N780SW

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,105 hrs · 42,882 cycles

SEVERAL EMERGENCY LIGHTS ON RT SIDE OF CABIN INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,741 hrs · 42,654 cycles

RH EMERGENCY EXIT LIGHT INOP. / [01] R&R RH EMERGENCY EXIT LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.

Part: SLIDE — LOW (ZN 800 DOOR) · airframe 71,570 hrs · 42,540 cycles

FWD SERVICE DOOR SLIDE PRESSURE LOW / [01] R&R FWD SERVICE DOOR ESCAPE SLIDE PER MT 725-61-06.

Part: SIGN — OUT OF POSITION (EMERGENCY LIGHTS) · airframe 71,562 hrs · 42,534 cycles

L1 AND R1 DOOR LOWER EXIT SIGNS MISSING DIRECTIONAL ARROWS. REMOVED AND REPLACED L-1 AND R-1 LWR EXIT SIGN LENS ASSY IAW AMM 33-51-01.

Part: NONE — INOPERATIVE · airframe 71,329 hrs · 42,373 cycles

ROW 12-14ABC AND 18ABC SIDEWALL LIGHTS INOP / [01] REPLACED THE WINDOW LIGHT LAMP WITH NEW ON ROW 12-14 A; B; C AND 18 A; B; C PER AMM TASK 33-21-00-960-801. OPS CHECK GOOD.

Part: NONE — MISSING · airframe 71,329 hrs · 42,373 cycles

ROW 15DEF LIGHT COVER DISPLACED / [01] REINSTALLED THE ROW 15 D; E; F WINDOW LIGHT COVER PER AMM TASK 33-21-00-960-801.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,893 hrs · 41,452 cycles

AFT SERVICE DOOR EXTERNAL EMERGENCY LIGHT EXTINGUISHED. / [01] RELAMPED AFT SERVICE DOOR EXTERNAL EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,861 hrs · 40,837 cycles

SUPPLEMENTAL INFORMATION: EMERGENCY EXIT LIGHT IN BIN BULLNOSE IS INOP OVER SEAT 22 RIGHT ; / [01] RELAMPED AND PERFORMED GOOD TEST OF ROW 22 RIGHT BIN(AREA) LIGHT PER AMM 33-51-03-960-801.; [02] VERIFIED ACTION 1

Part: LIGHT — INOPERATIVE (R/H OVERWING) · airframe 68,861 hrs · 40,837 cycles

SUPPLEMENTAL INFORMATION: RIGHT OVERWING SLIDE LIGHT DOES NOT ILLUMINATE. ; RIGHT OVERWING SLIDE LIGHT DOES NOT ILLMINATE. / [01] REPLACED RIGHT OVERWING SLIDE LIGHT LAMP AND PERFORMED SATISFACTORY TEST OF NEW LAMP PER AMM 33-51-04-960-801; NO DEFECTS NOTED.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: BATTERY — FAILED (CABIN) · airframe 68,861 hrs · 40,837 cycles

M1674 BATTERY PACK FAILS CAPACITY TEST ; / [01] REMOVED AND REPLACED M1674 BATTERY PACK PER AMM 33-51-06-960-805 STEP 4.A. THROUGH 4.D.(6)(A); [02] REMOVED AND REPLACED M1674 POWER SUPPLY AS PER AMM. TASK 33-51-06-960-806 5.E.(1-4); [03] M1674 REQUIRES CHARGING TIME OF 180 MINUTES. POWER ON AND CHARGING START AT 13:15 HRS AS PER AMM. 33-51-06-960-805 D.6.B.2; [04] VERIFIED CORRECTIVE ACTION ENTRIES 2. AND 3.; [05] VERIFIED INSTALLATION OF M1674 POWER SUPPLY PER AMM 33-51-06-960-806 AND REPLACED M1674 BATTERY AND; CHARGED BATTERIES FOR 180 MINUTES; AND PERFORMED SATISFACTORY INSTALLATION TEST PER AMM 33-51-06-960-805; NO DEFECTS NOTED.; [06] VERIFIED CORRECTIVE ACTION ITEM 5.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 68,861 hrs · 40,837 cycles

FWD ENTRY SLIDE LIGHT OUT. REPLACING LAMP DID NOT CORRECT PROBLEM. TROUBLESHOT FORWARD ENTRY SLIDE LIGHT (L371). ON FURTHER INVESTIGATION, FOUND CONNECTOR D11074 STA 365 WL 226 LBL 72 DISCONNECTED. RECONNECTED AND PERFORMED GOOD OPERATIONAL TEST IAW AMM TASK 33-51-04-960-802 STEP 3.F.(10) & (11) & WDM 33-51-12 PAGE 2 SHEET 1.

Part: FUSE — INOPERATIVE (CABIN) · airframe 68,861 hrs · 40,837 cycles

RIGHT HAND AFT EXIT IDENTIFIER IS OUT ; / [01] REPLACED FUSE AT EMERGENCY EXIT POWER SUPPLY M1669 AND PERFORMED GOOD INSTALLATION TEST AS PER AMM. 33-51-06-960-804 AND WDM. 33-51-21; [02] VERIFIED REPLACED FUSE AT EMERGENCY EXIT POWER SUPPLY M1669 AND PERFORMED GOOD INSTALLATION TEST AS PER AMM. 33-51-06-960-804 AND WDM. 33-51-21; [03] VERIFIED CORRECTIVE ACTION ENTRIES 1. AND 2.; [04] COMPLETED STEP 1. (INSTALLATION RETURN AIR GRILLE); [05] VERIFIED CORRECTIVE ACTION ENTRY 4. COMPLETE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,861 hrs · 40,837 cycles

AFT ENTRY SLIDE LIGHT OUT ; / [01] RELAMPED AFT ENTRY SLIDE LIGHT AND PERFORMED SATISFACTORY TEST OF NEW LAMP; NO DEFECTS NOTED.; [02] CORRECTION TO ITEM 1: ALL WORK PERFORMED PER AMM33-51-04-960-801.; [03] VERIFIED CORRECTIVE ACTION 1 AND 2.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

RIGHT OVERWING EXTERIOR EXIT LIGHT IS OUT ; / [01] RELAMPED RIGHT OVERWING SLIDE LIGHT AND PERFORMED SATISFACTORY TEST OF NEW LAMP PER AMM 33-51-04-960-801; NO DEFECTS NOTED.; [02] VERIFIED CORRECTIVE ACTION 1.

Part: FUSE — INOPERATIVE (CABIN) · airframe 68,861 hrs · 40,837 cycles

BULLNOSE EXIT LIGHT BETWEEN ROW 8 AND 9 RIGHT IS OUT ; / [01] RELAMPED AREA LIGHT BETWEEN ROW 8 AND 9 RIGHT PER AMM 33-51-03-960-801; NEW LAMP ALSO FAILS TO ILLUMINATE.; [02] VERIFIED CORRECTIVE ACTION 1. <BR><BR>RELAMPING FAILED TO RESOLVE THE ISSUE.; [03] REPLACED FUSE AT EMERGENCY EXIT POWER SUPPLY M1669 AND PERFORMED GOOD INSTALLATION TEST AS PER AMM. 33-51-06-960-804 AND WDM. 33-51-21; [04] VERIFIED CORRECTIVE ACTION ENTRY 3.

Part: LIGHT — BROKEN (CABIN) · airframe 688,860 hrs · 40,837 cycles

G-4 GALLEY EMERGENCY EXIT LIGHT IS BROKEN. ; / [01] REPLACED G-4 GALLEY EMERGENCY EXIT LIGHT PER AMM 33-51-01-960-802.; [02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.; [03] COMPLETED STEP 1'S FUNCTIONAL TESTING.; [04] VERIFIED GOOD FUNCTIONAL CHECK; [05] VERIFIED ACCOMPLISHMENT OF STEP 1 & CORRECTIVE ACTION ITEM 3.

Part: CONNECTOR — BROKEN (CABIN) · airframe 68,860 hrs · 40,837 cycles

G-1 GALLEY EMERGENCY EXIT LIGHT HAS BROKEN CONNECTOR. ; / [01] RE-TERMINATED CONNECTOR(JIFFY SPLICE) FOR G1 GALLEY EMERGENCY EXIT LIGHT (L1186) PER SWPM 20-30-12 AND WDM 33-51-21.<BR><BR>CRIMPER: I.D.: E11329; [02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.; [03] COMPLETED STEP 1'S FUNCTIONAL TESTING.; [04] VERIFIED GOO FUNCTIONAL CHECK; [05] VERIFIED GOOD FUNCTIONAL.; [06] ALL WORK COMPLETED.

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 68,861 hrs · 40,837 cycles

SUPPLEMENTAL INFORMATION: THE L/H HORIZONTAL STAB REMOVABLE L/E SPLICE AT STAB TIP; STAB BL 281.81; IS CRACKED. ; / [01] REMOVED AND REPLACED CRACKED L/H HORIZONTAL STAB REMOVABLE L/E SLICE AT STAB TIP STAB BL 281.81 IAW SRM 51-40-02-0G-0 AND DWG# 186A1001; [02] VERIFIED SPLICE INSTALLED PER ARM 51-40-02 AND DWG #186A1001

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

PANEL 193CR HAS DELAMINATED DENT TO OUTER SURFACE. ON INSPECTION OF PANEL FOUND TWO PUNCTURES TO OUTER SURFACE FACE SHEET, LOCATED 8' FROM AFT EDGE 18.75' FROM UPPER EDGE, & AT 5' FROM AFT EDGE; 19' FROM UPPER EDGE. ORIGINAL DAMAGE NOTED, & DAMAGES FOUND ARE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4A(5-6). REPAIRS TO BE ACCOMPLISHED IAW SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-11 PER SRM 53-40-70-2R-1 PAR 4B(1).

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON SKIN UNDER ADF 1 ANTENNA AT FASTENER HOLES AT BS 693 - BS 702 BETWEEN STR 1 AND STR 2R. ; / [01] REMOVED CORROSION ON SKIN BS 693-702 AT FASTENER HOLES BETWEEN STR1 AND STR2R PER SRM 51-10-02-0G-0; [02] ADDED MEASUREMENT CHART; [03] VERIFIED MEASUREMENT CHART; [04] VERIFIED CORRECTIVE ACTION ENTRY 1. ALL CORROSION REMOVED.; [05] UT THICKNESS TESTED BLENDED AREAS PER 737NDT PART 4 51-00-00 PROCEDURE 2. LOWEST REMAINING THICKNESS IS .036'. FILLED OUT GRID MAP FOR ENGINEERING. CAL ID E650 ATS2342.; [06] LIMIT STATEMENT FROM OUT OF LIMITS PER ARM90-7023-01 ONLY .002 MAX ONLY; [07] VERIFIED CORRECTIVE ACTION ENTRY 6. OUT OF LIMITS.; [08] HFEC INSPECTED BLENDED AREAS IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. <BR>EQUIP ID#: IS000450 S/N: N500D000M120071; [09] HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16; NO CRACKS NOTED. <BR>HFEC INSPECTED COUNTERSINKS IAW 737 NDTM PART 6 53-30-00 PROCEDURE 3; NO CRACKS NOTED.<BR> <BR>EQUIP ID#: IS000450 S/N: N500D000M120071 EQUIP ID#: ATS2407 S/N: MM1591DD064104; [10] AS PER EA 21-153-03198; THE DAMAGE IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITH AN INSPECTION THRESHOLD DEFINED IN EA 21-153-03198-DTI. REF: MPM 52.07.01.03 PARAGRAPH 1.B.; [11] VERIFIED CORRECTIVE ACTIONS STEP 10.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON CAPTAIN'S AFT O/B SEAT TRACK BS 243 LBL 22 WL 207. ; / [01] REPLACED SEAT TRACK ON CAPTAINS AFT O/B SEAT TRACK BS 243 LBL 22 WL 207 PER AMM 25-11-11-400-801 REF IPC 25-11-51-09A TOURQUED TO 60 IN-LBS PER SRM 51-40-04-0G-0 TOURQUE WRENCH USED: ID:ATS2657 S/N:0821900635 DATE:08/2021 DUE:08/2022.; [02] VERIFIED COMPLETION; [03] VERIFIED CORRECTIVE ACTION ENTRY 1. CARD COMPLETE.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON CAPTAIN'S FWD I/B SEAT TRACK BS 226 LBL 12 WL 207. ; / [01] REPLACED SEAT TRACK ON CAPTIANS FWD I/B SEAT TRACK BS 226 RBL 12 WL 207 PER AMM 25-11-11-400-801 REF IPC 25-11-51-09A TOURQUED TO 60 IN-LBS PER SRM 51-40-04-0G-0 TOURQUE WRENCH USED: ID:ATS2657 S/N:0821900635 DATE:08/2021 DUE:08/2022.; [02] REPLACED SEAT TRACK ON CAPTIANS FWD I/B SEAT TRACK BS 226 LBL 12 WL 207 PER AMM 25-11-11-400-801 REF IPC 25-11-51-09A TOURQUED TO 60 IN-LBS PER SRM 51-40-04-0G-0 TOURQUE WRENCH USED: ID:ATS2657 S/N:0821900635 DATE:08/2021 DUE:08/2022.; [03] VERIFIED COMPLETION; [04] VERIFIED CORRECTIVE ACTION ENTRY 1. CARD COMPLETE.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON F/O'S AFT I/B SEAT TRACK BS 243 RBL 12 WL 207. ; / [01] REPLACED SEAT TRACK ON F/O'S AFT I/B SEAT TRACK BS 243 RBL 12 WL 207 PER AMM 25-11-11-400-801 REF IPC 25-11-51-09A TOURQUED TO 60 IN-LBS PER SRM 51-40-04-0G-0 TURQUE WRENCH USED: ID:ATS2657 S/N:0821900635 DATE:08/2021 DUE:08/2022.; [02] CERTIFIED ACTION1.; [03] UPDATED PARTS USED INFORMATION.; [04] VERIFIED CORRECTIVE ACTION ENTRY 1. CARD COMPLETE.

Part: NONE — PEELING (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

PASSENGER CABIN FLOOR BOARD 241ABF HAS PEELING STRANDS ON UPPER SURFACE ; / [01] IDENTIFIED PART IAW SRM 53-00-50-0I-1 FIG 6; TABLE 6.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F.<BR><BR>REPAIR WILL BE ACCOMPLISHED IAW SRM 53-00-50-2R-1.<BR><BR>REMOVED 16 THROUGH INSERTS TO FACILITATE REPAIR; REMOVED DAMAGE; AND CLEANED REPAIR AREA IAW SRM 53-00-50-2R-1 PARA 3A-F.; [08] CURED REPAIR PLIES USING THERMOMETER ID: PER 1919 SN: 180657982; UNBAGGED & TRIMMED EDGES IAW SRM53-00-50-2R-1 PARA 3. M.<BR><BR>INSTALLED 16 EA. THROUGH INSERTS USING BMS 5-107 LOT # AK0DP4051K IAW SRM 53-00-50-2R-1 PARA 3.N.<BR><BR>INSERTS REQUIRE CURE.; [09] ADDING TO CORRECTIVE ACTION LINE 8. 'ALSO INCLUDING IAW BOEING DWG 147A5810 SHEET 88.'; [10] VERIFIED CORRECTIVE ACTION 6-9; [11] CURED INSERTS USING THERMOMETER ID:ATS1174 S/N:25810009WS IAW SRM 53-00-50-2R-1 PAR 3N.; [12] VERIFIED CORRECTIVE ACTION 11; [13] VERIFIED CURE SHEET ATTACHED; JOB COMPLETE

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON F/O'S AFT O/B SEAT TRACK BS 243 RBL 22 WL 207. ; / [01] REPLACED SEAT TRACK ON F/O'S AFT O/B SEAT TRACK BS 243 RBL 22 WL 207 PER AMM 25-11-11-400-801 REF IPC 25-11-51-09A TOURQUED TO 60 IN-LBS PER SRM 51-40-04-0G-0 TURQUE WRENCH USED: ID:ATS2657 S/N:0821900635 DATE:08/2021 DUE:08/2022.; [02] VERIFIED COMPLETION; [03] SIGNED PART BLOCK; [04] VERIFIED CORRECTIVE ACTION ENTRY 1. CARD COMPLETE.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON F/O'S FWD O/B SEAT TRACK BS 226 RBL 22 WL 207. ; / [01] REPLACED SEAT TRACK ON F/O'S FWD O/B SEAT TRACK BS 226 RBL 22 WL 207 PER AMM 25-11-11-400-801 REF IPC 25-11-51-09A TOURQUED TO 60 IN-LBS PER SRM 51-40-04-0G-0 TURQUE WRENCH USED: ID:ATS2657 S/N:0821900635 DATE:08/2021 DUE:08/2022.; [02] VERIFIED COMPLETION; [03] SIGNED PART BLOCK; [04] VERIFIED REPLACEMENT OF F/O'S FWD O/B SEAT TRACK; BS 226; RBL 22 WL 207 PER AMM 25-11-11-400-801 AND REF IPC 25-11-51-09A

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON CAPTAIN'S FWD O/B SEAT TRACK BS 226 LBL 22 WL 207. ; / [01] REPLACED SEAT TRACK ON CAPTAINS FWD O/B SEAT TRACK BS 226 LBL 22 WL 207 PER AMM 25-11-11-400-801 REF IPC 25-11-51-09A TOURQUED TO 60 IN-LBS PER SRM 51-40-04-0G-0 TOURQUE WRENCH USED: ID:ATS2657 S/N:0821900635 DATE:08/2021 DUE:08/2022.; [02] VERIFIED COMPLETION; [03] VERIFIED CORRECTIVE ACTION ENTRY 1. CARD COMPLETE.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON CAPTAIN'S AFT I/B SEAT TRACK BS 243 LBL 12 WL 207. ; / [01] REPLACED SEAT TRACK ON CAPTAINS AFT I/B SEAT TRACK BS 243 LBL 12 WL 207 PER AMM 25-11-11-400-801 REF IPC 25-11-51-09A TOURQUED TO 60 IN-LBS PER SRM 51-40-04-0G-0 TOURQUE WRENCH USED: ID:ATS2657 S/N:0821900635 DATE:08/2021 DUE:08/2022.; [02] VERIFIED COMPLETION; [03] VERIFIED CORRECTIVE ACTION ENTRY 1. CARD COMPLETE.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON F/O'S FWD I/B SEAT TRACK BS 226 RBL 12 WL 207. ; / [01] REPLACED SEAT TRACK ON F/O'S FWD I/B SEAT TRACK BS 226 RBL 12 WL 207 PER AMM 25-11-11-400-801 REF IPC 25-11-51-09A TOURQUED TO 60 IN-LBS PER SRM 51-40-04-0G-0 TOURQUE WRENCH USED: ID:ATS2657 S/N:0821900635 DATE:08/2021 DUE:08/2022.; [02] VERIFIED COMPLETION; [03] VERIFIED REPLACEMENT OF F/O'S FWD I/B SEAT TRACK; BS 226; RBL 226; RBL 12; WL 207 PER AMM 25-11-11-400-801 REF AND IPC 25-11-51-09A

Part: WEB — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON 1016 BULKHEAD WEB AT B.S. 1016; L.B.L. 2; W.L. 190. ; / [01] EVALUATED CORROSION ON BS 1016 BULKHEAD WEB LBL2 WL190 REMOVED .005' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.032' FOUND OUT OF LIMITS PER SRM 53-80-08-1A-1 USING ATS TOOL ID # ATS1225 S/N UNKNOWN;[10] FABRICATED REPAIR PARTS; APPLIED CHEMICAL CONVERSION COATING AND PRIMER PER EA 21-153-03150. REQUEST OK TO INSTALL.; [11] VERIFIED CORRECTIVE ACTIONS STEP 10 AND OK TO INSTALL GIVEN.; [12] INSTALLED PERMANENT FASTENERS BEFORE SQUEEZE OUT TIME; APPLIED SEALANT AT 8:30AM UTC TIME (1:30AM LOCAL TIME) 10/27/2021.; [13] VERIFIED CORRECTIVE ACTIONS STEP 12.; [14] REPAIRED PER SWA EA # 21-153-03150; [15] VERIFIED REPAIRED PER SWA EA # 21-153-03150.; [16] VERIFIED ALL STEPS COMPLETE.

Part: NONE — CRACKED (LH HOR STAB) · airframe 68,861 hrs · 40,837 cycles

SUPPLEMENTAL INFORMATION: LT HORIZ STAB FRONT SPAR UPPER SLIDE SEAL IS CRACKED LT HORI STAB FRONT SPAR UPPER SLIDE SEAL IS CRACKED / REMOVED AND REPLACED LT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-000-802 AND AMM 53-31-31-400-802 TOOL INFO IS000258 R03886 01/2022 CERTIFIED ACTION 1 VERIFIED CORRECTIVE ACTION ENTRY 1. CARD COMPLETE

Part: NONE — CRACKED (RH HOR STAB) · airframe 68,861 hrs · 40,837 cycles

SUPPLEMENTAL INFORMATION: RT HORIZ STAB FRONT SPAR UPPER SLIDE SEAL IS CRACKED RT HORI STAB FRONT SPAR UPPER SLIDE SEAL IS CRACKED / REMOVED AND REPLACED RT FRONT UPPER SLIDE SEAL IAW AMM 53-31-31-000-802 AND AMM 53-31-31-400-802 TOOL INFO IS000258 R03886 01/2022 CERTIFIED ACTION 1 VERIFIED CORRECTIVE ACTION ENTRY 1. CARD COMPLETE

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON FLOOR SUPPORT BS 312-328 RBL 11 WL 208. ; / [01] REMOVED CORROSION ON FLOOR SUPPORT AT BS312-328 RBL 11 WL208 1'X1' AREA WITH A .050' MATERIAL LOSS. ORIGINAL THICKNESS WAS .080'. OUT OF LIMITS. WORK PERFORMED IAW SRM 51-10-02 AND SRM 53-10-51-1A-1; [02] VERIFIED CORRECTIVE ACTION 1.; [03] REMOVED DAMAGED FLOOR SUPPORT AT BS312-328; RBL 11;WL 208 IAW B737 SRM 51-40-02.; [04] CERTIFIED ACTION 3.; [05] LOCATED AND DRILLED AND COUNTERSUNK NEW FLOOR SUPPORT STA 312-328; RBL 11; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0 DWG#141A5400. OK TO INSTALL.; [06] INSPECTED ACTION 5; [07] INSTALLED NEW FLOOR SUPPORT STA 312-328; RBL 11; WL 208 PER SRM 51-40-02-0G-0; 51-40-03-0G-0; DWG#141A5400.; [08] RII INSPECTED ACTION 7; [09] INSPECTION COMPLETE

Part: NONE — CRACKED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

FWD ENTRY DOOR MOP SILL CRACKED AT BS 303 LBL 55 WL 209. ; / [01] REMOVED DAMAGED FWD ENTRY DOOR MOP SILL BS 270-360; LBL 55; WL 208 PER SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW FWD ENTRY DOOR MOPSILL BS 270-360; LBL 55; WL 208 PER SRM 51-40-05-0G-0 AND BOEING DWG 141A8110. OK TO INSTALL.; [03] VERIFIED CORRECTIVE ACTION ENTRY 1. OK TO INSTALL GIVEN.; [04] INSTALLED FED MOPSILL BS270-BS360 LBL55 WL208 I.A.W BOEING DWG 141A8110;141A8310 AND SRM 51-40-02-0G-0; [05] VERIFIED CORRECTIVE ACTION ITEM 4.; [06] VERIFIED TASK IS COMPLETE.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CRACKED FLOOR SUPPORT BS 312-328 LBL 45 WL 208. ; / [01] UPDATED TABLE; [02] REMOVED DAMAGED FLOOR SUPPORT STA 312-328; LBL 45; WL 208 PER SRM 51-40-02-0G-0.; [03] LOCATED AND DRILLED NEW FLOOR SUPPORT STA 312-328; LBL 45; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG#141A5400. OK TO INSTALL.; [04] INSPECTED ACTION 3; OK TO INSTALL; [05] OK TO INSTALL; [06] INSTALLED NEW FLOOR SUPPORT STA 312-328; LBL 45; WL 208 PER SRM 51-40-02-0G-0; 51-40-03-0G-0; DWG#141A5400.; [07] RII INSPECTED ACTION 6; [08] INSPECTION COMPLETE

Part: NONE — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON AFT SERVICE DOOR MOP SILL UPPER SURFACE BS 977-991 RBL 50 WL 208. ; / [01] REMOVED CORROSION ON AFT SERVICE DOOR MOPSILL STA 977-991; RBL 50; WL 208. MAX MATERIAL REMOVED WAS .023' 1' BY 4' BY 1'; FROM .080'. OUT OF LIMITS PER SRM 53-70-15-01-1; SRM 53-70-15-1A-1; SRM 51-10-02-0G-0. MEASURED DEPTH WITH SPHERICAL MICROMETER ID#IS000459; S/N# 67127987; EXPIRES 01/2022.; [02] VERIFIED CORRECTIVE ACTION STEP 1.; [03] REMOVED ASD MOP SILL LOCATED AND DRILLED NEW ASD MOP SILL<BR>SI # 7530246 ALL I.A.W BOEING DWG 147A8540;147A8501;SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0 OK TO INSTALL; [04] VERIFIED CORRECTIVE ACTION 3; [05] ON ASD MOPSILL 100% TEMPORARY AND PERMANENT FASTENER INSTALLED WITHIN SEALANT SQUEEZE OUT TIME I.A.W SOPM 20-50-19; [06] VERIFIED ON ASD MOPSILL 100% TEMPORARY AND PERMANENT FASTENER INSTALLED WITHIN SEALANT SQUEEZE OUT TIME I.A.W SOPM 20-50-19; [07] REMOVED AND REPLACED AFT SERVICE DOOR MOPSILL I.A.W BOEING DWG 147A8501;147A0000 AND SRM 51-40-02-0G-0; [08] VERIFIED CORRECTIVE ACTION 7.; [09] VERIFIED ALL STEPS ARE COMPLETE.; [10] VERIFIED ALL INSPECTION STEP ARE COMPLETE.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON PASSENGER CABIN CREASE BEAM BS716 LBL60 WL208. CREASEBEAM WEB BS 706 - 716; LBL 65 - 70, WL 208 REPLACED ON CARD TTG8Q006SPMB.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

R/H STRINGER 8 FRAME CRACKED BS 500A RBL 65 WL 273. ; / [01] UPDATED MEASUREMENTS TABLE.; [02] REPAIRED R/H STRINGER 8 FRAME AT BS 500A RBL 65 WL 273 PER EA 1-A53-12114 R7.; [03] COMPLETE; [04] ALL STEPS COMPLETE

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CRACKED FLOOR SUPPORT BS380-400 BL 0 WL 208. ; / [01] REMOVED CRACKED FLOOR SUPPORT FROM BS380-400 BL 0; IAW B737 SRM 51-40-02-0G-0.; [02] RECEIVE NEW FLOOR SUPPORT ANGLE 143A5410U11 ; LOCATED AND DRILLED IAW B737 SRM 51-40-05-0G-0 AND DWG 143A5400. OK TO INSTALL.; [03] CERIFIED ACTIONS 1 AND 2.; [04] VERIFIED ACTION 2; [05] INSTALLED NEW FLOOR SUPPORT ANGLE 143A5410U11; IAW B737 SRM 51-40-02-0G-0 AND DWG 143A5400.; [06] CERTIFIED ACTION 5; [07] VERIFIED ACTION 5; [08] VERIFIED ACTION 5 (RII)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS727B+4 - 727C; BS727C+10 - BS727D; BS727D+10; BS727E+6 - BS753; BS767 - BS778; BS790; BS795; BS810; BS827 - BS841; BS853 - BS873. RBL25 WL208. MARKED ; / [01] UPDATED TABLE; 06] LOCATED AND DRILL NEW SEAT TRACK RBL 25 STA 727B-887 WL208 IAW DWG 146A5300 REV:A AND SRM 51-40-05; [07] VERIFIED CORRECTIVE ACTION 5;6; [08] REQUEST OK TO INSTALL.; [09] CERTIFIED ACTIONS 5;6; AND 8; [10] VERIFIED SEAT TRACK FABRICATED IN ACCORDANCE WITH BOEING DRAWING 146A5350 AS SHOWN ON ATS DWG ATSHFAB-100-315. REFER TO ATS BUILD RECORD ON CUSTOMER RO NO ATSHFAB-100-316; JOB NUMBER: 529637.; [11] VERIFIED CORRECTIVE ACTION ITEM 6 & 10.; [12] OK TO INSTALL NEW SEAT TRACK; FROM ACTION 8; [13] OK TO INSTALL.; [14] INSTALLED PASSENGER CABIN SEAT TRACK BS727B TO BS887 RBL25 IAW SRM 51-40-02-0G-0 BOEING DWG 147A5300.; [15] CERTIFIED ACTION 14.; [16] VERIFIED CORRECTIVE ACTIONS STEP 14 COMPLETED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS546- BS562; BS578 - BS663; BS670; BS677 - BS692; BS696 - BS725; BS727 - BS727A+10. RBL45 WL208. MARKED ; / [01] UPDATED TABLE; [02] ACCOMPLISHED STEPS 1-6; [03] COMPLETED STEPS 1 - 6.; [04] APPLIED CHEMICAL CONVERSION COATING PER SOPM 20-43-03 TYPE 5; CLASS F; STEP F; [05] APPLIED CHEMICAL CONVERSION COATING ON BS 546-BS562;BS578-BS663;BS670;BS677-BS692;BS696-BS725;BS 727-BS727A+10. RBL 45 WL 208 PER SOPM 20-43-03 TYPE 5; CLASS F; STEP F; [06] VERIFIED CHEMICAL CONVERSION COATING.; [07] VERIFIED CHEMICAL CONVERSION COATING APPLIED ON PASSENGER CABIN SEAT TRACK BS 546-BS562;BS578-BS663;BS670;BS677-BS692;BS696-BS725;BS 727-BS727A+10. RBL 45 WL 208 PER SOPM 20-43-03 TYPE 5; CLASS F; STEP F; [08] APPLIED ALUMINIZED PRIMER ON BS 546-BS562;BS578-BS663;BS670;BS677-BS692;BS696-BS725;BS 727-BS727A+10. RBL45 WL208 PER SRM 53-00-52-1A-1 STEPS 2. B. (2) AND SOPM 20-41-04 FIGURE 1 (SHEET 1 OF 3).; [09] VERIFIED CORRECTIVE ACTION ENTRY 8. CARD COMPLETE

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS380 - BS400; BS410 - BS428; BS440 - BS460; BS461. RBL25 WL208. MARKED ; / [01] UPDATED TABLE; [02] UPDATED STEPS 1-4; [03] COMPLETED STEPS 1-4; [04] COMPLETED STEP 5; [05] COMPLETED STEP 5 AND CHANGED TO PARTIAL; [06] VERIFIED COMPLETION OF STEP 5; [07] COMPLETED STEP 6; [08] INSPECTION COMPLETE

Part: NONE — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON PASSENGER CABIN CREASE BEAM BS727C+18 RBL69 WL208. ; / [01] UPDATED TABLE; [02] REMOVED 1 EA FASTENER IN PASSENGER CABIN CREASEBEAM WEB STA 727C+18; RBL 69; WL 208 FOR ACCESS PER SRM 51-40-02-0G-0.; [03] REMOVED CORROSION ON UPPER SURFACE ON CREASEBEAM WEB STA 727C+18; RBL 69; WL 208. AREA BLENDED IS 1' BY 1' PER SRM 51-10-02-0G-0.; [04] VERIFIED CORRECTIVE ACTIONS 1-3; [05] UT INSPECTED BLENDED AREAS IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.029' ADJACENT TO 0.032'. <BR>EQUIP ID#: ATS2031 S/N: 170515011; [06] MAX MATERIAL REMOVED WAS .003' FROM .032'.IN LIMITS PER SRM 53-60-13-1A-1.; [07] PASSENGER CABIN CREASE BEAM WEB BS 727C-727D; RBL 69; WL 208 TO BE REMOVED AND REPLACED ON CCN: TTG8Q006SMWB.; [08] VERIFIED CORRECTIVE ACTION ENTRY 7. CARD COMPLETE; [09] UPON FURTHER INVESTIGATION FOUND CREASE BEAM WEB TO BE IN LIMITS; REPLACEMENT NOT REQUIRED. CHEMICAL CONVERSION COATING; APPLICATION OF PRIMER AND FASTENER INSTALLATION TO BE ACCOMPLISHED ON CCN: TTG8Q006SMWB.; [10] COMPLETE; [11] VERIFIED CORRECTIVE ACTIONS 1-3.<BR><BR>VERIFIED UPON FURTHER INVESTIGATION FOUND CREASE BEAM WEB TO BE IN LIMITS; REPLACEMENT NOT REQUIRED. CHEMICAL CONVERSION COATING; APPLICATION OF PRIMER AND FASTENER INSTALLATION TO BE ACCOMPLISHED ON CCN: TTG8Q006SMWB.; [12] ALL WORK COMPLETE

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS727B+8 - BS727C; BS727C+7 - BS727D+10; BS727E+5 - BS727E+16; BS747; BS759; BS767; BS778; BS791- BS807; BS725 - BS741; BS751 - BS873. RBL45 WL208. MARKED ; / [01] UPDATED TABLE; [02] ACCOMPLISHED STEPS 1-10; [03] COMPLETED STEPS 1 - 10.; [04] APPLIED CHEMICAL CONVERSION COATING PER SOPM 20-43-03 TYPE 5; CLASS F; STEP F; [05] APPLIED CHEMICAL CONVERSION COATING ON BS727+8-BS727C; BS727C+7-BS727D+10;BS727E+5-BS727E+16;BS;747;BS759;BS767;BS778;BS791-BS807;BS725-BS741;BS751-BS873. RBL45 WL 208 PER SOPM 20-43-03 TYPE 5; CLASS F; STEP F; [06] VERIFIED CHEMICAL CONVERSION COATING.; [07] VERIFIED CHEMICAL CONVERSION COATING APPLIED ON PASSENGER SEAT TRACK AT BS727+8-BS727C; BS727C+7-BS727D+10;BS727E+5-BS727E+16;BS;747;BS759;BS767;BS778;BS791-BS807;BS725-BS741;BS751-BS873. RBL45 WL 208 PER SOPM 20-43-03 TYPE 5; CLASS F; STEP F; [08] APPLIED ALUMINIZED PRIMER ON BS727+8-BS727C; BS727C+7-BS727D+10; BS727E+5-BS727E+16; BS747; BS759; BS767; BS778; BS791-BS807; BS725-BS741; BS751-BS873. RBL45 WL 208 PER SRM 53-52-1A-1 STEP 2. B. (2) AND SOPM 20-41-04 FIGURE 1 (SHEET 1 OF 3); [09] VERIFIED CORRECTIVE ACTION ENTRY 8. CARD COMPLETE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS480 - BS487; BS500 - BS500A; BS500A+10; BS500A+17; BS500B+8; BS500B; BS500C; BS500C+8; BS500D; BS520. RBL45 WL208. MARKED ; / [01] UPDATED TABLE; [02] ACCOMPLISHED STEPS 1-10; [03] COMPLETED STEPS 1 - 10.; [04] APPLIED CHEM CONV COATING ON PASS CAB SEAT TRACK BS480 - BS487; BS500 - BS500A; BS500A+10; BS500A+17; BS500B+8; BS500B; BS500C; BS500C+8; BS500D BS520. RBL45WL208 PER SOPM 20-43-03 TYPE 5; CLASS F; STEP F; [05] VERIFIED CHEMICAL CONVERSION COATING APPLIED ON PASS CABIN SEAT TRACK AT BS480 - BS487; BS500 - BS500A; BS500A+10; BS500A+17; BS500B+8; BS500B; BS500C; BS500C+8; BS500D BS520. RBL45 WL208 PER SOPM 20-43-03 TYPE 5; CLASS F; STEP F.; [06] APPLIED ALUMINIZED PRIMER ON PASS CAB SEAT TRACK BS480 - BS487; BS500 - BS500A; BS500A+10; BS500A+17; BS500B+8; BS500B; BS500C; BS500C+8; BS500D BS520. RBL45WL208 PER SRM 53-00-52-1A-1 STEPS 2. B. (2) AND SOPM 20-41-04 FIGURE 1 (SHEET 1 OF 3); [07] VERIFIED CORRECTIVE ACTION ENTRY 6. CARD COMPLETE

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS390; BS410 - BS428; BS440 - BS460. RBL45 WL208. MARKED ; / [01] UPDATED TABLE; [02] ACCOMPLISHED STEPS 1-3; [03] VERIFIED STEPS 1 - 3 ARE COMPLETE.; [04] APPLIED CHEMICAL CONVERSION COATING ON PASSENGER CABIN SEAT TRACK BS 410 - 428 RBL 45; WL 208 PER SOPM 20-43-03 TYPE 5; CLASS F; STEP F; [05] CORRECTED BS LOCATION IN PARTIAL UPDATE STEP 3.; [06] CERTIFY FOR UPDATE.; [07] APPLIED CHEMICAL CONVERSION COATING ON PASSENGER CABIN SEAT TRACK BS390; BS 410 - BS428; BS440 - BS460 RBL45 WL 208 PER SOPM 20-43-03 TYPE 5; CLASS F; STEP F; [08] CERTIFIED APPLIED CHEMICAL CONVERSION COATING ON PASSENGER CABIN SEAT TRACK BS390; BS 410 - BS428; BS440 - BS460 RBL45 WL 208 PER SOPM 20-43-03 TYPE 5; CLASS F; STEP F; [09] APPLIED ALUMINIZED PRIMER ON PASSENGER CABIN SEAT TRACK BS390; BS 410 - BS428; BS440 - BS460 RBL45 WL 208 PER SRM 53-00-52-1A-1 AND SOPM 20-43-04 FIGURE1 (SHEET 1 OF 3); [10] UPDATED STEP 3; [11] VERIFIED UPDATED STEP 3; [12] VERIFIED CORRECTIVE ACTION ENTRIES 9-10.; [13] VERIFIED CARD COMPLETE

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

R/H STRINGER 8 FRAME CRACKED BS 827 RBL 65 WL 273. ; / [01] UPDATED MEASUREMENTS TABLE.; [02] REPAIRED R/H STRINGER 8 FRAME AT BS 827 RBL 65 WL 273 PER EA 1-A53-12114 R7.; [03] COMPLETE; [04] ALL STEPS COMPLETE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

L/H STRINGER 8 FRAME CRACKED BS 440 LBL 65 WL 273. ; / [01] UPDATED MEASUREMENTS TABLE.; [02] REPAIRED L/H STRINGER 8 FRAME AT BS 440 LBL 65 WL 273 PER EA 1-A53-12114 R7.; [03] COMPLETE; [04] COMPLETE

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON PASSENGER CABIN CREASE BEAM BS714 LBL68 WL208. ; / [01] UPDATED TABLE; [02] REMOVED 1 EA FASTENER IN CREASEBEAM WEB STA 714; LBL 68; WL 208 FOR ACCESS PER SRM 51-40-02-0G-0.;[22] CREASE BEAM WEB REPLACED. ALL WORK ACCOMPLISHED.; [23] ADDED LBL 65 TO TABLE ALTHOUGH CORROSION WAS AT LBL 68.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

R/H STRINGER 8 FRAME CRACKED BS 787 RBL 65 WL 273. ; / [01] UPDATED MEASUREMENTS TABLE.; [02] REPAIRED R/H STRINGER 8 FRAME AT BS 787 RBL 65 WL 273 PER EA 1-A53-12114 R7.; [03] COMPLETE; [04] ALL STEPS COMPLETE.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

PASSENGER CABIN SEAT TRACK HAS CRACKED FASTENER BS727B RBL25 WL208. MARKED ; / [01] UPDATED TABLE; [02] CRACK FASTENER IN PASSENGER CABIN SEAT TRACK STA 727B; RBL 25; WL 208 WAS REPLACED ON SEAT TRACK REPLACEMENT ON CARD# TTG8Q006SPNJ; INTERIOR 1564; VERIFIED WITH SEAT TRACK FWD FASTENER INSPECTION CARD #TTG8Q00313NB; INT 1546.; [03] VERIFIED FASTENER AT BS 727B; RBL 25; WL 208; REPLACED ON FAULT# TTG8Q006SPNJ; VERIFIED FASTENER INSPECTION COMPLETE ON FAULT# TTG8Q00313NB

Part: NONE — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON FWD ENTRY DOOR CUTOUT LOWER SURFACE OF UPPER SILL WEB BS 307-312 AND BS 313-316 LBL 36 WL 284. ; / [01] VERIFIED APPLICABILITY OF SRM 53-10-15-0I-1 AND SRM 53-10-15-1A-1; [11] REPAIRED CORROSION ON FWD. ENTRY DOOR CUTOUT UPPER SILL WEB LOWER SURFACE AS PER EA# 21-153-03233/TTG8Q0099FX1.; [12] EDITED MEASUREMENTS 3 AND 4 OF MEASUREMENT TABLE TO REFLECT END BL.; [13] CERTIFIED CORRECTION.; [14] VERIFIED CORRECTIVE ACTIONS 11-13.<BR><BR>ACCOMPLISHED REPAIR PER EA# 21-153-03233

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON CABIN CREASE BEAM BS 713 LBL 69 WL 208. REMOVED 1 FASTENER IN THE CREASE BEAM WEB IAW SRM 51-40-02-0G-0. REMOVED CORROSION ON UPPER SURFACE OF CREASE BEAM WEB. AREA BLENDED IS 1' BY 1' IAW SRM 51-10-02-0G-0. EDDY CURRENT INSPECTED ON BLENDED AREA IAW NDT MANUAL PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND. CORROSION OUT OF LIMITS. CREASE BEAM REPLACED IAW CARD TTG8Q006SPMB.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS727B - BS762; BS776 - BS794; BS807 - BS827; BS840 - BS855; BS873 - BS887. LBL25 WL208. MARKED ; / [01] UPDATED TABLE; [10] INSTALLED NEW SEAT TRACK STA 727B-887; LBL 25; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-04-0G-0; DWG# 146A5300; REV A.; [11] VERIFIED CORRECTIVE ACTION 10.; [12] SEAT TRACK HAS BEEN REPLACED. ALL WORK ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS727B+3; BS727C+2; BS727D+11; BS727E+4; BS750; BS762; BS783 - BS795; BS811; BS824. LBL45 WL208. MARKED ; / [01] UPDATED TABLE; [02] SEAT TRACK WENT OUT OF LIMITS ON CARD#TTG8Q006SN6D AND WILL BE REPLACED ON CARD# TTG8Q006SN6D;; [03] VERIFIED STEPS 1-9. AND CORRECTIVE ACTION ENTRY 2.; [04] VERIFIED CARD COMPLETE

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS487; BS500+7; BS500A+17; BS500B - BS500B+8; BS500C+7; BS500D; BS520. RBL25 WL208. MARKED ; / [01] UPDATED TABLE;[25] REPLACED NEW PASSENGER CABIN SEAT TRACK BS 480 - 520 RBL 25 WL 208 PER DWG 143A5310 REV:A AND 143A5300 REV:A AND 143A5034 REV:A IAW SRM 51-40-02-0G-0 USED 75 IN-LB SCREWGUN ID:ATS2170 S/N:SP19K30738 DATE:01/2021 DUE:01/2022. USED TOURGE WRENCH ID:E11413 S/N:990737484; [26] JOB IS DONE; [27] VERIFIED ITEM 25 CORRECTIVE ACTIONS.; [28] VERIFIED ALL ITEMS COMPLETE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON CABIN SEAT TRACK BS 540 - 559, BS 564 - 592, BS 598 - 683, BS 685 - 709, BS 716 - 727+12, & BS 727A - 727B. LBL 25 WL 208. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1, & SRM 51-10-02-0G-0. REMOVED THE SEAT TRACK IAW SRM 51-40-02-0G-0. SEAT TRACK FABRICATED IAW DWG 144A5350. LOCATED & DRILLED THE NEW SEAT TRACK IAW SRM 51-40-05-0G-0, & DWG 144A5300. INSTALLED THE REPLACEMENT SEAT TRACK IAW SRM 51-40-02-0G-0, & DRAWING 144A5300, SHT 1, REV E.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON SEAT TRACK, BS 540 - 559, BS 570 - 589, BS 598 - 639, BS 645, BS 656 - 638, BS 727A - 727B LBL 45, WL208. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1, & SRM 51-10-02-0G-0. REMOVED THE SEAT TRACK IAW SRM 51-40-02-0G-0. LOCATED & DRILLED A NEW SEAT TRACK IAW SRM 51-40-05-0G-0, AND DWG 144A5300. INSTALLED THE REPLACEMENT SEAT TRACK IAW SRM 51-40-02-0G-0, AND DRAWING 144A5300 SHT 2 REV E.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS844; BS857; BS876; BS881; BS887. LBL45 WL208. MARKED ; / [01] UPDATED TABLE; [02] REMOVED CORROSION ON PASSENGER CABIN SEAT TRACK STA 844-887; LBL 45; WL 208. MAX MATERIAL REMOVED WAS .037' .5 BY 4'. OUT OF LIMITS PER SRM 53-00-52-1A-1; SRM 51-10-02-0G-0. MEASURED DEPTH WITH DIAL DEPTH GAUGE ID# NCX000697; S/N UNKNOWN; EXPIRES 07/2022.; [03] VERIFIED CORRECTIVE ACTION ENTRY 2.; [04] UPDATED STEP 6; [05] OK TO INSTALL SEAT TRACK AT BS 727B TO 887 LBL 45 WL 208; [06] VERIFIED CORRECTIVE ACTIONS STEP 6 AND OK TO INSTALL GIVEN.; [07] COMPLETED STEP 7; [08] VERIFIED STEP 7.; [09] VERIFIED INSTALLED NEW SEAT TRACK AT BS 727B - 887 LBL 45; WL 208 PER SRM 51-40-02-0G-0; BOEING DWG# 146A5300 REV A; [10] MAINTENANCE IS COMPLETE.; [11] MAINTENANCE IS COMPLETE; [12] VERIFIED COMPLETE INSTALLATION STEP 7.; [13] VERIFIED ALL INSPECTION ITEMS ARE COMPLETE.

Part: NONE — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON B.S. 1016 CHORD BETWEEN STRINGERS 25 LEFT AND 25 RIGHT; W.L. 190. ; / [01] EVALUATED CORROSION ON CHORD SPLICE; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [10] INSPECTED ACTION 9; OK TO INSTALL; [11] INSTALLED BS 1016 CHORD B/W STR 26L-26R WL 190 IAW SRM 51-40-02-0G-0; DWG# 148A0070.; [12] TORQUE WRENCH ID #3274D; SN: 1298502641; CAL DATE: 11/2021; [13] VERIFIED CORRECTIVE ACTIONS 11 AND 12.; [14] INSTALLED STR 27L AND STR 27R STR END FITTINGS; APPLIED FILLET SEAL TO ALL AREAS; AND APPLIED CIC TO AREA; IAW SRM 51-40-02-0G-0; SRM 51-40-04-0G-0; DWG# 148A0070.

Part: NONE — CORRODED (R2 DOOR) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON AFT SERVICE DOOR EXTERIOR HANDLE ASSY PAN ; / [01] UPDATED MEASUREMENT TAB; [02] UPDATED MEASUREMENT TAB; [03] CORROSION ON AFT SERVICE DOOR EXTERIOR HANDLE ASSY PAN WAS REPAIRED ON CUSTOMER RO NO P1540381-1 AND JOB# 543578; [04] VERIFIED AFT SERVICE DOOR WAS REPAIRED ON CUSTOMER RO NO P1540381-1 AND JOB# 543578 SEE ATTACHMENT.

Part: FLANGE — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON PREVIOUS UPPER FLANGE REPAIR BS 986 AT LBL 42 WL 208 AT NUTPLATE HOLES. ; / [01] REMOVED NUTPLATE BS986 LBL42 WL208 I.A.W SRM 51-40-02-0G-0; [02] NO ALLOWABLE LIMITS FOUND FOR PREVIOUS REPAIR ON SRM. DAMAGED UPPER FLANGE OF BS986 FLOOR BEAM TO BE REMOVED AND CONTACT ENGINEERING FOR REPAIR PROCEDURES; [28] REMOVED AND REPLACED BS986 FLOOR BEAM REPAIR LBL3-LBL50 WL 208 PER 737-700 SRM 51-40-02-0G-0 AS SHOWN IN SWA EA-1-753-33330 REV IR; [29] VERIFIED CORRECTIVE ACTION 28.; [30] VERIFIED ALL INSPECTION ITEMS ARE COMPLETE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON SUPPORT INTERCOSTAL AT B.S. 259+3 - 259+8; L.B.L 3 - R.B.L. 3; W.L.207.54. REMOVED CORROSION ON SUPPORT INTERCOSTAL. FOUND TO BE OUT LIMITS ALL IAW SRM 51-10-02-0G-0, AND SRM 53-10-51-1A-1, ALLOWABLE DAMAGE 1 FIG 104 GROUP 2 PAR 4.B (2) (A) DETAIL C & E. REMOVED SUPPORT INTERCOSTAL AND LOCATED, DRILLED AND INSTALLED THE NEW SUPPORT INTERCOSTAL IAW DWG 141A5210, SRM 51-10-05-0G-0 AND SRM 51-40-02-0G-0.

Part: FLANGE — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON PREVIOUS UPPER FLANGE REPAIR BS 986 RBL 42 - RBL 35 WL 208 AT NUTPLATE HOLES. ; / [01] REMOVED NUTPLATE BS986 LBL42 WL208 I.A.W SRM 51-40-02-0G-0;21] INSTALLED FLOOR SUPPORT BS986-BS1006 RBL45 WL 208 REMOVED FOR ACCESS ON CORRECTIVE ITEM 6 I.A.W BOEING DWG 147A0000 AND SRM 51-40-02-0G-0; [22] INSTALLED FLOOR SUPPORT BS967-BS986 RBL17 WL 208 REMOVED FOR ACCESS ON CORRECTIVE ACTION 7 I.A.W BOEING DWG 140A9870 SRM 51-40-02-0G-0; [23] VERIFIED CORRECTIVE ACTION 21 AND 22.; [24] INSTALLED INTERCOSTAL BS986-BS1006 RBL38 WL 208 REMOVED FOR ACCESS ON CORRECTIVE ACTION 5 I.A.W BOEING DWG 147A5730;SRM 51-40-02-0G-0; [25] INSTALLED FASTENER BS967-BS1006 RBL0-RBL50 WL 208 I.A.W SRM 51-40-02-0G-0 AS SHOWN IN SWA EA-1-753-33330 REV IR; [26] VERIFIED CORRECTIVE ACTION 24.; [27] INSTALLED FASTENER BS967-BS1006 RBL0-RBL50 WL 208 I.A.W WHERE THE FASTENER ARE COMMON TO REPAIR RECORD ON CORRECTIVE ACTION 4 SRM 51-40-02-0G-0 AS SHOWN IN SWA EA-1-753-33330 REV IR;

Part: NONE — OUT OF TOLERANCE (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

AFT CARGO BAY FLOOR SUPPORT RAIL HAS BONUS HOLE AT 767+5 RBL 3 WL156 ; / [01] DAMAGE ON ACB FLOOR SUPPORT RAIL BS 767+5; RBL 3; WL 156 FOUND TO BE OUT OF LIMITS DUE TO 100% MATERIAL LOSS IAW SRM 53-00-53-1A-2; [02] CUT OUT DAMAGE ON ACB FLOOR SUPPORT RAIL BS 767+8; RBL 3; WL 156; CUT OUT 2.9'X.8'; IAW SRM 53-00-53-2R-2.; [03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.; [04] EDDY CURRENT INSPECTED DAMAGE CUT OUT AND SURROUNDING AREA IN ACCORDANCE WITH 737 NDT MANUAL; PART 6; PROCEDURE 23. NO CRACKS NOTED.<BR><BR>TOOL I.D. ATS279 (OLYMPUS NORTEC 500D); [05] TRIMMED; LOCATED; DRILLED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING; AND PRIMED CHANNEL FOR ACB FLOOR SUPPORT RAIL BS 767+5; RBL 3; WL 156. MADE FROM BAC1510-1355; PO #824811. OK TO INSTALL CHANNEL.; [06] VERIFIED CORRECTIVE ACTION STEP 5. VERIFIED OK TO INSTALL CHANNEL.; [07] INSTALLED REPAIR CHANNEL ON ACB FLOOR SUPPORT RAIL BS 767+5; RBL 3; WL 156; APPLIED FILLET SEAL AND CIC IAW SRM 53-00-53-2R-2.; [08] VERIFIED CORRECTIVE ACTION ENTRY 7.; [09] VERIFIED CARD COMPLETE.

Part: NONE — CORRODED (R2 DOOR) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON AFT SERVICE DOOR EXTERIOR HANDLE ASSY CAM FOLLOWER. ; / [01] UPDATED MEASUREMENT TAB; [02] CORROSION ON AFT SERVICE DOOR EXTERIOR HANDLE ASSY CAM FOLLOWER WAS REPAIRED ON CUSTOMER RO NO P1540381-1 AND JOB# 543578; [03] CORROSION ON AFT SERVICE DOOR EXTERIOR HANDLE ASSY CAM FOLLOWER WAS REPAIRED ON CUSTOMER RO NO P1540381-1 AND JOB# 543578; [04] VERIFIED AFT SERVICE DOOR WAS REPAIRED ON CUSTOMER RO NO P1540381-1 AND JOB# 543578 SEE ATTACHMENT.

Part: GUIDE ARM — CORRODED (L2 DOOR) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON AFT ENTRY DOOR GUIDE ARM; GUIDE TRACK ; / [01] REMOVED AFT ENTRY DOOR GUIDE ARM AND ROLLER PER MM 52-13-21-000-802; [02] REMOVED AFT ENTRY DOOR; UPPER HINGE FITTING; FUSELAGE SIDE PER MM 52-13-41-000-801; [03] UPDATED MEASUREMENTS TAB; [04] CORROSION DAMAGE ON AFT ENTRY DOOR GUIDE ARM; LOWER GUIDE TRACK WAS FOUND TO BE REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-0G-0 PAR 9C; [05] REMOVED DAMAGED AFT ENTRY DOOR GUIDE ARM; LOWER GUIDE TRACK PER SOPM 20-50-01; [06] CORRECTION TO DISCREPANCY CORROSION IS ON LWR TRACK; [07] INSTALLED NEW AFT ENTRY DOOR GUIDE ARM; LWR GUIDE TRACK PER SOPM 20-50-01 AND BOEING DRW 147A6104; [08] VERIFIED CORRECTIVE ACTION STEPS 3;4;5;6 AND 7.; [09] ACCOMPLISHED PARTIAL ON STEP 2; [10] CAP SEALED NUTS ON AFT ENTRY DOOR GUIDE ARM; LOWER GUIDE TRACK PER MM 51-31-00-390-805; [11] PARTIAL STEP 2 REINSTALLED AFT ENTRY DOOR; UPPER HINGE FITTING; FUSELAGE SIDE PER MM 52-13-41-400-801; [12] VERIFIED CORRECTIVE ACTION ENTRIES 9. THRU 11.; [13] VERIFIED STEP 2 COMPLETE; [14] COMPLETED STEP 1; INSTALLATION OF AED GUIDE ARM/ROLLER ASSY DOCUMENTED ON TASK ID: TTG8Q006ZCRL<BR>AED TORQUE TUBE ACCESS PANEL 241AL REMOVAL/INSTALLATION DOCUMENTED ON CARD ID: TTG8Q006ZCRE; [15] COMPLETED PART REQUIREMENT BLOCK; [16] VERIFIED ITEM 14 CORRECTIVE ACTIONS.; [17] UPDATED TABLE; [18] VERIFIED

Part: NONE — CORRODED (L2 DOOR) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON AFT ENTRY DOOR; EXTERIOR HANDLE ASSY PAN. ; / [01] AED EXTERIOR HANDLE PAN REMOVED AND REPLACED PER SRM 51-40-02-0G-0; REFERENCING BOEING DWG 147A6116. WORK ACCOMPLISHED ON ATS COMPONENTS WORK ORDER RO# P1540486-1.; [02] VERIFIED STEP 1.; [03] VERIFIED ITEM 1 CORRECTIVE ACTIONS.

Part: BEAM — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON B.S.270 LATERAL BEAM AT L.B.L 9; L.B.L. 6; L.B.L. 4; R.B.L. 3 AND R.B.L. 9; W.L. 207.54. ; / [01] REMOVED FASTENER ON BS270 RBL9-LBL9 WL208 I.A.W SRM 51-40-02-0G-0; [08] DAMAGE ON BS270 LATERAL BEAM FROM LBL9-RBL9 WL207.5 18'X1' AREA FOUND TO BE OUT LIMITS I.A.W SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 FIG 104 GROUP 3 PAR 4.C(2)(A)DETAIL C;E LATERAL BEAM TO BE REPAIRED PER M-21-153-00277 ATTACHED ON COSTUMER CARD TTG8Q006SX2U; [09] INSTALLED 100% TEMPORARY AND PERMANENT FASTENER BEFORE SQUEEZE OUT TIME ON REPAIR AREA BS249-BS270 WL 207.5 RBL10-LBL10 I.A.W SOPM 20-50-19.

Part: NONE — CORRODED (L2 DOOR) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON AFT ENTRY DOOR; EXTERIOR HANDLE ASSY; CAM FOLLOWER. ; / [01] REMOVED AND REPLACED AED EXTERIOR HANDLE CAM FOLLOWER PER CMM 52-15-16; PG 704; PARAGRAPH 2.D.(5) AND (6).<BR>WORK ACCOMPLISHED ON ATS COMPONENTS WORK ORDER RO# P1540486-1.; [02] VERIFIED STEP 1.; [03] VERIFIED ITEM 1 CORRECTIVE ACTIONS.

Part: NONE — CORRODED (R2 DOOR) · airframe 68,861 hrs · 40,837 cycles

CORROSION ON AFT SERVICE DOOR; EXTERIOR HANDLE ASSY; CAM. ; / [01] UPDATED MEASUREMENT TAB; [02] CORROSION ON AFT SERVICE DOOR; EXTERIOR HANDLE ASSY; CAM WAS REPAIR ON CUSTOMER RO NO P1540381-1 AND JOB# 543578; [03] VERIFIED AFT SERVICE DOOR WAS REPAIRED ON CUSTOMER RO NO P1540381-1 AND JOB# 543578 SEE ATTACHMENT.

Part: DOOR — CORRODED (CABIN) · airframe 68,861 hrs · 40,837 cycles

LAV SERVICE DOOR HAS CORROSION ON LOWER FWD CORNER ON EXTERIOR SIDE OF DOOR ; / [01] EVALUATED CORROSION ON LAV SERVICE DOOR; FOUND 0.030 REMOVED FROM ORIG 0.100 IN 3'X2' AREA; FOUND TO BE OUT OF LIMITS PER SRM 52-40-01-1A-4 USING DIAL DEPTH GAUGE ID NCX000697 S/N UNKNOWN; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [03] REPLACED LAV SERVICE DOOR IAW MM 52-49-07-000-801;MM 52-49-07-400-801 USED BONDING METER ID# ATS1257 S/N DC003961 BOND CHECK GOOD; [04] VERIFIED CORRECTIVE ACTION ITEM 3.

Part: SUPPORT — CORRODED (BS 400) · airframe 68,861 hrs · 40,837 cycles

R/H FLOOR TO SIDEWALL SUPPORT CORRODED AROUND FASTENER HOLES BS 400+6; 400+10; RBL 25; WL 156 ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 400+6 RBL 25 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ID NCX000697 S/N UNKNOWN; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [03] FABRICATED; LOCATED AND DRILLED NEW R/H FLOOR TO SIDEWALL SUPPORT BS 396 TO 420 RBL25; WL156 FROM EXTRUSION BAC1496-444#7075T62 CLAD; LOT# 1467644-1 PER SRM 51-40-05-0G-0;DWG 142A7500 AND DWG 143A7501; [04] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON R/H FLOOR TO SIDEWALL SUPPORT BS 396 TO 420 RBL25; WL 156 PER AMM 51-21-41-370-802; AND AMM 51-21-72-370-804. INSTALLED NUTPLATES PER SRM 51-40-02-0G-0 AND DWG 143A7501; [05] VERIFIED STEPS 3 AND 4 COMPLETE; [06] VERIFIED ALL STEPS COMPLETE; [07] INSPECTED ACTION 3;4; [08] INSPECTION COMPLETE

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

WATER SERVICE PAN UPPER SURFACE AFT SUPPORT ANGLE CRACKED (BS 907+11; RBL 14) ; / [01] EVALUATED CRACK; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION 1; [03] REMOVED WATER SERVICE PAN; AFT CRACKED SUPPORT ANGLE; BS 907+11; RBL-14. IAW SRM 51-40-02-0G-0.; [04] LOCATED; DRILLED AND DEBURRED NEW WATER SERVICE PAN SUPPORT ANGLE BS 907+11; RBL7-RBL18 IAW SRM 51-40-05 AND DWG# 147A7221. OK TO INSTALL.; [05] VERIFIED CORRECTIVE ACTION 4; OK TO INSTALL GIVEN.; [06] INSTALLED NEW WATER SERVICE PAN SUPPORT ANGLE BS 907+11; RBL7-RBL18 IAW SRM 51-40-02 AND DWG# 147A7221.; [07] VERIFIED CORRECTIVE ACTION ITEM 6.; [08] VERIFIED TASK IS COMPLETE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

AFT CARGO BAY SHEAR TIE CORRODED BS 847 S26 - 27L, WL 153. EVALUATED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED ACB SHEAR TIE IAW SRM 51-40-02. LOCATED, DRILLED AND PRIMED IAW DWG 146A3230, 146A1202 AND SRM 51-40-05-0G-0. INSTALLED THE SHEAR TIE IAW SRM 51-40-02-OG-O, DWG146A3230 AND DWG 146A1281.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO BAY SUB THRESHOLD CORRODED AROUND FASTENER HOLES BS 440+33; 440+33; RBL 29; WL 156 ; / [01] AFTER FURTHER INVESTIGATION; FOUND CORROSION ON SUB THRESHOLD WEB TO BE AT BS 440+33 AND BS 440+39; [02] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DIAL DEPTH GAUGE ID NCX000697 S/N UNKNOWN; [03] VERIFIED CORRECTIVE ACTION ITEM 1 & 2.; [04] RECEIVED NEW SUB THRESHOLD WEB PER P.O.#837311. LOCATED ; DRILLED ; DEBURRED AND INSTALLED NUT PLATES PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 143A8330.; [05] VERIFIED CORRECTIVE ACTION ENTRY 4.; [06] VERIFIED CARD COMPLETE

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

AFT CARGO BAY SHEAR TIE CORRODED BS 727C; S25L - 26L; WL 149. EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED SHEAR TIE IAW SRM 51-40-02. LOCATED, DRILLED AND PRIMED NEW SHEAR TIE IAW DWGS 146A3230, 146A1281 AND SRM 51-40-05-0G-0. INSTALLED NEW SHEAR TIE IAW SRM 51-40-02-OG-O, DWG 146A3230 AND DWG 146A1202.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

FWD CARGO BAY FWD SHIELD CORRODED AROUND FASTENER HOLES BS 420+9; BS 420+12.5; RBL 25; WL 156 ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [03] DRILLED NEW R/H FLOOR TO SIDEWALL SUPPORT BS TO 420 440 RBL25; WL156 PER SRM 51-40-05-0G-0 N/P 143A8126-21 AND DWG 143A0080; [04] UPDATED PARTS AND VERIFIED ALL STEPS COMPLETE; [05] INSPECTION COMPLETE

Part: SHIELD — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

AFT CARGO BAY FWD SHIELD CORRODED AROUND FASTENERS HOLES BS 767+1; 767+3; 767+7; 767+11; 767+15; RBL 22; WL 156 ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION 1; [03] RECEIVED NEW ACB FWD SHIELD BS 767-787; RH; LOCATED AND DRILLED NEW SHIELD; BS767-787; IAW SRM 51-40-05-0G-0; DWG146A0081; [04] VERIFIED CORRECTIVE ACTION ITEM 3.; [05] VERIFIED COMPLETE

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

AFT CARGO BAY STRINGER CLIP CORRODED BS 747, S26R, WL 150. REMOVED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, LOCATED AND DRILLED A NEW STRINGER CLIP IAW 51-40-05-0G-051-40-02-0G-0 AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG 146A1260.

Part: SUPPORT — CORRODED (BS 420-500C) · airframe 68,861 hrs · 40,837 cycles

FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT CORRODED BS 420+10; 420+13; 440+10; 440+14; 460+6; 460+10; 500+10; 500B+14; 500C+6; RBL 25; WL 156 ; / [01] AFTER FURTHER INVESTIGATION; L/H FLOOR TO SIDEWALL SUPPORT IS LBL 25; NOT RBL 25. EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 440+10 LBL 25 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53--1A-2 USING DIAL DEPTH GAUGE ID NCX000697 S/N UNKNOWN; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [03] RECEIVED NEW FCB LH FLOOR TO SIDEWALL SUPPORT; LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT; BS 396- 500D; LH IAW SRM 51-40-05-0G-0; DWG143A7500.; [04] VERIFIED ACTION 3; [05] INSPECTION COMPLETE

Part: SUPPORT — CORRODED (BS 727A-787) · airframe 68,861 hrs · 40,837 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT CORRODED AROUND FASTENERS HOLES BS 727A+18; 727C+10; 727E+6; 727E+10; 727E+14; 747+4; 747+10; 767+3 - 767+11; 787+7; 787+11; LBL 22; WL 156 ; / [01] EVALUATED CORROSION AT ALL LOCATION; FOUND DEEPEST LOCATION TO BE AT BS 747+10 LBL 22 WL 156; FOUND 0.015 REMOVED FROM ORIGINAL 0.040 IN A 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ID NCX000697 S/N UNKNOWN; [02] VERIFIED CORRECTIVE ACTION 1; [03] RECEIVED NEW ACB LH FLOOR TO SIDEWALL SUPPORT; PO#839533; LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT; IAW SRM 51-40-05-0G-0; DWG 146A7500; [04] VERIFIED CORRECTIVE ACTION ENTRY 3. CARD COMPLETE.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

FWD CARGO BAY AFT SHIELD CORRODED BS 500+1; 500+6; 500+17; RBL 25; WL 156 ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [03] LOCATED; DRILLED AND DEBURRED NEW FCB AFT SHIELD FROM BS 490-500A IAW SRM 51-40-05 AND DWG #143A0080.; [04] VERIFIED LOCATED; DRILLED AND DEBURRED NEW FCB AFT SHIELD FROM BS 490-500A IAW SRM 51-40-05 AND DWG #143A0080.; [05] ALL AMT STEPS COMPLETE

Part: SUPPORT — CORRODED (BS 727A-747) · airframe 68,861 hrs · 40,837 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT CORRODED AT FASTENER HOLES BS 727A+14; 727B+10; 727C+14; 727E+2; 727E+6; 727E+10; 727E+14; 727E+18; 747+2; 747+7 RBL 22; WL 156 ; / [01] EVALUATED CORROSION AT ALL LOCATION; FOUND DEEPEST LOCATION TO BE AT BS 727E+14 RBL 22 WL 156; FOUND 0.015 REMOVED FROM ORIGINAL 0.040 IN A 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ID NCX000697 S/N UNKNOWN; [02] VERIFIED CORRECTIVE ACTION 1; [03] RECEIVED NEW PART ON PO# 830535; LOCATED AND DRILLED NEW RH FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-05-0G-0; DWG146A7500;; [04] VERIFIED CORRECTIVE ACTION ENTRY 3.; [05] VERIFIED CARD COMPLETE

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT CORRODED AT FASTENER HOLES BS 727A+14; 727B+10; 727C+14; 727E+2; 727E+6; 727E+10; 727E+14; 727E+18; 747+2; 747+7 ; / [01] FAULT LOCATION INCOMPLETE. FAULT TO BE CORRECTED ON FAULT #TTG8Q006RD3S

Part: RAIL — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

AFT CARGO BAY RAIL HAS ELONGATED HOLE BS 727+8; LBL 7; WL 156 ; / [01] DAMAGE FOUND ON ACB RAIL BS 727+8; LBL 7; WL 156 FOUND TO BE OUT OF LIMITS DUE TO 100% MATERIAL LOSS IAW SRM 53-00-53-1A-2.; [11] INSTALLED NEW ACB RAIL AND REPAIR CHANNEL BS 727+4-BS 727B+12; LBL 7; WL 156; APPLIED FILLET SEAL TO SPLICE AND CIC IAW SRM 53-00-53-2R-2.; [12] VERIFIED INSTALLED NEW ACB RAIL AND REPAIR CHANNEL BS 727+4-BS 727B+12; LBL 7; WL 156; APPLIED FILLET SEAL TO SPLICE AND CIC IAW SRM 53-00-53-2R-2.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

AFT CARGO BAY STIFFENER ANGLE CORRODED BS 794, RBL 21; WL 153. EMOVED DAMAGE ON ACB STIFFENER ANGLE BS 794 RBL21 WL 153 IAW SRM 51-10-02. REMOVED DAMAGE IN AN AREA OF 1'X1' ON ACB STIFFENER ANGLE BS 794 RBL 21 WL 153 IAW SRM 51-10-02. FOUND TO BE WITH IN LIMITS IAW SRM 53-60-15-1A-1 AND DWG 146A8205. VERIFIED CORRECTIVE ACTION 8 (IN LIMITS). APPLIED CHEMICAL CONVERSION COATING AND PRIMERED BARE METAL ON ACB STIFFENER ANGLE BS794 RBL21 WL 153 IAW SRM 51-20-01.

Part: SUPPORT — CORRODED (BS 500B-500C) · airframe 68,861 hrs · 40,837 cycles

FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT CORRODED BS 500B+19; 500C+13; 500C+15; RBL 25; WL 156 ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500B+19 RBL 25 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ID NCX000697 S/N UNKNOWN; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [03] FABRICATED; LOCATED; DRILLED;APPLIED CHEMICAL CONVERSION COATING; PRIMED AND INSTALLED NUTPLATES TO NEW R/H FLOOR TO SIDEWALL SUPPORT BS 500A-500D RBL25; WL156 FROM EXTRUSION BAC1496-444#7075T62 CLAD; LOT# 1467644-1 PER SRM 51-40-05-0G-0;DWG 142A7500 AND DWG 143A7501; [04] VERIFIED STEP 3 COMPLETE; [05] VERIFIED ALL STEPS COMPLETE; [06] INSPECTED AND VERIFIED ACTION3;4; [07] INSPECTION COMPLETE

Part: RIB — CRACKED (RH HOR STAB) · airframe 68,861 hrs · 40,837 cycles

RT HORIZ. STAB REMOVABLE L/E RIB AT L/E STA 300.51 IS CRACKED. INSTALLED BS 300.51 R/H L/E RIB IAW SRM 51-40-02 AND BOEING DWG 186A1001.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

FWD CARGO BAY BS 500D STR19L GUSSET IS CRACKED ; / [01] REMOVED FCB GUSSET BS500D STR19L IAW SRM 51-40-02.; [02] LOCATED; DRILLED AND DEBURRED NEW GUSSET @ BS 500D STR19L IAW SRM 51-40-05. OK TO INSTALL.; [03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2. VERIFIED OK TO INSTALL.; [04] INSTALLED NEW GUSSET IN FCB @ BS 500D STR19L IAW SRM 51-40-02 AND DWG #143A7902.; [05] VERIFIED CORRECTIVE ACTIONS 4

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

FWD CARGO BAY BS 500D STR19R GUSSET IS CRACKED ; / [01] REMOVED FCB GUSSET BS500D STR19R IAW SRM 51-40-02.; [02] LOCATED DRILLED AND DEBURRED NEW GUSSET @ BS 500D STR19R IAW SRM 51-40-05. OK TO INSTALL.; [03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2. VERIFIED OK TO INSTALL.; [04] INSTALLED NEW GUSSET IN FCB @ BS 500D STR19R IAW SRM 51-40-02 AND DWG #143A7902.; [05] VERIFIED CORRECTIVE ACTIONS 4

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED. WELDED CRACKED RADIUS OF ACB; FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1 PARA 4.B.(2) AND (4). FLUORESCENT DYE PENETRANT INSPECTED REPAIR AREA IN ACCORDANCE WITH SOPM 20-20-02 METHOD C. NO DEFECTS NOTED. SANDED REPAIR WELD SMOOTH PER SRM 53-60-15-2R-1 PARA 4.B.(5). APPLIED CHEMICAL CONVERSION COATING AND PRIMED REPAIRED AREA PER SRM 53-60-15-2R-1.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

FWD CARGO BAY BS 500D STR21L GUSSET IS CRACKED ; / [01] REMOVED FCB GUSSET BS500D STR21L IAW SRM 51-40-02.; [02] LOCATED; DRILLED AND DEBURRED NEW GUSSET @ BS500D STR21L IAW SRM 51-40-05. OK TO INSTALL.; [03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2. VERIFIED OK TO INSTALL.; [04] INSTALLED NEW GUSSET IN FCB @ BS 500D STR21L IAW SRM 51-40-02 AND DWG #143A7902.; [05] VERIFIED CORRECTIVE ACTIONS 4

Part: PLATE — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORROSION IN FWD SERVICE DOOR GUIDE PLATE TRACKS. REMOVED DAMAGED FWD SERVICE DOOR GUIDE PLATE, UPPER HINGE LOWER TRACK AND INSTALL A NEW TRACK IAW SOPM 20-50-01 AND DWG 141A6504. CORROSION DAMAGE ON FWD SERVICE DOOR GUIDE PLATE TRACKS UPPER AND LOWER WERE FOUND TO BE REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-0G-0 STEP 9C. REMOVED AND REPLACED FSD UPPER HINGE, UPPER GUIDE PLATE IAW SOPM 20-50-01, REFERENCING DWG 141A6504, SHEET 1. INSTALLED GUIDE ARM ROLLER ASSY. RESTORED TORQUE TUBE ASSY. SEAL FASTENERS FOR LOWER GUIDE PLATE.

Part: RIB — CRACKED (RH HOR STAB) · airframe 68,861 hrs · 40,837 cycles

RT HORIZ. STAB REMOVABLE L/E RIB IS CRACKED AT L/E STA 309.00. INSTALLED HSS 309.00 RT L/E RIB IAW SRM 51-40-02 AND DWG 186A1001.

Part: BEAM — CRACKED (R1 DOOR) · airframe 68,861 hrs · 40,837 cycles

FORWARD SERVICE DOOR #4 BEAM; I/B FWD SIDE CRACKED APROX. 1.500' IN LENGTH. ; / [01] FORWARD SERVICE DOOR #4 BEAM WAS REPLACED ON CUSTOMER RO NO P1513410-1; AND JOB# 543364; [02] VERIFIED FSD #4 BEAM WAS REPLACED ON CUSTOMER RO NO P1513410-1; AND JOB# 543364

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 68,861 hrs · 40,837 cycles

LT HORIZ. STAB REMOVABLE L/E RIB IS CRACKED T L/E STA 78.29. ; / [01] REMOVED AND REPLACED CRACKED LT. HORIZ. STAB REMOVABLE L/E RIB AT L/E STA 78.29 IAW SRM 51-40-02-0G-0 STEP 4 AND DWG # 186A1001.; [02] INSPECTED ACTION 1

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,861 hrs · 40,837 cycles

CORRODED STRINGER AT B.S. 520+17; STRINGER 23 LEFT. FOUND 0.020 REMOVED FROM 0.036; IN AREA OF 1'X1' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1. CUT OUT STRINGER SECTION BS 500D+11'- BS 520+18' STR 23 L IAW SRM 53-00-03-2R-1; STEP 4-B. INSTALLED NEW STRINGER SECTION AND HAT SECTION IAW SRM 53-00-03-2R-1, DWG 143A3210, AND DWG 143A0060. THE DAMAGE WAS REPAIRED IAW SRM 53-00-03-2R-1 (REPAIR 1) AND EA 21-153-02933.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 68,618 hrs · 40,683 cycles

RT SIDE OVERWING EXIT DOOR SIDEWALL LIGHT INOP. CLOSING DMA REFERENCE 0087709 R & R RT OVERWING EMERGENCY EXIT DOOR BALLAST IAW AMM 33-51-04 CLOSING# 31027.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,169 hrs · 40,373 cycles

EMERGENCY LIGHT BATTERY PACKS AT LOCATION M01668 FAILED CAPACITANCE CHECK. / R&R BATTERY PACKS PER DWG.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 68,169 hrs · 40,373 cycles

LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER 53-31-31.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,169 hrs · 40,373 cycles

EMERGENCY LIGHT BATTERY PACKS AT LOCATION M01669 FAILED CAPACITANCE CHECK. / R&R BATTERY PACKS PER DWG.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 68,169 hrs · 40,373 cycles

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

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD BORE CORRODED. REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD BORE CORRODED. REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD BORE CORRODED. REPAIRED LUG FACE PER EA.

Part: FITTING — CORRODED (R/H MLG) · airframe 67,109 hrs · 39,688 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING UPPER INBD HAT SIDE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 REPAIR 2

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD LUG FACE CORRODED. REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD BORE CORRODED. REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG FACE CORRODED. REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG FACE CORRODED. REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD LUG FACE CORRODED. REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG FACE CORRODED. REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD BORE CORRODED. REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD BORE CORRODED. REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD BORE CORRODED. REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG FACE CORRODED. REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD BORE CORRODED. REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG FACE CORRODED. REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,109 hrs · 39,688 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG FACE CORRODED. REPAIRED LUG FACE PER EA.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 66,172 hrs · 39,088 cycles

R/H WING JUST AFT OF #2 PYLON UPPER SHELF PANEL SEAL RETAINER IS CRACKED. / REMOVED AND REPLACED SEAL RETAINER BRACKET IAW SRM 51-40-02

Part: PANEL — ELONGATED · airframe 65,414 hrs · 38,612 cycles

TRANSFERRED FROM N/R #D365840: WING TO BODY FAIRING PANEL 193B HAS ELONGATED FASTENER HOLES AT LOCATIONS 9-11;13;15-19;23-25;28;34-38 MOD / R&R THE 193B PANEL PER AMM 53-51-21

Part: CONTROL LEVER — CRACKED (COCKPIT) · airframe 65,250 hrs · 38,502 cycles

NR 2 ENGINE THROTTLE LEVER CRACKED 1/4" IN LENGTH. REPAIRED LEVER PER EA.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 64,884 hrs · 38,243 cycles

L2 DOOR EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 64,884 hrs · 38,243 cycles

R2 DOOR EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MT.

Part: COVER — UNSECURE (CABIN) · airframe 64,623 hrs · 38,057 cycles

RT EXIT LIGHT COVER FELL OFF. R&R EXIT LIGHT COVER PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 64,063 hrs · 37,670 cycles

LT AFT DOOR EMERGENCY LIGHT FAILED CAPACITY CHECK. R&R BATTERY PACK PER AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 64,053 hrs · 37,666 cycles

AFT GALLEY EMERGENCY FLASHLIGHT INOP. R&R BATTERY PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,037 hrs · 37,654 cycles

AFT GALLEY DOOR UPPER EMERGENCY LIGHT BULB INOP. R&R BULB PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,037 hrs · 37,654 cycles

EMERGENCY BATTERY PACK INOP AT M1672. R&R BATTERY PACK PER AMM.

Part: HOUSING — DAMAGED (CABIN) · airframe 64,037 hrs · 37,654 cycles

UPPER CENTER EMERGENCY EXIT LIGHT HOUSING DAMAGED AT OVERWING EXIT AREA. R&R LIGHT IAW AMM.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 64,037 hrs · 37,654 cycles

AFT LAV SHEAR WEB COMMON TO AFT ENTRY DOOR MOPSILL CRACKED BETWEEN BS 986 TO BS 1016. R&R SHEAR WEB IAW DWG AND SRM.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 64,037 hrs · 37,654 cycles

LT LOWER VAPOR BARRIER CRACKED AT LBL 25. REPAIRED BARRIER PER SRM.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 64,037 hrs · 37,654 cycles

LT LOWER VAPOR BARRIER CRACKED AT LBL 25. REPAIRED BARRIER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,037 hrs · 37,654 cycles

FRAME CRACKED AT BS 294.5, RBL 65. REPAIRED FRAME IAW EA & ER.

Part: BEAM — CRACKED (LEFT WING) · airframe 64,037 hrs · 37,654 cycles

TE SUPPORT BEAM FOR PANEL 561AB IS CRACKED / REMOVED AND REPLACED TE SUPPORT BEAM FOR PANEL 561AB IAW SRM 51-40-02-0G-0 548403U 24AUG18

Part: FAIRING — CRACKED (RIGHT WING) · airframe 64,037 hrs · 37,654 cycles

RT WING FLAP TRACK AFT FAIRING 644BB HAS A CRACK AT THE FWD L/E. / REPAIRED CRACKS AT FWD LE OF RT WING FLAP TRACK AFT FAIRING 644BB IAW SRM 57-53-70; SRM 57-53-70-2R-1; SRM 51-70-05-2R-6; SRM 51-40-02; AMM 51-21-71

Part: FLOOR PANEL — DAMAGED (E & E COMPT) · airframe 64,037 hrs · 37,654 cycles

E-BAY FLOOR PANEL # 284A6813-5 HAS A DAMAGED INSERT ON OUTBOARD EDGE OF PANEL (MARKED) / E-BAY PANEL P/N 284A6813-5; REMOVED DAMAGED INSERT; REPAIRED THE PANEL AND INSTALLED NEW INSERT PER SRM 53-10-54 REPAIR 1 AND SRM 53-00-50 REPAIR 4. 57543U 23AUG.18

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 64,037 hrs · 37,654 cycles

R1 DOOR MOP SILL CORRODED BETWEEN BS 294 TO BS 328, RBL 55. R&R MOPSILL IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (L1 DOOR) · airframe 64,037 hrs · 37,654 cycles

L1 DOOR MOP SILL SUPPORT ANGLE CORRODED AT BS 318, LBL 64. R&R ANGLE PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,037 hrs · 37,654 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 43 TO RBL 45. REPAIRED FLOORBEAM PER ER AND EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 64,037 hrs · 37,654 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R SUPPORT IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 64,037 hrs · 37,654 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS 727B+12 TO BS 887, LBL 45. R&R SEAT TRACK IAW SRM & DWG.

Part: ANGLE — CORRODED (FSD THRESHOLD) · airframe 64,037 hrs · 37,654 cycles

***CORROSION*** FWD SERVICE DOOR MOP SILL ATTACH ANGLE AROUND NUT PLATES BS 300 324 RBL56 WL208. / REMOVED AND REPLACED FWD SERVICE DOOR MOP SILL ATTACH ANGLE AROUND NUT PLATES BS 300324 RBL 56 WL 208 IAW SRM 51-40-02-0G-0 & 53-10-15-1A-2 AND PER DRAWING 141A8310 GW 92421U 9-2-18

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 64,037 hrs · 37,654 cycles

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

Part: FLOOR PANEL — DAMAGED (FLIGHT DECK) · airframe 64,037 hrs · 37,654 cycles

COCKPIT FLOOR DAMAGED STA 254-260; LBL 15-RBL5; AND STA 268-270; LBL 10-15; WL 208. / REPAIRED COCKPIT FLOOR DAMAGE STA 254 - 260; LBL 15 - RBL 5 AND STA 268 - 270; LBL 10 - LBL 15; WL 208 PER ER # 18-04150 REV IR AND EA 1-753-33329 REV IR.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 64,037 hrs · 37,654 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO BS 294, RBL 1. R&R SUPPORT IAW SRM & EA.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 64,037 hrs · 37,654 cycles

AFT FLOOR PANEL 242VF I/B EDGE IS DAMAGED JUST FWD FWD OF AFT GALLEY CUT-OUT. (MARKED) / AFT FOOR PANEL 242 I/B EDGE JUST FWD OF AFT GALLEY CUT-OUT HAS BEEN REPAIRED IAW SRM 53-00-50-212-2 AND SRM 53-00-50-2R-6.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 64,037 hrs · 37,654 cycles

AFT FLOOR PANEL 241AEF FWD EDGE OF LARGE CUT-OUT IS SOFT. (MARKED) / REPAIRED MULTIPLE PUNCTURES ON UPPER SKIN OF AFT FLOOR PANEL 241XF IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-6. 59049U 8-24-18

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 64,037 hrs · 37,654 cycles

AFT FLOOR PANEL 241ACF LOWER SKIN DAMAGED AT FWD GALLEY CUT-OUT. (MARKED) / AFT FLOOR PANEL 241ACF LOWER SKIN AT FWD GALLEY CUT OUT (MARKED) WAS REPAIRED IAW SRM 53-00-50-2R-4.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 64,037 hrs · 37,654 cycles

AFT FLOOR PANEL 241AAF HAS DAMAGED INSERTS; AND PUNCTURE ON UPER SURFACE. 10036C 8/22/18 / AFT FLOOR PANEL 241AAF WITH DAMAGED INSERTS AND PUNCTURE ON UPPER SURFACE CENTER OF BOARD WAS REPAIRED IAW SRM 53-00-50-2R-2

Part: GUSSET — CRACKED (FUSELAGE) · airframe 64,037 hrs · 37,654 cycles

GUSSET CRACKED AT BS 867. R&R GUSSET PER SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 64,037 hrs · 37,654 cycles

AFT CARGO BAY SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 20. R&R SHIELD PER SRM & DWG.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 64,037 hrs · 37,654 cycles

AFT CARGO BAY ; CORROSION ON CARGO BAY FLOOR STRAP BS772 LBL10 TO RBL10 / RECEIVED NEW ACB FLOOR STRAP ON PO# 699391

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 64,037 hrs · 37,654 cycles

AFT CARGO BAY INTERCOSTAL CORRODED AT BS 927+4, LBL 3. R&R INTERCOSTAL PER SRM & DWG.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 64,037 hrs · 37,654 cycles

FWD CARGO BAY; FWD CORNER SCUFF PLATE IS CRACKED / RECEIVED NEW FWD CARGO BAY; FWD CORNER SCUFFPLATE ON SWA PO # 700089

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 64,037 hrs · 37,654 cycles

FWD CARGO BAY; AFT CORNER SCUFF PLATE IS CRACKED / RECEIVED NEW FWD CARGO BAY; AFT CORNER SCUFFPLATE ON SWA PO #702234

Part: NONE — DELAMINATED (LWR FUSELAGE) · airframe 64,037 hrs · 37,654 cycles

SUPPLEMENTAL INFORMATION: FAIRING PANEL 193B HAS DISBONDS ON EXTERIOR SURFACE / REPAIRED EXTERIOR SURFACE DISBONDS ON PANEL 193B IAW SRM 53-40-70; SRM 53-40-70-2R-1; SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-11

Part: STIFFENER — NONE (LWR FUSELAGE) · airframe 64,037 hrs · 37,654 cycles

SUPPLEMENTAL INFORMATION: FAIRING PANEL # 193AR HAS CHAFFING AND OVERSIZED HOLES ON THE INTERNAL SIDE OF PANEL ALONG THE EDGES AND / REPAIRED FARING PANEL # 193AR CHAFFING AND OVERSIZED HOLES ON THE INTERNAL SIDE OF PANEL ALONG THE EDGES IAW DRM 51-70-05-2R-6 AND ADDITIONAL DAMAGE 4.5' FROM FWD EDGE AND 3.75' FROM FWD EDGE IAW SRM 51-70-05-2R-2

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 64,037 hrs · 37,654 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO BAY; AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED ACB; AFT CORNER SCUFFPLATE PER SWA EA# 1-A53-2076 REV11

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 64,037 hrs · 37,654 cycles

HORIZONTAL PRESSURE DECK CRACKED BETWEEN BS 663 TO BS 675, BETWEEN LBL 30 TO LBL 45. REPAIRED DECK PER ER AND EA.

Part: STIFFENER — CRACKED (LT WHEEL WELL) · airframe 64,037 hrs · 37,654 cycles

SUPPLEMENTAL INFORMATION: L/H HORIZONTAL STIFFENER ON FWD SIDE OF BS663 LBL8 IS CRACKED AT WL160 / REMOVED AND REPLACED L/H HORIZONTAL STIFFENER AT BS663 LBL8 FWD SIDE IAW SRM 51-40-02-0G-0 AND DWG 111A1000

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 64,037 hrs · 37,654 cycles

VAPOR BARRIER ATTACH ANGLE CRACKED IN VERTICAL FLANGE AT BS 663, RBL 8. REPAIRED ANGLE PER ER AND EA.

Part: STIFFENER — CRACKED (RT WHEEL WELL) · airframe 64,037 hrs · 37,654 cycles

SUPPLEMENTAL INFORMATION: R/H HORIZONTAL STIFFENER ON FWD SIDE OF BS663 RBL8 IS CRACKED AT WL160 / REMOVED AND REPLACED HORIZONTAL STIFFENER ON FWD SIDE OF BS 663 RBL 8 WL 160 IAW SRM 51-40-02 AND DWG 111A1001.

Part: STIFFENER — CRACKED (RT WHEEL WELL) · airframe 64,037 hrs · 37,654 cycles

VERTICAL STIFFENER IS CRACKED ON AFT SIDE OF BS663 RBL27 WL144 / LOCATED; DRILLED; DEBURRED NEW VERTICAL STIFFNER; BS 663 RBL27 WL142. INSTALLED ON CUSTOMER CARD T829885.

Part: SKIN — CRACKED (LT WING) · airframe 64,037 hrs · 37,654 cycles

L/W #3 L/E SLAT LOWER SKIN CRACKED AT ACTUATOR ATTACHMENT RIB / RECEIVED A NEW #3 SLAT ASSY. #3 SLAT WILL BE INSTALLED ON CUST. CARD # T830127.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 64,037 hrs · 37,654 cycles

LOWER VAPOR BARRIER CRACKED AT BS 663, LBL 7. REPAIRED BARRIER IAW SRM.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 64,037 hrs · 37,654 cycles

LOWER VAPOR BARRIER CRACKED AT BS 663, RBL 7. REPAIRED BARRIER IAW SRM.

Part: STIFFENER — CRACKED (LT WHEEL WELL) · airframe 64,037 hrs · 37,654 cycles

VERTICAL STIFFENER IS CRACKED ON AFT SIDE OF BS663 LBL27 WL144 / REMOVED AND REPLACED VERTICAL STIFFENER AT BS 663 LBL 27 WL 144 IAW SRM 51-40-02-0G-0 AND DWG 111A1000

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,037 hrs · 37,654 cycles

LT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: SENSOR — OUT OF TOLERANCE (TE FLAP) · airframe 63,951 hrs · 37,604 cycles

DECLARED EMERGENCY, SELECTED FLAPS 5 ON APPROACH AND GOT FLAP ASYMMETRY OF UP AND NOT EVEN FLAP 1. USED ALT FLAPS EXT SWITCH TO EXTEND LEDS FOR A NO FLAP LANDING. R&R F2 SKEW SENSOR PER AMM.

Part: TRANSMITTER — OUT OF TOLERANCE (TE FLAP) · airframe 63,951 hrs · 37,604 cycles

DECLARED EMERGENCY, SELECTED FLAPS 5 ON APPROACH AND GOT FLAP ASYMMETRY OF UP AND NOT EVEN FLAP 1. USED ALT FLAPS EXT SWITCH TO EXTEND LEDS FOR A NO FLAP LANDING. R&R LT FLAP POSITION TRANSMITTER PER AMM.

Part: SIGN — MISSING (CABIN) · airframe 63,401 hrs · 37,228 cycles

FORWARD ENTRANCE EMERGENCY EXIT LIGHT COVER MISSING RED ARROW ON SIGN. R&R SIGN PER AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 63,401 hrs · 37,228 cycles

R2 DOOR LOWER EMERGENCY EXIT SIGN MISSING DIRECTIONAL ARROW. R&R COVER PER AMM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 62,314 hrs · 36,533 cycles

LEFT WING OTBD AFT FLAP LOWER INBOARD CORNER DELAMINATED. REPAIRED THE FLAP IAW EA.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 62,314 hrs · 36,533 cycles

LEFT WING OTBD, AFT FLAP, LOWER INBOARD CORNER DELAMINATED. REPAIRED THE AFT FLAP IAW EA.

Part: ATTACH BRACKET — CRACKED (WNG-BDY FAIRING) · airframe 62,314 hrs · 36,533 cycles

RIGHT WING TO BODY FAIRING PANEL 191AR AFT CENTER ATTACH BRACKET CRACKED. R & R THE ATTACH BRACKET IAW SRM.

Part: RETAINER — CRACKED (RT WING) · airframe 62,314 hrs · 36,533 cycles

RIGHT WING AFT T/E UPPER PANEL AFT OF ENG; BULB SEAL BRACKET CRACKED. / R&R'D RIGHT WING AFT T/E UPPER PANEL AFT OF ENG; BULB SEAL BRACKET PER SRM 51-10-02.

Part: CONTROL PANEL — FAULTY (FUEL BOOST) · airframe 61,438 hrs · 35,966 cycles

NR 2 AFT FUEL BOOST PUMP LIGHT CAME ON IN CLIMB. RETURNED TO BASE. R & R THE NR 1 AFT BOOST PUMP CONTROL PANEL IAW AMM.

Part: STOP — CRACKED (AFT CARGO THRESH) · airframe 60,436 hrs · 35,314 cycles

AFT CARGO DOOR STOP CRACKED. / REMOVED AND REPLACED CARGO DOOR STOP PER SIP

Part: LENS — LOOSE (CABIN) · airframe 59,995 hrs · 35,051 cycles

L1 DOOR EXIT LENS COVER LOOSE. SECURED LENS IAW EA.

Part: BRACKET — OUT OF ADJUST (R1 DOOR) · airframe 58,629 hrs · 34,254 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUST BRACKET. ADJUSTED BRACKET IAW AMM.

Part: SPRING — FAULTY (L1 DOOR GATE) · airframe 57,938 hrs · 33,842 cycles

LOUD SOUND OF RUSHING AIR COMING THROUGH FORWARD PART OF FORWARD ENTRY DOOR REPORTED BY FLIGHT ATTENDANTS. RETURNED TO DEPARTURE. AIRCRAFT PRESSURIZATION WAS NORMAL. R & R L1 DOOR LOWER HINGE, FLAPPER SEAL SPRING IAW AMM.

Part: GIRT BAR — OUT OF ADJUST (L2 DOOR SLIDE) · airframe 57,536 hrs · 33,583 cycles

L2 DOOR EMERGENCY SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED THE GIRT BAR IAW AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,536 hrs · 33,583 cycles

LEFT FORWARD OVERWING EMERGENCY ESCAPE LATCH LIGHT BULB INOPERATIVE. R & R THE BULB IAW AMM.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 57,536 hrs · 33,583 cycles

L2 DOOR EMERGENCY LIGHT INOPERATIVE. SECURED CONNECTOR IAW SWPM.

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 57,536 hrs · 33,583 cycles

AFT CARGO DOOR SKIN CREASED ABOVE DOOR HANDLE. REPAIRED IAW AMM & DWG.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 57,536 hrs · 33,583 cycles

RIGHT WING NR 7 SLAT LOWER SKIN CRACKED AT SS 322.71. REPAIRED THE SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,536 hrs · 33,583 cycles

RIGHT WING NR 6 SLAT LOWER SKIN CRACKED AT SLAT STA 202.45. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 57,536 hrs · 33,583 cycles

LEFT WING NR 1 SLAT LOWER SKIN CRACKED AT SLAT STATION 451.97. REPAIRED THE SKIN IAW SRM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 56,302 hrs · 32,837 cycles

RIGHT PHOTO LUMINESCENT LIGHT STRIP DAMAGED AT ROW 1. R & R STRIP IAW SIP.

Part: FUEL NOZZLE — FAULTY (NR 1 ENGINE) · airframe 55,872 hrs · 32,579 cycles

AIR TURN BACK & DECLARED EMER. SHORTLY AFTER TAKEOFF FLIGHT ATTENDANTS CALLED & SAID PAXS WERE REPORTING A FIRE ON LT SIDE OF THE ACFT. R & R FUEL NOZZLE ASSEMBLY IAW MM.

Part: ANGLE — CRACKED (LT WING) · airframe 54,100 hrs · 31,560 cycles

LEFT WING INBD FIXED TE PANEL ANGLE SUPPORT BRACKET CRACKED OTBD TOP EDGE. REPAIRED ANGLE IAW EA.

Part: SIGN — BROKEN (CABIN) · airframe 53,600 hrs · 31,286 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 53,600 hrs · 31,286 cycles

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

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 53,645 hrs · 31,310 cycles

FUEL CROSS FEED VLV IN OPEN POSITION. R & R CROSS FEED VLV ACTUATOR IAW AMM.

Part: LIGHT — FAILED (CABIN) · airframe 51,723 hrs · 30,249 cycles

RIGHT OVERWING EMER LIGHT LOCATION 1669 FAILED CAPACITY CHECK. R & R LIGHT IAW AMM.

Part: RELAY — FAULTY (COCKPIT) · airframe 51,022 hrs · 29,837 cycles

DIVERSION ON TAKEOFF ROLL AT 122DTS BOTH CTR PUMP LOW PRESS LIGHTS ILLUMINATED. R & R RT UFI RELAY IAW MM.

Part: RELAY — FAULTY (COCKPIT) · airframe 51,022 hrs · 29,837 cycles

DIVERSION ON TAKEOFF ROLL AT 122DTS BOTH CTR PUMP LOW PRESS LIGHTS ILLUMINATED. R & R LT UFI RELAY IAW MM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

LONGITUDINAL FLOORBEAM HOLES UPPER AFT END CRACKED AT BS 727B LBL 24.75. REPAIRED BEAM ACO & EA.

Part: FITTING — DAMAGED (LT HORIZ STAB) · airframe 50,879 hrs · 29,761 cycles

LEFT HORIZONTAL STABILIZER CTR SECTION FRONT SPAR FITTING DAMAGED ON RT LOWER SURFACE IN THE AREA OF THE SLIDER SEAL LINK ASSEMBLY. REPAIRED.

Part: SPAR — DAMAGED (LT HORIZ STAB) · airframe 50,879 hrs · 29,761 cycles

LEFT HORIZONTAL STABILIZER CTR SECTION FRONT SPAR DAMAGED ON RT SIDE IN THE AREA OF THE SLIDER SEAL LINK ASSEMBLY. REPAIRED SPAR IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

LONGITUDINAL FLOORBEAM HOLES UPPER AFT END CRACKED AT BS 727B RBL 24.75. REPAIRED BEAM ACO & EA.

Part: SPAR — DAMAGED (LT HORIZ STAB) · airframe 50,879 hrs · 29,761 cycles

LEFT HORIZONTAL STABILIZER CTR SECTION FRONT SPAR DAMAGED ON LT SIDE IN THE AREA OF THE SLIDER SEAL LINK ASSEMBLY. REPAIRED SPAR IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

LEFT WW OTBD AFT LOWER CHORD ASSEMBLY WEB CRACKED. R & R WEB IAW SRM & ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM UNDER SEAT TRACK ASSEMBLY VERTICAL FLANGE 2ND FASTENER FROM TOP CRACKED AT BS 727B LBL 46.5. REPAIRED FLANGE IAW EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

L ANGLE BRACKET ON FWD SIDE OF FLOORBEAM CRACKED AT BS 727B, LBL 45.5, 1ST, 2ND & 4TH HOLE FROM TOP. REPAIRED L ANGLE BRACKET IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

LONGITUDINAL FLOORBEAM UPPER AFT ANGLE UNDER SEAT TRACK CRACKED AT BS 727B+1 LBL 24.75. REPAIRED BEAM IAW SRM & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM WEB UNDER SEAT TRACK CRACKED AT BS 727B RBL 24.75. REPAIRED BEAM IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727B LBL 44.5. REPAIRED FLANGE IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM UPPER CHORD UNDER SEAT TRACK CRACKED AT BS 727B, RBL 25.75 BEAM HOLE. REPAIRED CHORD IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

LONGITUDINAL FLOORBEAM UPPER AFT ANGLE HOLES UNDER SEAT TRACK CRACKED AT BS 727B, LBL 46.5. REPAIRED BEAM IAW SRM & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

AFT SEAT TRACK HOLE CRACKED AT BS 727B+1 RBL 24.75. REPAIRED SEAT TRACK IAW SRM & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM UNDER SEAT TRACK ASSEMBLY VERTICAL FLANGE 3RD FASTENER FROM TOP CRACKED AT BS 727B LBL 46.5. REPAIRED FLANGE IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM WEB UNDER SEAT TRACK ASSEMBLY CRACKED AT BS 727B RBL 45.5 OTBD HOLE 5 INCHES DOWN FROM TOP FLANGE, 1ST HOLE. REPAIRED WEB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

LONGITUDINAL FLOORBEAM UPPER AFT ANGLE UNDER SEAT TRACK CRACKED AT BS 727B+1 LBL 45.5. REPAIRED BEAM IAW SRM & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM UNDER SEAT TRACK ASSEMBLY CRACKED AT BS 727B LBL 25.75, 6TH FASTENER FROM TOP OF VERTICAL FLANGE. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM UNDER SEAT TRACK ASSEMBLY CRACKED AT BS 727B, LBL 46.5, 2ND FASTENER FROM TOP OF VERTICAL FLANGE. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM UNDER SEAT TRACK ASSEMBLY VERTICAL FLANGE 5TH FASTENER FROM TOP CRACKED AT BS 727B LBL 44.5. REPAIRED FLANGE IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM WEB UNDER SEAT TRACK ASSEMBLY CRACKED AT BS 727B, RBL 45.5, INBD HOLE 3.5 INCHES DOWN FROM TOP FLANGE, 4TH FASTENER DOWN. REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM WEB UNDER SEAT TRACK ASSEMBLY CRACKED AT BS 727B, RBL 45.5, INBD HOLE 4.6 INCHES DOWN FROM TOP FLANGE, 5TH FASTENER DOWN. REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM UPPER CHORD UNDER SEAT TRACK CRACKED AT BS 727B RBL 25.75. REPAIRED BEAM IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

L ANGLE BRACKET ON FWD SIDE OF FLOORBEAM CRACKED AT BS 727B, RBL 24.75, 2ND & 5TH HOLES FROM TOP. REPAIRED L ANGLE BRACKET IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM CRACKED AT BS 727B, LBL 44.5, INBD 3/16 FASTENER HOLE. REPAIRED FLOORBEAM TRACK IAW EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM FASTENER HOLE CRACKED AT BS 727B, LBL 43.5 INBD 3/16. REPAIRED TRACK IAW EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

VERTICAL WEB CRACKED AT BS 663 LBL 40. REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM UNDER SEAT TRACK ASSEMBLY AFT HOLE IN LUG AREA CRACKED AT BS 727B+2 RBL 24.75. REPAIRED BEAM IAW EA.

Part: PLATE — CRACKED (RT WING) · airframe 50,879 hrs · 29,761 cycles

RIGHT WING PANEL 651GB INBD WIGGLE PLATE CRACKED. R & R WIGGLE PLATE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727A+19, RBL 46.5. REPAIRED TRACK IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM CRACKED AT BS 727B, RBL 42.5. REPAIRED BEAM IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727A+18, LBL 46.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727A+19, LBL 23.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727A+18, RBL 44.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727A+19, RBL 23.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727B+1, RBL 46.5. REPAIRED TRACK IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM UNDER SEAT TRACK ASSEMBLY TOP FASTENER BEAM HOLE VERTICAL FLANGE CRACKED AT BS 727B, RBL 46.5. REPAIRED TRACK IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM UNDER SEAT TRACK ASSEMBLY CRACKED AT BS 727B RBL 25.75, TOP FASTENER BEAM HOLE ON VERTICAL FLANGE. REPAIRED BEAM IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727A+19 RBL 25.75. REPAIRED SEAT TRACK IAW SRM & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY AFT HOLE IN LUG AREA CRACKED AT BS 727B+2, RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727A+19, LBL 44.5. REPAIRED SEAT TRACK IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM UNDER SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727B+1, RBL 44.5. REPAIRED TRACK IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

LEFT NR 3 WINDOW FRAME E - F POST NR 7 HOLE CRACKED. REPAIRED POST IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK UPPER FLANGE CRACKED AT BS 727B, LBL 25.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727A+18, LBL 44.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727B+1, RBL 44.5. REPAIRED TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727A+18, LBL 23.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727A+19, LBL 46.5. REPAIRED SEAT TRACK IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM UNDER SEAT TRACK ASSEMBLY AFT HOLE IN LUG AREA CRACKED AT BS 727B+2 RBL 45.5. REPAIRED BEAM IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

LEFT NR 3 WINDOW FRAME E - F POST NR 8 HOLE CRACKED. REPAIRED POST IAW ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

FLOORBEAM UNDER SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727B+1, RBL 46.5. REPAIRED TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK ASSEMBLY TOP FLANGE CRACKED AT BS 727B+1 RBL 25.75. REPAIRED SEAT TRACK IAW SRM & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,879 hrs · 29,761 cycles

SEAT TRACK UPPER FLANGE CRACKED AT BS 727B, LBL 23.75. REPAIRED SEAT TRACK IAW EA.

Part: SIGN — LOOSE (CABIN) · airframe 50,488 hrs · 29,554 cycles

CENTRAL CABIN OVERHEAD EXIT SIGN LOOSE. SECURED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,477 hrs · 28,395 cycles

RT BULLNOSE EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 47,893 hrs · 28,036 cycles

L2 DOOR INTERIOR EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,375 hrs · 27,128 cycles

RT EMERGENCY OVERWING DOOR HANDLE LIGHT INOP. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 46,375 hrs · 27,128 cycles

LEFT EMERGENCY OVERWING EXIT SIGN LIGHTS INOP. RELAMPED IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 46,252 hrs · 27,059 cycles

L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 46,099 hrs · 26,973 cycles

EMERGENCY "EXIT" SIGN AT MID-CABIN LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 44,033 hrs · 25,698 cycles

RIGHT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT CONNECTOR BROKEN AT ROW 13. REMOVED AND REPLACED CONNECTOR PER SWPM AND AMM.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

SHEAR WEB CRACKED BETWEEN BS 986.5 TO BS 1016, LBL 34.5. REMOVED AND REPLACED SHEAR WEB PER SRM.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

SHEAR WEB CRACKED BETWEEN BS 986.5 TO BS 1016, RBL 38. REMOVED AND REPLACED SHEAR WEB IAW DWG AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FRAME CRACKED AT BS 907, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW ATS ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FRAME CRACKED AT BS 867, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FRAME CRACKED AT BS 360, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW ATS ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FRAME CRACKED AT BS 500A, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FRAME CRACKED AT BS 727D, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FRAME CRACKED AT BS 727D, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FRAME CRACKED AT BS 440, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FRAME CRACKED AT BS 400, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FRAME CRACKED AT BS 480, BETWEEN STR 8L AND STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FRAME CRACKED AT BS 480, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FRAME CRACKED AT BS 400, BETWEEN STR 8L AND STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FRAME CRACKED AT BS 597, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FRAME CRACKED AT BS 867, BETWEEN STR 8R AND 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FRAME CRACKED AT BS 747, BETWEEN STR 8L AND 9L. REPAIRED FRAME PER EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

CREASE BEAM WEB SUPPORT ANGLE CLIP CRACKED AT BS 663, STR 17L. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 5. REPAIRED 'T' CHORD PER SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 44,033 hrs · 25,698 cycles

RIGHT HORIZONTAL STABILIZER RIB VERTICAL STIFFENERS CRACKED AT STA 92.7. REMOVED AND REPLACED STIFFENERS PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

AFT CARGO BAY SUBTHRESHOLD WEB CORRODED BETWEEN BS 787 TO BS 847, BETWEEN RBL 20 TO RBL 28. REMOVED AND REPLACED WEB IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

BULKHEAD VERTICAL STIFFENER ATTACH ANGLE CRACKED. REMOVED AND REPLACED BRACKET PER SRM.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 44,033 hrs · 25,698 cycles

BULKHEAD LINER SUPPORT CHANNEL CRACKED AT BS 727+4, RBL 3. REMOVED AND REPLACED CHANNEL PER SRM AND DWG.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 42,944 hrs · 25,060 cycles

R2 DOOR SLIDE OUT OF CONTANER. RE-INSTALLED R2 DOOR SLIDE IAW MM AND MT.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 40,349 hrs · 23,529 cycles

ELECTRICAL ODOR IN MID CABIN AREA. MEL'S BALLAST.

Part: EEC — FAULTY (NR 2 ENGINE) · airframe 40,295 hrs · 23,497 cycles

NR 2 ENGINE SLOW TO DE-ACCELERATE WHEN THRUST LEVERS RETARDED TO IDLE. REMOVED AND REPLACED NR 2 ELECTRONIC ENGINE CONTROL PER MM.

Part: EEC — FAULTY (NR 2 ENGINE) · airframe 40,152 hrs · 23,405 cycles

DURING DESCENT FROM CRUISE NR 2 ENGINE HUNG AT 71 PERCENT N1 WITH THROTTLES AT IDLE. HUNG FOR 1 MIN THEN N1 RETURNED TO NORMAL IDLE THRUST. EVENT HAPPENED TWICE THEN NOT AGAIN FOR FLIGHT. REMOVED AND REPLACED NR 2 EEC PER MM.

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 38,919 hrs · 22,718 cycles

R2 SLIDE LOOSE. SECURED SLIDE GIRT BAR PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 38,972 hrs · 22,746 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 38,853 hrs · 22,674 cycles

NR 1 FUEL GAUGE AND NR 2 FUEL GAUGE INDICATED A 100 POUND IMBALANCE EVERY 20 MINUTES IN FLIGHT. REMOVED AND REPLACED CROSSFEED FUEL ACTUATOR PER MT AND MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 36,421 hrs · 21,233 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 36,421 hrs · 21,233 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: TRUNNION — CORRODED (LT MLG) · airframe 34,835 hrs · 20,276 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 34,835 hrs · 20,276 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 34,218 hrs · 19,906 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 34,218 hrs · 19,906 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHT FAILED FUNCTION TEST. REMOVED AND REPLACED BATTERIES PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,507 hrs · 17,626 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BL 0. REPAIRED BEAM PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,169 hrs · 15,636 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,347 hrs · 13,946 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 23 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,281 hrs · 13,340 cycles

DURING SCHEDULED MV3 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: ACM — FAULTY (RT PACK) · airframe 21,211 hrs · 12,145 cycles

DIVERSION - SMOKE/SULPHUR SMELL IN CABIN. FOUND RT PACK TRIPPED. RT AIR CYCLE MACHINE INOP. REMOVED AND REPLACED RT AIR CYCLE MACHINE PER MM.

Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 21,022 hrs · 12,030 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATES OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 12,994 hrs · 7,500 cycles

L2 DOOR EVAC SLIDE PRESSURE INDICATION LOW. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: COVER — LOOSE (CABIN) · airframe 6,300 hrs · 3,783 cycles

EEPLS COVER LOOSE. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — DEPLOYED (FWD ENTRY DOOR) · airframe 5,560 hrs · 3,364 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE DEPLOYED AT GATE. REMOVED AND REPLACED SLIDE AND CASE PER MM.

Part: COVER — LOOSE (CABIN) · airframe 4,346 hrs · 2,661 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER LOOSE AT ROW 11. R&R EEPLS COVER PER MM.