIN L/E (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; CCO 55-10-0014; AND BOEING DRWG# 002A0001.

Part: SKIN — ELONGATED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

R/H HORIZ STAB HAS ELONGATED FASTENER HOLE AT HORIZ STAB STA 166.30 APPROX 33' AFT OF SKIN L/E (LOWER SKIN) / OVERSIZED HOLE TO 7/32' PER SRM 51-40-02; CCO 55-10-0014; AND BOEING #002A0001.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 120.30, NR 4 VERTICAL STIFFENER. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 120.30, NR 3 VERTICAL STIFFENER. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.70, NR 2 VERTICAL STIFFENER. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.70, 1ST RIB STIFFENER FROM FORWARD. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.70, NR 3 VERTICAL STIFFER. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 120.30, NR 2 STIFFENER. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 129.5, 2ND STIFFENER FROM FORWARD. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 45,314 hrs · 26,523 cycles

RT HORIZONTAL STAB RIB CRACKED AT STA 129.5, 3RD VERTICAL STIFFENER FROM FORWARD. REPAIRED RIB PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,297 hrs · 25,922 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 43,794 hrs · 25,611 cycles

R1 DOOR SLIDE GIRT BAR BRACKET LOOSE. SECURED THE BRACKET IAW MM.

Part: LENS — MISSING (CABIN) · airframe 43,328 hrs · 25,315 cycles

RIGHT OVERWING EXIT LIGHT LENS MISSING. R & R LIGHT ASSY IAW MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR GIRT BAR) · airframe 42,680 hrs · 24,943 cycles

L2 DOOR SLIDE GIRT BAR OUT OF ADJUST. R & R SLIDE IAW MT.

Part: ANGLE — CRACKED (BS 500C) · airframe 42,325 hrs · 24,718 cycles

FORWARD CARGO BAY ANGLE CRACKED AT BS 500C, STRINGER 25R. R & R THE ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (BS 947) · airframe 42,325 hrs · 24,718 cycles

AFT CARGO BAY SUPPORT ANGLE CRACKED AT BS 947, STRINGER 26L. R & R THE SUPPORT ANGLE IAW SRM & DWG.

Part: BAFFLE — CRACKED (BS 927-947) · airframe 42,325 hrs · 24,718 cycles

AFT CARGO BAY BAFFLE CRACKED BETWEEN BS 927 TO 947, RBL 20. R & R THE BAFFLET IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 500D-520) · airframe 42,325 hrs · 24,718 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 500D - 520, BL 0. REPAIRED THE FLOOR SUPPORT IAW SRM AND DWG.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 42,325 hrs · 24,718 cycles

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

Part: CREASE BEAM — CRACKED (BS 302) · airframe 42,325 hrs · 24,718 cycles

L1 INNER CREASE BEAM CRACKED AT BS 302.9. R & R THE CREASE BEAM IAW DWG AND SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 42,325 hrs · 24,718 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED. R & R THE GIRT BAR FITTING IAW DWG AND SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 42,325 hrs · 24,718 cycles

L1 DOOR INNER THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 312 - 344. REPAIRED THE SUPPORT ANGLE IAW AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,325 hrs · 24,718 cycles

PASSENGER CABIN AFT WET AREA FLOORBEAM T-CAP CORRODED AT BS 986.5, LBL 42. R & R T-CAP IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,325 hrs · 24,718 cycles

INTERCOSTAL CORRODED BETWEEN BS 294.5 TO BS 312, RBL 11. R & R INTERCOSTAL IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,325 hrs · 24,718 cycles

PASSENGER CABIN AFT WET AREA FLOORBEAM T-CAP CORRODED AT BS 986.5, BETWEEN RBL 11 TO RBL 37. R & R T-CAP IAW SRM & EA.

Part: CREASE BEAM — CORRODED (BS 330 - 344) · airframe 42,325 hrs · 24,718 cycles

R1 DOOR CUTOUT CREASE BEAM INNER ANGLE CORRODED BETWEEN BS 330 TO 344. R & R THE ANGLE IAW SRM.

Part: ATTACH ANGLE — DAMAGED (SCUFF PLATE) · airframe 42,325 hrs · 24,718 cycles

L1 DOOR FORWARD SCUFF PLATE ATTACH ANGLE DAMAGED. R & R THE ATTACH ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (BS 827) · airframe 42,325 hrs · 24,718 cycles

FRAME WEB CRACKED AT BS 827, BETWEEN STRINGERS 8 - 9R. REPAIRED FRAME IAW ER.

Part: FRAME — CRACKED (BS 360) · airframe 42,325 hrs · 24,718 cycles

FRAME WEB CRACKED AT BS 360, BETWEEN STRINGERS 8 - 9R. REPAIRED THE FRAME IAW ER AND EA.

Part: FRAME — CRACKED (BS 727D) · airframe 42,325 hrs · 24,718 cycles

FRAME WEB CRACKED AT BS 727D, BETWEEN STRINGERS 8 - 9R. REPAIRED FRAME IAW ER.

Part: SUPPORT ANGLE — CORRODED (R1 DOORWAY) · airframe 42,325 hrs · 24,718 cycles

R1 DOOR CUTOUT LOWER THRESHOLD SUPPORT ANGLE INNER CREASE BEAM CHORD CORRODED ON UPPER SURFACE. R & R THE SUPPORT ANGLE IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 42,325 hrs · 24,718 cycles

AFT CARGO BAY FLOORBEAM TEE ASSEMBLY CORRODED AT BS 772. R & R THE TEE ASSEBMLY IAW SRM & DWG.

Part: FRAME — CRACKED (BS 296) · airframe 42,325 hrs · 24,718 cycles

R1 DOOR CUTOUT LOWER STAB FRAME CRACKED AT BS 296, STRINGER 17R. R & R THE FRAME IAW DWG AND SRM.

Part: CREASE BEAM — CORRODED · airframe 42,325 hrs · 24,718 cycles

AFT GALLEY DOOR CUTOUT SURROUND CREASE BEAM CORRODED. R & R CREASE BEAM IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 42,325 hrs · 24,718 cycles

STRINGER CLIP 8R CRACKED AT BS 360. R & R THE STRINGER CLIP IAW DWG AND SRM.

Part: FRAME — CRACKED (BS 787) · airframe 42,325 hrs · 24,718 cycles

FRAME WEB CRACKED AT BS 787, BETWEEN STRINGERS 8 - 9R. REPAIRED THE FRAME IAW ER.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 42,325 hrs · 24,718 cycles

LEFT HORIZONTAL STABILIZER RIB LOWER CHORD VERTICAL STIFFENER, CRACKED AT HSS 129.50. 3RD FROM FRONT SPAR. REPAIRED THE STIFFENER IAW SRM & EA.

Part: PLATE — CRACKED (HORIZONTAL STAB) · airframe 42,325 hrs · 24,718 cycles

LEFT HORIZONTAL STABILIZER UPPER FRONT SPAR SLIDING SEAL PLATE CRACKED ALONG THE CORNER PLATES. R&R SLIDING SEAL PLATE IAW AMM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 42,325 hrs · 24,718 cycles

LEFT HORIZONTAL STABILIZER AT HSS 129.5 RIB LOWER CHORD VERTICAL STIFFENER CRACKED, 4TH FROM FRONT SPAR. REPAIRED THE STIFFENER IAW SRM & EA.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 42,325 hrs · 24,718 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS. 663, LBL 34. REPAIRED THE BULKHEAD WEB IAW SRM.

Part: CHANNEL — CORRODED (BS 500A-500D) · airframe 42,325 hrs · 24,718 cycles

FORWARD CARGO BAY ZEE CHANNEL CORRODED BETWEEN BS 500A TO 500D, RBL 25. R & R THE CHANNEL IAW SRM.

Part: CHANNEL — CORRODED (BS 500-500A) · airframe 42,325 hrs · 24,718 cycles

FORWARD CARGO ZEE CHANNEL CORRODED BETWEEN BS 500 TO 500A, RBL 25. R & R THE CHANNEL IAW SRM AND DWG.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 42,325 hrs · 24,718 cycles

LEFT HORIZONTAL STABILIZER RIB LOWER CHORD VERTICAL STIFFENER, CRACKED AT HSS 129.50, 2ND FROM FRONT SPAR. REPAIRED THE STIFFENER IAW SRM AND EA.

Part: FAIRING — CRACKED (LT WING TE FLAP) · airframe 42,325 hrs · 24,718 cycles

LEFT WING FLAP TRACK FAIRING 544BB CRACKED ALONG LEADING EDGE. REPAIRED THE FAIRING IAW SRM.

Part: CREASE BEAM — CORRODED (AFT GALLEY DOOR) · airframe 42,325 hrs · 24,718 cycles

AFT GALLEY DOOR CUTOUT SURROUND CREASE BEAM CORRODED. R & R THE CREASE BEAM IAW DWG & SRM.

Part: DOOR FRAME — CRACKED (R1) · airframe 42,325 hrs · 24,718 cycles

R1 DOOR CUTOUT FORWARD SIDE REVEAL FRAME CRACKED ABOVE UPPER HINGE. R & R DOOR FRAME IAW DWG AND SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 42,325 hrs · 24,718 cycles

RIGHT WING LEADING EDGE NR 5 SLAT LOWER SKIN CRACKED AT ACTUATOR ATTACH POINT SS 85.19. REPAIRED NR 5 SLAT IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,325 hrs · 24,718 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 41,788 hrs · 24,421 cycles

FORWARD RT EMERGENCY BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 41,788 hrs · 24,421 cycles

LEFT EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT ROW 17. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 41,788 hrs · 24,421 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 41,788 hrs · 24,421 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 41,788 hrs · 24,421 cycles

LEFT OVERWING EMERGENCY BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: SENSOR — DIRTY (NLG WW) · airframe 41,396 hrs · 24,191 cycles

IN FLIGHT WITH GEAR LEVER UP OR OFF FWD PANEL NOSE GEAR RED LIGHT & OVERHEAD PANEL GREEN GEAR DOWN LIGHT ILLUMINATED. CLEANED SENSOR PSEU IAW MMM.

Part: SPRING — DEFECTIVE (AILERON) · airframe 40,910 hrs · 23,887 cycles

DIVERSION, AILERON FEEL WAS UNUSUALLY LOW WHEN HAND FLYING. R & R SPRING ON AILERON & FEEL CENTERING UNIT IAW AMM 27-11-81.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,599 hrs · 23,714 cycles

LEFT EMER EXIT SIDE LIGHT BULB INOPERATIVE, BETWEEN ROW 1 - 11. R & R BULB IAW AMM.

Part: HYDRAULIC LINE — LEAKING (NR 1 ENGINE) · airframe 39,353 hrs · 22,975 cycles

DIVERSION, NR 1 ENG HYD PUMP FAIL A SYS. FOUND QUICK D LINE ON ENG NR 1 DRIVEN PUMP LEAKED. R & R QUICK D LINE IAW AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 38,244 hrs · 22,340 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,018 hrs · 21,659 cycles

LEFT OVERWING EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 36,544 hrs · 21,392 cycles

R2 DOOR EMER LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: SKIN — DEFECTIVE (LE SLAT) · airframe 35,894 hrs · 21,029 cycles

LEFT WING NR 4 SLAT NOSE SKIN FWD INBD FASTENER HOLE DEFECTIVE. R & R SLAT IAW MM.

Part: SKIN — DEFECTIVE (LE SLAT) · airframe 35,894 hrs · 21,029 cycles

LEFT WING NR 4 SLAT NOSE SKIN INBD CTR FASTENER HOLE DEFECTIVE. R & R SLAT IAW MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

LOWER BULKHEAD CHORD CRACKED A BS 540 STRINGER 22R. REPAIRED CHORD IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

LOWER BULKHEAD CHORD CRACKED AT BS 540 STRINGER 22R. REPAIRED CHORD IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

LOWER BULKHEAD CHORD CRACKED AT BS 540 STRINGER 22L. REPAIRED CHORD IAW EA.

Part: STRAP — DELAMINATED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

STRAP DELAMINATED BETWEEN BS 727A TO 727B STRINGER 2L. REPAIRED STRAP IAW SOPM & SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FORWARD SEAT TRACK FLANGE OTBD FWD HOLE CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FLOORBEAM VERTICAL WEB ANGLE CRACKED AT BS 727B RBL 45.5 AT HOLE H. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FLOORBEAM VERTICAL WEB ANGLE CRACKED AT BS 727B RBL 24.75 AT HOLE H. REPAIRED ANGLE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

AFT SEAT TRACK A FASTENER HOLE CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FORWARD SEAT TRACK FLANGE OTBD FWD HOLE CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FLOORBEAM VERTICAL WEB CRACKED AT BS 727B RBL 24.75 AT HOLE H. REPAIRED WEB IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FORWARD SEAT TRACK FLANGE INBD FWD HOLE CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FORWARD SEAT TRACK FLANGE INBD FWD HOLE CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FORWARD SEAT TRACK FLANGE OTBD FWD HOLE CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FORWARD SEAT TRACK FLANGE OTBD AFT HOLE CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FORWARD SEAT TRACK FLANGE OTBD AFT HOLE CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FORWARD SEAT TRACK FLANGE OTBD AFT HOLE CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FORWARD SEAT TRACK FLANGE INBD FWD HOLE CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FORWARD SEAT TRACK FLANGE INBD AFT HOLE CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

SKIN CRACKED AT BS 540 STRINGER 22R HOLE F. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

SKIN CRACKED AT BS 540 STRINGER 22R HOLE B. REPAIRED SKIN IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FORWARD SEAT TRACK FLANGE INBD AFT HOLE CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FORWARD SEAT TRACK FLANGE INBD AFT HOLE CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FORWARD SEAT TRACK FLANGE OTBD AFT HOLE CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 35,894 hrs · 21,029 cycles

RIGHT WING UPPER TE SHELF PANEL BETWEEN 7 TO 8 SPOILERS L BRACKET CRACKED. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

SKIN CRACKED AT BS 540 STRINGER 22L HOLE B. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,894 hrs · 21,029 cycles

FLIGHT DECK RT NR 1 WINDOW FRAME UPPER OTBD CORNER CRACKED. REPAIRED FRAME IAW EA & ACO.

Part: PLATE — CRACKED (RT WING) · airframe 33,002 hrs · 19,386 cycles

RT WING LOWER FIXED TE PANEL 651GB CRACKED WIGGLE PLATE AT 2 FASTENERS. REPAIRED PLATE IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 32,138 hrs · 18,862 cycles

OVERWING SMALL EMERGENCY EXIT LIGHT PLASTIC COVER LOOSE. R&R LENS IAW MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 31,296 hrs · 18,382 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. R & R LIGHT ASSY IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 31,170 hrs · 18,303 cycles

CO-PILOTS NR 3 WINDOW FRAME FWD POST, 2ND HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 31,170 hrs · 18,303 cycles

PILOTS NR 3 WINDOW FRAME FWD POST, 2ND HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW EA.

Part: BATTERY — FAILED (CABIN) · airframe 30,752 hrs · 18,049 cycles

RIGHT EMERGENCY LIGHTS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER AMM.

Part: LENS — BROKEN (CABIN) · airframe 29,531 hrs · 17,316 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: ATTACH BRACKET — CORRODED (L1 DOOR) · airframe 29,157 hrs · 17,105 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,157 hrs · 17,105 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 138.7. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,157 hrs · 17,105 cycles

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

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,157 hrs · 17,105 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 175.5. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,157 hrs · 17,105 cycles

LEFT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 138.7. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,157 hrs · 17,105 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 184.7. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,157 hrs · 17,105 cycles

LEFT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 98. REPAIRED SKIN IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 28,686 hrs · 16,803 cycles

RIGHT EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM AND SSM.

Part: BATTERY — FAILED (CABIN) · airframe 28,686 hrs · 16,803 cycles

LEFT EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM AND SSM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,683 hrs · 16,802 cycles

LEFT STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 27,028 hrs · 15,786 cycles

FWD EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED COVER PER AMM.

Part: COVER — MISSING (CABIN) · airframe 25,594 hrs · 14,944 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 25,167 hrs · 14,692 cycles

FWD EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,362 hrs · 14,235 cycles

DURING SCHEDULED MV2 CHECK FOUND, LT EMERGENCY EXIT LIGHT INOP BETWEEN ROW 11 TO ROW 15. REMOVED AND REPLACED EEPLS PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 23,983 hrs · 14,028 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MT.

Part: BATTERY — FAILED (CABIN) · airframe 23,983 hrs · 14,028 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 23,101 hrs · 13,529 cycles

DURING SCHEDULED OTS CHECK, FOUND FWD EEPLS BROKEN. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,980 hrs · 13,454 cycles

OVERWING EEPLS INOP. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 22,485 hrs · 13,160 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS COVER LOOSE AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,285 hrs · 13,041 cycles

DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOOR SUPPORT BEAM CORRODED AT BS 771, LBL 13. REPAIRED BEAM PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,285 hrs · 13,041 cycles

DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOOR SUPPORT BEAM CORRODED AT BS 771, LBL 3. REPAIRED BEAM PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,285 hrs · 13,041 cycles

DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOOR SUPPORT BEAM CORRODED AT BS 771, RBL 3. REPAIRED BEAM PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,285 hrs · 13,041 cycles

DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOOR SUPPORT BEAM CORRODED AT BS 771, LBL 8. REPAIRED BEAM PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,081 hrs · 12,909 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP AT ROW 11. RELAMPED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 21,961 hrs · 12,842 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,961 hrs · 12,842 cycles

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

Part: FUSE — BLOWN (CABIN) · airframe 21,799 hrs · 12,750 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT FUSE LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED FUSE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 20,065 hrs · 11,700 cycles

EEPLS LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,957 hrs · 11,636 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP AT ROW 17. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 18,679 hrs · 10,848 cycles

L1 DOOR EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 18,045 hrs · 10,450 cycles

EEPLS BROKEN AT ROW 1. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 18,065 hrs · 10,462 cycles

EEPLS BROKEN AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 17,437 hrs · 10,078 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 17,365 hrs · 10,042 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,286 hrs · 9,986 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED EMERGENCY LIGHT PER MM.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 15,345 hrs · 8,815 cycles

FOUND R1 DOOR EMERGENCY EXIT SIGN DETACHED. ATTACHED LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 15,065 hrs · 8,656 cycles

DURING SCHEDULED HC2 CHECK, FOUND AFT LT AND RT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (COCKPIT) · airframe 15,065 hrs · 8,656 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT FWD EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 15,065 hrs · 8,656 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST AT ROW 16 ABC. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 15,065 hrs · 8,656 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZ STAB AFT OF LEADING EDGE SKIN CRACKED AT BS 147.90. REPAIRED CRACK PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 15,065 hrs · 8,656 cycles

DURING SCHEDULED HC2 CHECK, FOUND MID CABIN LT AND RT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — BROKEN (CABIN) · airframe 14,492 hrs · 8,312 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,809 hrs · 6,664 cycles

DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 11,206 hrs · 6,319 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 11,073 hrs · 6,240 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 8,963 hrs · 5,018 cycles

FWD CABIN EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 7,468 hrs · 4,180 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1 DEF. REMOVED AND REPLACED LIGHT COVER PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 6,627 hrs · 3,690 cycles

DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 4,793 hrs · 2,649 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BULB — INOPERATIVE (L1 DOOR) · airframe 3,599 hrs · 2,011 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.