N7817J

Part: COVER — DETACHED (ZN 200 FUS TOP) · airframe 60,307 hrs · 30,792 cycles

CREW REPORTS LEFT EMERGENCY EXIT ROW LIGHT LENS COVER FELL OFF<[01] REPLACED LENS COVER PER AMM 33-51-03

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 60,202 hrs · 30,730 cycles

LEFT SIDE EMERGENCY EXIT LIGHT (OVER WING) LENSE COVER MISSING.<[01] INSTALLED LENS COVER ON LEFT SIDE EMERGENCY EXIT SIGN (OVER WING) REF AMM 33-51-01.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 59,993 hrs · 30,593 cycles

LH AFT EMERGENCY LIGHT BATTERY REQUIRES REPLACEMENT.<[01] REPLACED LH AFT EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-03. OPS GOOD.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 59,675 hrs · 30,382 cycles

EXTERIOR EMERGENCY LIGHT R/H BELOW WING INOP<[01] RELAMPED LIGHT PER AMM 33-51-04 OPS CHECK GOOD

Part: RELAY — WARNING LIGHT (ZN 200 FUS TOP) · airframe 59,468 hrs · 30,242 cycles

UPON INITIAL FLAP RETRACTION ON T/O WE ENCOUNTERED A RUNAWAY STAB TRIM. THE RUNAWAY CONTINTED EVEN AFTER FLAPS WERE UP. AUTOPILOT WAS NEVER ENGAGED. SPEED TRIM LIGHT CAME ON FOR AWHILE THAN FLASHED IN<[01] R/R'D R64 AND R384 PER AMM 27-41-00. PERFORMED DFCS BITE. NO FAULTS NOTED.

Part: HANDLE — LOOSE (ZN 200 FUS TOP) · airframe 58,536 hrs · 29,639 cycles

CUSTOMER WALK: L1 DOOR BOTH ASSIST HANDLES ON LINER NEED TIGHTEN<[01] ADJUSTED L1 DOOR ASSIST HANDLE AS PER AMM 52-11-31-400-802.;[02] VERIFIED STEP NO1.

Part: FITTING — ELONGATED (ZN 500 LEFT WING) · airframe 58,536 hrs · 29,639 cycles

L/W REAR SPAR FIXED T/E PANEL 551GB INB FWD SUPPORT LINK UPPER FITTING HOLE ELONGATED @ REAR SPAR MKD DOT<[01] REMOVED AND REPLACED SUPPORT BRACKET AT L/W REAR SPAR FIXED T/E PANEL 551GB REF B-737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1

Part: RIB — CRACKED (ZN 600 RIGHT WIN) · airframe 58,536 hrs · 29,639 cycles

NO-1 ENG INB FAN COWL INT.INTERCOSTAL RIB CRACKED AT EDGE AT ENG OIL SERVICE DOOR AREA MKD DOT<[01] REMOVED AND REPLACED INT; INTERCOSTAL RIB AT EDGE ON #1 ENGINE I/B FAN COWL AT ENGINE OIL SERVICE DOOR AREA. PER SRM 51-40-02-0G-O;[02] VERIFIED REPLACEMENT

Part: FITTING — CRACKED (ZN 500 LEFT WING) · airframe 58,607 hrs · 29,681 cycles

L/W REAR SPAR FIXED T/E PANEL 551GB FWD WIGGLE FITTING CRACKED AND SHEARED FASTENERS @ ORSS 261 MKD DOT<[01] REMOVED AND REPLACED WIGGLE PLATE AT LH WING REAR SPAR FIXED T/E (PANEL 551GB) REF: SRM 51-40-02-0G-0.;[02] VERIFIED INSTALLATION

Part: SUPPORT — CRACKED (ZN 200 FUS TOP) · airframe 58,536 hrs · 29,639 cycles

MAIN CABIN CENTER AISLE FLOOR SUPPORT BREAK CRACKED AT STA 540 LBL-1<[01] REMOVED AND REPLACED FLOOR SUPPORT BREAK AT MAIN CABIN STA 540 LBL-1 PER BOEING 737-700 SRM 51-40-02-0G-0;[02] VERIFIED REPLACEMENT

Part: PANEL — DELAMINATED (ZN 600 RIGHT WIN) · airframe 58,536 hrs · 29,639 cycles

NO-2 PYLON STRUT PANEL 441EL EDGE DELAMINATED MKD<[01] MEASUREMENTS;[02] REPAIRED EDGE DAMAGE AT #2 PYLON STRUT PANEL #441EL AS PER BOEING &37 SRM 51-70-04-2R-6.MATERIAL USED EY3804 PO# 1799597;RESTORED ORIGINAL FINISHED.;[03] VERIFIED STEP 2

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 58,536 hrs · 29,639 cycles

L/H HORIZONTAL STABILIZER FRONT SPAR REMOVABLE FAIRING INNER SUPPORT RIB # 6 CRACKED @ EDGE MKD DOT<[01] REMOVED L/H HORIZONTAL STAB L/E RIB #6 AS PER B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW RIB AS PER B737-700 SRM 51-40-05-0G-0;[03] VALIDATED STEP 1 & 2<BR><BR><BR>OK TO INSTALL NEW UNIT;[04] INSTALLED NEW L/H HORIZONTAL STAB L/E RIB #6 AS PER B737-700 SRM 51-40-02-0G-0.;[05] VALIDATED STEP 4

Part: SUPPORT — CRACKED (ZN 200 FUS TOP) · airframe 58,536 hrs · 29,639 cycles

MAIN CABIN FLOOR SUPPORT BREAK CRACKED @ STA 540 RBL-1 MKD DOT<[01] REMOVED AND REPLACED FLOOR SUPPORT BREAK AT MAIN CABIN STA 540 RBL-1 PER BOEING 737-700 SRM 51-40-02-0G-0;[02] VERIFIED REPLACEMENT

Part: PANEL — LOOSE (ZN 100 FUS LOWER) · airframe 58,536 hrs · 29,639 cycles

FORWARD CARGO COMPARTMENT FORWARD BLKHD PANEL 121KW BATTERY NET TIE DOWNS LOOSE / PULLED OUT. (51-016)<[01] REMOVED PANEL 121KW AS PER SRM 51-40-02-0G-0.;[02] RE-INSTALLED INSERTS AT PANEL 121KW BATTERY NET TIE DOWNS AS PER SOPM 20-50-22.;[03] RE-INSTALLED TIE DOWNS AT PANEL 121KW AS PER SRM 51-40-02-0G-0.;[04] VERIFIED REMOVAL; INSERT AND TIEDOWN INSTALLATION.<BR>OK TO INSTALL PANEL;[05] RE-INSTALLED PANEL 121KW AS PER SRM 51-40-02-0G-0.;[06] WORK COMPLETED.;[07] VERIFIED WORK COMPLETED

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 58,040 hrs · 29,302 cycles

FWD SERVICE DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW. REMOVED AND REPLACED SIGN IAW AMM 33-51-01.

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 58,040 hrs · 29,302 cycles

RIGHT OVERWING EMERGENCY EXIT DOOR INTERIOR LOWER HANDLE MOLDING IS NOT SECURED. SECURED HANDLE IAW AMM 52-22-00.

Part: FITTING — ELONGATED (RH WING) · airframe 57,150 hrs · 28,690 cycles

RIGHT WING LOWER TRAILING EDGE SUPPORT ROD OUTBOARD OF #6 TRANSMISSION UPPER TEE FITTING HOLE ELONGATED / [01] ACCOMPLISH EA 22-157-02564 ASSIGNED AS A SUBTASK.;[02] REPAIRED RIGHT WING LOWER TRAILING EDGE SUPPORT ROD O/B OF #6 TRANSMISSION UPPER TEE FITTING PER EA 22-157-02564-WIP2.;[03] UPDATE PARTS

Part: SUPPORT ROD — ELONGATED (RH WING) · airframe 57,150 hrs · 28,690 cycles

RIGHT WING TRAILING EDGE SUPPORT ROD OUTBOARD OF #6 TRANSMISSION LOWER SUPPORT BEAM FORWARD HOLE ELONGATED / [01] REMOVED RIGHT WING TRAILING EDGE SUPPORT ROD OUTBOARD #6 TRANSMISSION LOWER SUPPORT BEAM PER SRM 51-40-02;[02] R&R RIGHT WING TRAILING EDGE LOWER SUPPORT BEAM OUTBOARD OF #6 TRANSMISSION REF SRM 51-40-02 & AMM 20-50-11.

Part: SIGN — LOOSE (FWD CABIN) · airframe 56,823 hrs · 28,463 cycles

THE FORWARD CABIN EMERGENCY EXIT SIGN IS HANGING FROM THE CEILING AND NEEDS TO BE SECURED / [01] SECURED FWD CABIN EMERGENCY EXIT SIGN BY TIGHTENING MOUNT MOUNT FASTENER IAW AMM 20-10-26.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 55,553 hrs · 27,666 cycles

FWD SERVICE DOOR SLIDE IS HANGING DOWN OUT OF BUSTLE ; / [01] REPOSITIONED SLIDE IN BUSTLE PER MT 725-61-06

Part: BRACKET — LOOSE (R1 DOOR) · airframe 55,523 hrs · 27,644 cycles

?A? FA REPORTS THAT GIRT AR BRACKETS ON FWD SERVICE DOOR ARE LOOSE & THAT GIRT BAR FALLS OUT WHEN DOOR IS OPENED ; / [01] RESECURED GIRT BAR BRACKETS ON FWD SERVICE DOOR IAW SIP

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 55,404 hrs · 27,569 cycles

RH WING OTBD AFT FLAP IS DELAMINATED ON INBD LOWER SURFACE 4 INCHES IN FROM INBD SIDE; 3.5 INCHES FROM T/E; MEASURING 4.25 INCHES IN DIAMETER REF BAR CODE TTG8QA8GEN. REPAIRED FLAP IAW SRM 51-70-10; PERMANENT REPAIR.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 55,382 hrs · 27,558 cycles

AFT ENTRY DOOR SLIDE LIGHT IS INOP. / [01] RELAMPED AND PERFORMED GOOD OPERATIONAL TEST OF AFT ENTRY DOOR SLIDE LIGHT PER AMM 33-51-04-960-801; [02] VERIFIED CORRECTIVE ACTIONS STEP 1.

Part: CONNECTOR — BROKEN (CABIN) · airframe 55,382 hrs · 27,558 cycles

EMERGENCY LIGHT L1065 CONNECTOR D40100P CONTACT IN POSITION #1 ; EMERGENCY LIGHT L1065 CONNECTOR D40100P CONTACT IN POSITION #1 IS ROKEN / [01] REMOVED AND REPLACED CONNECTOR D40100P WITH NEW CONNECTOR PER SWPM 20-72-24 AND HOOKUP LIST FOR CONNECTOR D40100P; [02] VERIFIED CORRECTIVE ACTIONS STEP 1.; [03] COMPLETED STEP 1.; [04] CAL ID FOR STEP 1 PER1281; DUE:01/2022; [05] VERIFIED STEP 1 COMPLETE.; [06] COMPLETED STEP 2; PERFORMED GOOD EMERGENCY LIGHTS OPERATIONAL TEST PER AMM 33-51-00-710-801; [07] VERIFIED CORRECTIVE ACTIONS STEP 6.; [08] CERTIFIED PERFORMED GOOD CONTINUITY CHECK OF CONNECTOR D40100P PER WDM 33-51-14 AND 33-51-22.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 55,382 hrs · 27,558 cycles

EXIT INDICATOR LIGHT L1189 FOWARD OF LH ESCAPE HATCH IS INOP ; / [01] UPON FURTHER INVESTIGATION; FOUND LIGHT ASSEMBLY L1189 DISCONNECTED. RECONNECTED LIGHT ASSEMBLY AND PERFORMED GOOD TEST OF EXIT INDICATOR L1189 PER AMM 33-51-01-960-802.; [02] VERIFIED CORRECTIVE ACTION 1.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON STR23L INBOARD VERTICAL FLANGE BS360+18 WL164 ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.036 IN A 1'X2' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-03-1A-1 USING MICROMETER ID 4566A S/N UNKNOWN; [[15] INSTALLED STRINGER SECTION AND SPLICE PER SRM 51-40-02-0G-0; SRM 53-00-03-2R-1 REPAIR 1;AND DWG 140A9101;

Part: SEAT TRACK — CORRODED (BS 512-500C) · airframe 55,382 hrs · 27,558 cycles

REJECT: CORROSION STILL EXISTS ON PASSENGER CABIN SEAT TRACK RBL 45 AT BS 512; BS 500A+14; BS 500B+8; AND BS 500C. ; / [01] UPDATED MEASUREMENT TABLE.; [02] COMPLETED STEPS 1-4; [03] DAIL DETH GAGE USED IS ATS2678; S/N UNKNOWN; [04] VERIFIED DIAL DEPTH GAGE; [05] ADDED TO REFERENCE THE AREA; [06] CERTIFIED CORRECTION TO REFERENCE; [07] COMPLETED PARTIALS FOR STEPS 1-4; [08] STEP 5 COMPLETE.; [09] VERIFIED STEPS 1-4 COMPLETE.<BR><BR>ALL WORK ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (BS 727B-827) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK RBL45 WL208.1 BS727B+8-BS727C; BS727D-BS727D+11; BS727E+7-747+2; BS747+17-BS767+10; BS787+2-BS807; BS827-BS827+8 ; / [01] UPDATED STEPS 1-6.; [02] COMPLETED STEPS 1-6; [03] STEP 7 COMPLETE.; [04] COMPLETED MEASUREMENT TABLE.; [05] VERIFIED STEP 7 COMPLETE. <BR><BR>ALL WORK ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (BS 480-520) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK RBL25 WL208.1 BS480-BS489; BS493-BS515; BS500A +17-BS500B +3; BS500C +3-BS500D; BS500D +12- BS520 ; / [01] UPDATED PARTIAL STEPS 1-5; [02] STEPS 1-5 COMPLETED. <BR><BR>CALIBRATED TOOL USED :<BR>DIAL DEPTH GAUGE P/N: ATS2677<BR>CAL DATE DUE:11/2022; [03] COMPLETED STEPS 1-5<BR>VERIFIED CORRECTIVE ACTION 2; [04] STEP 6 COMPLETE.; [05] EDITED MEASUREMENT TABLE.; [06] CERTIFIED EDIT; [07] EDITED MPN IN MEASUREMENT TABLE.; [08] CERTIFIED EDIT.; [09] VERIFIED STEP 6 COMPLETE<BR><BR>AND CORRECTIVE ACTIONS 5-8.<BR><BR>ALL WORK ACCOMPLISHED

Part: SEAT TRACK — CORRODED (BS 540-727A) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK RBL25 WL208.1 BS540-BS608; BS616-BS643; BS652-BS674; BS681-727A+14 ; / [01] STEPS 1-4 COMPLETE; [02] STEPS1-4 COMPLETE.<BR><BR>CAL TOOL USED : DIAL DEPTH GAUGE<BR>P/N ATS 2677<BR>CAL DATE DUE 11/2022; [03] COMPLETED STEPS 1-4<BR>VERIFIED CORRECTIVE ACTIONS STEP 1 AND 2; [04] STEP 5 COMPLETE.; [05] VERIFIED STEP 5 COMPLETE; [06] EDITED MEASUREMENT 18.; [07] CERTIFIED EDIT.; [08] VERIFIED CORRECTIVE ACTIONS 6; 7. <BR><BR>ALL WORK ACCOMPLISHED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON INTERCOSTAL BS 1006-1016 RBL 18 WL 202. REMOVED CORROSION ON INTERCOSTAL BS1010-1016 RBL18 WL202 1.0'X6.0' IAW SRM 51-10-02-0G-0. UT INSPECTED BLENDED AREA FOR REMAINING THICKNESS IAW NDT MANUAL PART 4; 51-00-00 PROCEDURE 2. LOWEST READING NOTED IS .059 INCH. BLENDED AREA IAW NDT MANUAL PART 6; 51-00-00 PROCEDURE 23. NO CRACKS FOUND.

Part: SEAT TRACK — CORRODED (BS 568-727A) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK RBL45 WL208.1 BS540-BS552; BS568-BS674; BS680-BS688; BS703-BS730; BS742-BS727A+14 ; / [01] UPDATED STEPS 1-5.; [02] COMPLETED STEPS 1-5; [03] STEP 6 COMPLETE.; [04] VERIFIED STEP 6 COMPLETED.; [05] VERIFIED ALL WORK COMPLETE

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK RBL45 WL208.1 BS376-BS400; BS415-BS424; BS440-BS480 ; / [01] BLENDED CORROSION DAMAGE FROM SEAT TRACK RBL 45.5 WL 208 BS376-400 BS415-424 AND BS440-480 IAW SRM 53-00-52-1A-1 STEP 2 A; [02] VERIFIED CORROSION REMOVAL FROM SEAT TRACK RBL 45.5 WL 208 BS376-400 BS415-424 AND BS440-480 IAW SRM 53-00-52-1A-1 STEP 2 A

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,382 hrs · 27,558 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON PASSENGER CABIN SEAT TRACK RBL45 WL208.1 BS480-BS487; BS500-BS512; BS500A+14-BS500B+8; BS500C-BS500C+13; BS500D+7-BS520 ; / [01] BLENDED CORROSION FROM SEAT TRACK AT RBL 45.5 WL 208 BS480-487 BS500-512 BS500A-500B+8 BS500C-500C+13 AND 500D+7-520 ALL IAW SRM 53-00-52-1A-1 STEP 2 A; [02] VERIFIED CORROSION REMOVAL FROM SEAT TRACK AT RBL 45.5 WL 208 BS480-487 BS500-512 BS500A-500B+8 BS500C-500C+13 AND 500D+7-520 ALL IAW SRM 53-00-52-1A-1 STEP 2 A<BR><BR>CORROSION STILL EXISTS AT LOCATIONS NOTED IN FAULT TTG8Q009JYZ9; [03] COMPLETED STEPS 1-5; [04] DIAL DEPTH GAGE USED ATS 2678 ; S/N UNKNOWN; [05] VERIFIED DIAL DEPTH GAGE ATS 2678 ;S/N UNKNOWN; [06] CORRECTED MATERIAL REMOVED FROM AREA ON SEAT TRACK; [07] VERIFIED CORRECTION OF AREA MATERIAL REMOVED FROM; [08] VERIFIED PARTIALS FOR STEPS 1-5; [09] STEP 6 COMPLETE.; [10] VERIFIED STEPS 1-6 COMPLETE; [11] EDITED STEPS 1-4 AND 14.; [12] CERTIFIED EDITS.; [13] VERIFIED CORRECTIVE ACTIONS 11; 22.<BR><BR>VERIFIED UPDATED MEASUREMENTS 1-4 AND 14. <BR><BR>ALL WORK ACCOMPLISHED

Part: SEAT TRACK — CORRODED (BS 727B-887) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK RBL25 WL208.1 BS727B-BS727C+6; BS727C+21-BS727D+10; BS727E+9-BS747; BS747+7-BS767+12; BS787+7-BS809; BS825-BS841; BS847-BS887 ; / [01] STEPS 1-7 COMPLETE.; [02] STEP 8 COMPLETE.; [03] STEPS 1-8 COMPLETE.<BR><BR>CAL TOOL USED DIAL DEPTH GAUGE:<BR>P/N ATS 2677<BR>CAL DATE DUE: 11/2022; [04] COMPLETED STEPS 1-8<BR>VERIFIED CORRECTIVE ACTIONS 1-3; [05] APPLIED CHEMICAL CONVERSION COAT PER SRM 51-20-01 AND 1 COAT ALUMINIZED EPOXY PRIMER IAW SOPM 20-41-04. STEP 9 COMPLETE.; [06] VERIFIED STEP 9 COMPLETE.<BR><BR>CORRECTIVE ACTION 5 VERIFIED COMPLETE; [07] EDITED MEASUREMENT 18.; [08] CERTIFIED EDIT; [09] EDITED MPN ON MEASUREMENT TABLE.; [10] CERTIFIED EDIT.; [11] VERIFIED CORRECTIVE ACTIONS 7-10.<BR><BR>ALL WORK ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (BS 390-480) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK LBL25 WL208.1 BS390 - BS399; BS403 - BS413; BS420 - BS426; BS434 - BS458; BS460 - BS480. ; / [01] UPDATED MEASUREMENTS; [02] ACCOMPLISHED STEPS 1 AND 2.; [03] STEP 1 COMPLETE. VERIFIED PARTIAL UPDATE OF STEP 2.; [04] STEP 3 COMPLETE.; [05] ALL WORK ACCOMPLISHED.

Part: SUPPORT ANGLE — CORRODED (BS 360 BL0) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON SUPPORT CLIP AT MAIN EBAY BL0 BS360. MARKED. ; / [01] REMOVED CORROSION IN AN AREA OF 1.7'X1' PER SRM 51-10-02-0G-0; [02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.; [03] UT INSPECTED DENT/BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.040.<BR>EQUIP ID#: ATS2031 S/N: 170515011; [04] GRID AREA NEEDED FOR ENGINEERING; [05] REMOVED SUPPORT CLIP AT MAIN EBAY BS 360 BL0 PER SRM 51-40-02-0G-0; [06] AFTER REMOVAL; FOUND ADDITIONAL CORROSION ON SUPPORT CLIP IN AN AREA OF 2'X1.7'; REMAINING THICKNESS IS 0.030' ORIGINAL THICKNESS IS 0.040'. FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. USING ATS TOOL MICROMETER ID: ATS601 SN: 87172291; [07] VERIFIED OUT OF LIMITS DUE TO NO LIMITS IN THE SRM.; [08] RECEIVED FROM OSS NEW SUPPORT CLIP; MATERIAL USED 7075 T62TO CLAD .040' LOT# 1468510-2 PO# 847253-SWA. LOCATED AND DRILLED NEW CLIP PER SRM 51-40-05-0G-0 AND DWG 141A1160; [09] VERIFIED CORRECTIVE ACTION 8.<BR>OK TO ALODINE AND PRIME; [10] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON CLIP PER AMM 51-21-41-370-802 AND AMM 51-21-72-370-804. OK TO INSTALL; [11] VERIFIED CORRECTIVE ACTION 10.<BR>OK TO INSTALL; [12] UPDATED MEASUREMEMNT TABLE; [13] INSTALLED SUPPORT CLIB AT MAIN E&E BAY BS 360 BL0 PER SRM 51-40-02-0G-0 AND DWG 141A1160; [14] VERIFIED CORRECTIVE ACTION 13; [15] VERIFIED JOB COMPLETE

Part: SEAT TRACK — CORRODED (BS 386-465) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK LBL45 WL208.1 BS386 - BS399; BS420 - BS426; BS439 - BS458; BS474; BS465. ; / [01] BLENDED CORROSION FROM SEAT TRACK AT LBL 45.5 WL 208 BS386-399; BS420-426; BS439-458 AND BS465-474 ALL IAW SRM 53-00-52-1A-1 STEP 2 A; [02] VERIFIED REMOVAL OF CORROSION FROM SEAT TRACK AT LBL 45.5 WL 208 BS386-399; BS420-426; BS439-458 AND BS465-474 ALL IAW SRM 53-00-52-1A-1 STEP 2 A; [03] COMPLETED STEP 1 THROUGH 4 USING DIAL GAGE ID:ATS2678 S/N: UNKNOWN.; [04] CERTIFIED EVALUATION OF SEAT TRACKS; [05] ADDED SRM TO REFERENCE; [06] CERTIFIED CORRECTION IN REFERENCE; [07] ADDED CORRECTION TO STEP 1 THROUGH 4; [08] CERTIFIED CORRECTION OF AREA MATERIAL REMOVED FROM; [09] VERIFIED PARTIALS FOR STEPS 1-4; [10] STEP 5 COMPLETE.; [11] ALL STEPS 1-5 COMPLETE; [12] EDITED MEASURMENT 18.; [13] CERTIFIED MEASURMENT UPDATE.; [14] EDITED MEASUREMENTS 1-4.; [15] CERTIFIED MEASUREMENT EDIT; [16] EDITED MEASUREMENT 14.; [17] CERTIFIED EDIT.; [18] VERIFIED CORRECTIVE ACTIONS 12-17.<BR><BR>ALL WORK ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (BS 840-887) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK LBL25 WL208.1 BS840; BS846 - BS861; BS876 - BS887. ; / [01] UPDATED PARAMETER VALUES; [02] ACCOMPLISHED STEPS 1 AND 2; [03] VERIFIED STEP 1 AND 2 COMPLETE; [04] STEP 3 COMPLETE.; [05] EDITED MEASUREMENT TABLE ADDED FULL MPN TO MEASUREMENT 10.; [06] CERTIFIED MEASUREMENT CORRECTION.; [07] COMPLETED MEASUREMENT TABLE.; [08] VERIFIED STEP 3 COMPLETE AND CORRECTIVE ACTIONS 4-7.<BR><BR>ALL WORK ACCOMPLISHED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON SUPPORT ANGLE AT MAIN EBAY BS380 S-23L. REMOVED CORROSION IN AN AREA OF 1' X 1' IAW SRM 51-10-02-0G-0. UT INSPECTED BLENDED AREA IAW NDTM PART 4 51-00-00 PROCEDURE 2, REMAINING THICKNESS IS 0.035'. EVALUATED CORROSION ON SUPPORT ANGLE, FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW SRM 51-40-05-0G-0 AND DWG 143A7902. INSTALLED SUPPORT ANGLE PER SRM 51-40-02-0G-0 AND DWG 143A7902.

Part: SEAT TRACK — CORRODED (BS 483-520) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK LBL45 WL208.1 BS483; BS492; BS500+6 - BS500+15; BS500A+13 - BS500B+11; BS500C - BS500C+11; BS500D+9 - BS520. ; / [01] BLENDED CORROSION FROM SEAT TRACK AT LBL45.5 WL 208 BS483-492; BS500+6-500+15; BS500A+13-500B+11; BS500C-500C+11; BS500D+9-520 ALL IAW SRM 53-00-52-1A-1 STEP 2 A; [02] VERIFIED REMOVAL OF CORROSION FROM SEAT TRACK AT LBL45.5 WL 208 BS483-492; BS500+6-500+15; BS500A+13-500B+11; BS500C-500C+11; BS500D+9-520 ALL IAW SRM 53-00-52-1A-1 STEP 2 A; 09] CERTIFIED EDIT OF P/N.; [10] EVALUATED CORROSION ON PASSENGER CABIN SEAT TRACK LBL45 WL208.1 BS483; BS492; BS500+6 - BS500+15; BS500A+13 - BS500B+11; BS500C - BS500C+11; BS500D+9 - BS520. LARGEST AREA OF DAMAGE REMOVAL FOUND TO BE 0.025' ON TOP OF TRACK. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1.; [11] INSTALLED FOD PROTECTION FOR SEAT TRACK REMOVAL FROM BS480-BS520 LBL25-LBL60 PER 20-60-07-913-801; [12] REMOVED SEAT TRACK FROM BS480-BS520 LBL45 PER SRM 51-40-02-0-0; [13] RECEIVED NEW SEAT TRACK ON CUSTOMER RO NO ATSHFAB-100-303. SEAT TRACK FABRICATED PER BOEING DWG 143A5310; ATSHFAB-100-303 REV C. REFER TO ATS BUILD RECORD 543960. PART MARKED PER ATS QCM 4.35.26.; [14] LOCATED AND DRILLED NEW SEAT TRACK PER SRM 51-40-05; SRM 51-40-08; DWG#143A5300. OK TO INSTALL.;

Part: SEAT TRACK — CORRODED (BS 727B-833) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK LBL25 WL208.1 BS727B+3; BS727B+12 - BS727C; BS727C+3 - BS727C+13; BS727D - BS727D+10; BS727D+14 - BS747; BS747+5 - BS805; BS814; BS821 - BS833. ; / [01] COMPLETED STEPS 1-8; [02] VERIFIED STEPS 1 - 8 COMPLETE.; [03] STEP 9 COMPLETE.; [04] VERIFIED STEP 9 COMPLETE.<BR><BR>ALL WORK ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (BS 540-727B) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK LBL25 WL208.1 BS540 - BS554; BS556 - BS597; BS599 - BS611; BS630 - BS643; BS660 - BS675; BS688 - BS707; BS715 - BS727+11; BS727A+3 - BS727B. ; / [01] UPDATED PARAMETER VALUES; [02] ACCOMPLISHED STEPS 1 AND 2; [03] UPDATED STEP 2 MICROMETER ID:DIAL DEPTH GAUGE ID: ATS400 <BR>SERIAL #: UNKNOWN <BR>DATE: 08/2021 <BR>DUE: 08/2022; [04] VERIFIED CORRECTIVE ACTION 1-3; [05] STEP 3 COMPLETE.; [06] VERIFIED STEP 3 COMPLETE. <BR><BR>ALL WORK ACCOMPLISHED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON INTERCOSTAL IN MAIN E&E BAY BS359 S-23L. REMOVED CORROSION IAW SRM 51-10-02-0G-0, UT INSPECTED BLENDED AREA IAW NDTM PART 4 51-00-00 PROCEDURE 2, REMOVED CORROSION IN AN AREA OF 1.5'X0.4' PER SRM 51-10-02-0G-0. REPAIRED PER EA 21-153-03572.

Part: SEAT TRACK — CORRODED (BS 483-500D) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK LBL25 WL208.1 BS483; BS494 - BS500+13; BS500A+7 - BS500B+2; BS500B+14; BS500C - BS500C+13; BS500D+9 - BS520; BS500D+6. ; / [01] UPDATED MEASUREMENTS; [02] ACCOMPLISHED STEPS 1 AND 2; [03] STEP 1 COMPLETE. VERIFIED PARTIAL UPDATE OF STEP 2.; [04] ACCOMPLISHED STEP 3; [05] VERIFIED STEP 2 AND 3 COMPLETE; [06] STEP 4 COMPLETE.; [07] STEP 4 COMPLETE; [08] EDITED MEASUREMENT TABLE. ADDED FULL MPN TO MEASUREMENT 10; [09] CERTIFIED EDIT.; [10] COMPLETED MEASUREMENT TABLE.; [11] EDITED MEASURMENT 8.; [12] CERTIFIED EDIT.; [13] VERIFIED CORRECTIVE ACTIONS 8-12.<BR><BR>ALL WORK ACCOMPLISHED

Part: ANGLE — CRACKED · airframe 55,382 hrs · 27,558 cycles

SUPPLEMENTAL INFORMATION: CRACKED ANGLE AT CABLE QUADRANT BS 685+10 ON THE RT SIDE OF BL 0 BEAM WL 207 ; / [01] UPDATED STEP 1.; [02] UPDATED STEP 1 FOR FABRICATION.; [03] UPDATED PARTIAL STEP<BR>OK TO ALODINE AND PRIME; [04] UPDATED PARTIAL STEP 1.; [05] VERIFIED THE LOCATE AND DRILL PER SRM 51-40-05; CHEMICAL CONVERSION COATING AND PRIMER APPLICATION PER SRM 51-20-01 AND AMM 51-21-72-370-804. OK TO INSTALL THE ANGLE.; [06] INSTALLED NEW ANGLE AT CABLE QUADRANT BS 685+10 ON RT SIDE OF BEAM BL0 WL 207. COMPLETED STEP 1.; [07] VERIFIED INSTALLATION OF THE NEW ANGLE AT CABLE QUADRANT BS 685+10 ON RT SIDE OF BEAM BL0 WL 207 PER SRM 51-40-02 AND DWG#273A9110. STEP 1 COMPLETE; [08] REPLACEMENT OF ANGLE AT CABLE QUADRANT BS 685+10 ON RT SIDE OF BEAM BL0 WL 207 PER SRM 51-40-02 AND DWG#273A9110 IS COMPLETE.

Part: SUPPORT ANGLE — CRACKED (BS 927) · airframe 55,382 hrs · 27,558 cycles

FLOOR SUPPORT ANGLE CRACKED BS 927+10- BS927+11 BL 0 WL 208 ; / [01] REMOVED FLOOR SUPPORT ANGLE AT BS 927+10 BL 0 WL 208 IAW SRM 51-40-02; [02] CORRECTION OF BODY STATIONS. REMOVED FLOOR SUPPORT ANGLE AT BS 927-947 BL 0 WL 208 IAW SRM 51-4-02; [03] CERTIFIED; [04] LOCATED AND DRILLED NEW FLOOR SUPPORT ANGLE AT BS 927-947 BL 0 WL 208 SRM 51-40-05-0G-0 AND DWG 147A5400 SHEET 22. OK TO INSTALL.; [05] VERIFIED LOCATE AND DRILL OF THE BS 927-947 BL 0 WL 208 INTERCOSTAL TOP CHORD PER SRM 51-40-05-0G-0 AND DWG 147A5400 SHEET 22. OK TO INSTALL.; [06] INSTALLED BS 927-947 BL 0 WL 208 INTERCOSTAL TOP CHORD PER SRM 51-40-02- DWG 147A5400 SHEET 22.; [07] VERIFIED CORRECTIVE ACTION 6; [08] VERIFIED JOB COMPLETE

Part: BAFFLE — ELONGATED (FUSELAGE) · airframe 55,382 hrs · 27,558 cycles

FWD CARGO BAY BAFFLE BS 500C-500D RBL 25 HAS ELONGATED HOLE. EVALUATED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0. LOCATED AND DRILLED NEW FCB BAFFLE BS500C-BS500D; RBL 25 PER DWG 143A7505 AND SRM 51-40-02-0G-0. OK TO INSTALL; [07] VERIFIED LOCATED AND DRILLED NEW FCB BAFFLE BS500C-BS500D; RBL 25 PER DWG 143A7505 AND SRM 51-40-02-0G-0. OK TO INSTALL; [08] INSTALLED NEW FCB BAFFLE AND ALL NUTPLATES BS500C-BS500D; RBL 25. PER DWG 143A7505 AND SRM 51-40-02-0G-0; [09] VERIFIED INSTALLED NEW FCB BAFFLE AND ALL NUTPLATES BS500C-BS500D; RBL 25. PER DWG 143A7505 AND SRM 51-40-02-0G-0

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 55,382 hrs · 27,558 cycles

FLOOR SUPPORT CRACKED BS 312+10 TO 312+11 BL 0 WL 208 ; / [01] CORRECTION TO FAULT: FLOOR SUPPORT CRACKED BS 312+10 TO 312+11 LBL45 WL 208; [02] REMOVED DAMAGE FLOOR SUPPORT BS 312-328 LBL45 WL 208 IAW SRM 51-40-02-0G-0.; [03] CERTIFIED REMOVED OF DAMAGE FLOOR SUPPORT; [04] LOCATED AND DRILLED NEW FLOOR SUPPORT BS321-328 LBL45 WL 208 IAW SRM 51-40-05-0G-0; OK TO INSTALL.; [05] CERTIFIED LOCATE AND DRILL OF NEW FLOOR SUPPORT; [06] VERIFIED LOCATED AND DRILLED NEW FLOOR SUPPORT BS321-328 LBL45 WL 208 IAW SRM 51-40-05-0G-0; OK TO INSTALL.; [07] INSTALLED NEW FLOOR SUPPORT AT BS 312-328 LBL45 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A5400; [08] CERTIFIED INSTALLATION OF FLOOR SUPPORT AT BS 312-328 LBL45 WL 208; [09]

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,382 hrs · 27,558 cycles

STRINGER CLIP CRACKED BS 294.5 STRINGER 13 LT ; / [01] REMOVED STRINGER CLIP AT BS 294.5 STR. 13 L/H IAW SRM 51-40-01 PARA. 4 AND FIG 8. FABRICATED NEW STRINGER CLIP USING 7075T62 LOT #1464682-1 PER DWG. #141A1311; [02] VERIFIED CORRECTIVE ACTION 1; [03] APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO FABRICATED STRINGER CLIP IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02 PARA. 6; [04] REQUEST OK TO INSTALL STRINGER CLIP; [05] VERIFIED CHEMICAL CONVERSION AND PRIMER APPLICATION PER SRM 51-20-01-0G-0 AND SOPM 20-41-02 PARA. 6. OK TO INSTALL CLIP.; [06] INSTALLED FABRICATED STRINGER CLIP AT BS 294.5 STRINGER 13 L/H IAW SRM 51-40-02 PARA 4; [07] EDITED TO CORRECT REMOVAL REFERENCE TO READ SRM 51-40-02; [08] VERIFIED ED

Part: ANGLE — CORRODED (BS 500D LBL 25) · airframe 55,382 hrs · 27,558 cycles

CORROSION FWD CARGO BAY AFT BULKHEAD L/H LOWER BULKHEAD SUPPORT ANGLE I/B END APPROX BS 500D; LBL 25; WL 153 ; / [01] WORK WILL BE PERFORMED ON FAULT. TTG8Q009FXXB; [02] DUPLICATE CARD; ALL EVALUATIONS ARE ACCOMPLISHED ON TTG8Q009FXXB; [03] INADVERTENTLY USED INSP ROW IN STEP 2 INSTEAD OF MECH SIGN OFF. DUPLICATE CARD; ALL EVALUATIONS ARE ACCOMPLISHED ON TTG8Q009FXXB; [04] VERIFIED CORRECTIVE ACTION ENTRY 1-3. CARD COMPLETE.

Part: BAFFLE — ELONGATED (FUSELAGE) · airframe 55,382 hrs · 27,558 cycles

FWD CARGO BAY BAFFLE BS 440 - 460 LBL 25 HAS ELONGATED HOLE ; / [01] EVALUATED DAMAGED HOLES AND FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.; [03] REMOVED FCB BAFFLE BS440-BS460; LBL25; WL157-WL154. PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW FCB BAFFLE BS440-BS460; LBL25; WL157-WL154. PER DWG 143A7505; AND SRM 51-40-05-0G-0. OK TO INSTALL.; [05] VERIFIED CORRECTIVE ACTION 4. OKAY TO INSTALL; [06] INSTALLED NEW FCB BAFFLE BS440-BS460; LBL25; WL157-WL154. PER DWG 143A7505; AND SRM 51-40-02-0G-0; [07] VERIFIED CORRECTIVE ACTION 6.

Part: BAFFLE — ELONGATED (FUSELAGE) · airframe 55,382 hrs · 27,558 cycles

FWD CARGO BAY BAFFLE BS 460 - 480 LBL 25 HAS ELONGATED HOLE ; / [01] EVALUATED DAMAGED HOLES AND FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.; [03] REMOVED FCB BAFFLE BS460-BS480; LBL25; WL157-WL154. PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW FCB BAFFLE BS460-BS480; LBL25; WL157-WL154. PER DWG 143A7505; AND SRM 51-40-05-0G-0. OK TO INSTALL.; [05] VERIFIED CORRECTIVE ACTION 4. OKAY TO INSTALL; [06] INSTALLED NEW FCB BAFFLE BS460-BS480; LBL25; WL157-WL154. PER DWG 143A7505; AND SRM 51-40-02-0G-0; [07] VERIFIED CORRECTIVE ACTION 6.

Part: CARGO TRACK — DAMAGED (FWD CARGO) · airframe 55,382 hrs · 27,558 cycles

FWD CARGO BAY RAIL BS 500C+19 LBL RBL 8.5 HAS ELONGATED HOLE ; / [01] VERIFIED EWIS PROTECTION; [02] REMOVED DAMAGED SECTION OF CARGO RAIL 500C +10' TO 500D RBL 8.5 IAW SRM 53-00-53-2R-2 REP.2; [03] FABRICATED REPAIR PARTS; CHANNEL FILLER BAC1509-100146 7050-T76511 LOT#1464335-1 AND CHANNEL SPLICE 53100004-001;LOCATED;DRILLED;CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 53-00-53-2R-2 REP.2; [04] VERIFIED DAMAGED PORTION OF CARGO FLOOR TRACK RAIL REMOVED AT 500C +10' TO 500D RBL 8.5 PER SRM 53-00-53-2R-2 REP.2; [05] VERIFIED CORRECTIVE ACTION STEP #3; [06] HFEC INSPECTED TRIMMED EDGE OF CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND. CAL ID ATS1465.; [07] OK TO INSTALL REPAIR PARTS; [08] VERIFIED OK INSTALL REPAIR PARTS.; [09] INSTALLED REPAIR PARTS PER SRM 51-40-02-0G-0 AND SRM 53-00-53-2R-2 REPAIR 2; [10] VERIFIED CORRECTIVE ACTION STEP 9.; [11] VERIFIED REPAIR IS COMPLETE.

Part: COUNTERWEIGHT — CORRODED (RUDDER) · airframe 55,382 hrs · 27,558 cycles

RUDDER COUNTER BALANCE WEIGHT HAS CORROSION ; / [01] REMOVED AND REPLACED RUDDER COUNTER-BALANCE WEIGHT IAW CMM55-40-09 STEP 2.C.(2)(B) PAGE302 AND STEP 2.C.(3)PAGE704. SRM 51-60-07-0G-0 STEP5.A.(6)(C)1)2)<BR>CAL TOOL:<BR>ID#4077A; S/N 0297200716; [02] VERIFIED CORRECTIVE ACTION 1 COMPLETE

Part: SUPPORT ANGLE — CORRODED · airframe 55,382 hrs · 27,558 cycles

SUPPLEMENTAL INFORMATION: FLOOR SUPPORT ANGLE CORRODED STA 706+8; WL-208; RBL-60 ; / [01] CORRECTION TO FAULT SHOULD BE RBL-63; [02] REMOVED 1EA FASTENER AT BS 706+8 RBL 65 OF CREASE BEAM IAW SRM 51-40-02; [03] VERIFIED APPLICABILITY OF SRM 53-40-13-0I-1 AND SRM 53-40-13-1A-1. REMOVED DAMAGE ON FLOOR SUPPORT ANGLE AT BS 706+8; WL 208; RBL 65 IAW SRM 51-10-02. AREA OF DAMAGE REMOVED IS 2.2'X1.1'. ORIGINAL THICKNESS FOUND TO BE 0.071' IAW SRM 53040-13-0I-1. WILL REQUEST NDI TO VERIFY REMAINING THICKNESS.; [04] CORRECTION OF RBL. SHOULD BE RBL 63; [05] CORRECTION OF RBL. SHOULD BE RBL 63; [06] VERIFIED; [07] VERIFIED CORRECTIVE ACTION 2-5; [08] UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.068' ADJACENT TO 0.071'. <BR>EQUIP ID#: ATS2031 S/N: 170515011; [09] AREA OF DAMAGE REMOVAL FOUND TO BE IN LIMITS IAW SRM 53-40-13-1A-1 STEP 4.A.(2) FIG. 103 F WITH ONLY 0.003' MATERIAL LOSS 0F 0.071' ORIGINAL THICKNESS.; [10] VERIFIED DAMAGE REMOVAL ON INNER CHORD FOUND IN LIMITS PER SRM 53-40-13-1A-1; WHILE VERIFYING DEPTH OF DAMAGE REMOVAL; FOUND ADDITIONAL CORROSION ON LOWER WEB (REF. FAULT TTG8Q009K39K); [11] APPLIED CHEMICAL CONVERSION COATING TO DAMAGE REMOVAL AREAS IAW SRM 51-20-01. OK TO PRIME.; [12] VERIFIED CORRECTIVE ACTION STEP 11 COMPLETE; [13] APPLIED PRIMER TO DAMAGE REMOVAL AREAS IAW SOPM 20-41-02; [14] INSTALLED 1EA FASTENER AT BS 706+8 RBL 65 OF CREASE BEAM IAW SRM 51-40-02;

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 55,382 hrs · 27,558 cycles

LEFT HAND HORIZONTAL STABILIZER LOWER SKIN HAS A CRACK MEASURING APPROXIMATELY ONE INCH IN LENGTH AT STAB STATION 193.90 APPROXIMATELY 18.5 INCHES FROM REAR SPAR. / [01] REMOVED CRACK DAMAGE LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 APPROXIMATELY 18.5 INCHES FROM REAR SPAR L=1.75IN X W=0.80IN IAW SRM 55-10-01-2R-11 STEP 4.B.2(A) AND (B).; [02] VERIFIED DAMAGE REMOVED PER SRM 55-10-01-2R-11 STEP 4.B.2(A) AND (B).; [03] HFEC INSPECTED CUT OUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. <BR>EQUIP ID#: IS000450 S/N: N500D000M120071; [04] FABRICATED REPAIR PARTS; (1) DOUBLER 2024-T3 0.080IN THICK LOT # 1467098-1 AND (2) FILLER 2024-T3 0.063IN THICK LOT #1446328-1;IAW SRM 55-10-01-2R-11 STEP 4.G - L.; [05] VERIFIED CORRECTIVE ACTION #4; [06] APPLIED CHEMICAL CONVERSION COATING TO REPAIR PARTS AND BARE SURFACES OF THE SKIN IAW SRM 55-10-01-2R-11 STEP 4.M.; [07] VERIFIED CORRECTIVE ACTION STEP 6.; [08] APPLIED BMS 10-79 TYPE III PRIMER TO REPAIR PARTS AND REPAIR AREAS OF THE SKIN IAW SRM 55-10-01-2R-11 STEP 4.N.; [09] VERIFIED CORRECTIVE ACTION ITEM 8 - OK TO INSTALL REPAIR; [10] VALIDATED APPLICABILITY SRM 55-10-01-2R-11.; [11] INSTALLED REPAIR PARTS IAW SRM 55-10-01-2R-11 STEP 4.O & P.;

Part: SKIN — CORRODED (BS847-1007 S2L-R) · airframe 55,382 hrs · 27,558 cycles

MULTIPLE AREAS OF CORROSION ON UPPER FUSELAGE SKIN UNDER DORSAL FIN; BS 847-1007; S-2L TO S-2R ; / [01] REMOVED CORROSION ON EXTERNAL FUSELAGE SKIN BS908-BS1000 BETWEEN STR3L-STR3R WL308 I.A.W SRM 51-10-02-0G-0;SRM 53-00-01-1A-1 PAR 4.A(2)(A) FIG.103/ALLOWABLE DAMAGE 1 DETAILS C;D [16] VERIFIED DAMAGED AREAS OF SKIN UNDER DORSAL FIN; BS 847-1007; REPAIRED ON EA 21-153-03562 AND EA 21-153-03562-WIP1

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,382 hrs · 27,558 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-26R RBL22 WL153. CRACK ON STRINGER WAS FOUND TO 1.0' LENGTH AND IS OUT OF LIMITS PER SRM 53-00-03-1A-1. APPLIED PRIMER TO REPAIR PARTS IAW SRM 53-00-03-2R-1, AMM 51-21-72-370-804. VERIFIED APPLIED PRIMER TO REPAIR PARTS IAW SRM 53-00-03-2R-1, AMM 51-21-72-370-804. INSTALL THE STR26R REPLACEMENT SEGMENT; STR SPLICE; CLIP AND SHEAR TIE; [13] APPLIED SEALING AROUND REPAIR AND CIC IAW SRM 53-00-03-2R-1 REP.1; [14] VERIFIED STEPS 2-4; REPAIR SEALING AND CIC PER SRM 53-00-03-2R-1 REP.1.

Part: SUPPORT ANGLE — CORRODED (BS 947 RBL 12-14) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT AT AFT CARGO BAY BS947 LBL6; RBL12; RBL14; RBL20. MARKED. ; / [01] CORROSION ON SUPPORT FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED CORROSION FOUND OUT OF LIMITS DUE TO NO LIMITS STATED IN SRM; [03] REMOVED AFT BULKHEAD TO FLOOR SUPPORT AT ACB BS947; RBL23-LBL10; WL173 PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED AFT BULKHEAD TO FLOOR SUPPORT AT ACB BS947; RBL23-LBL10; WL173 PER SRM 51-40-05-0G-0 AND DWG 147A7500; DWG 149A8117; [05] VERIFIED CORRECTIVE ACTION 4; [06] OK TO INSTALL AFT BULKHEAD TO FLOOR SUPPORT; [07] VERIFIED OK TO INSTALL; [08] INSTALLED AFT BULKHEAD TO FLOOR SUPPORT AT ACB BS947; RBL23-LBL10; WL173 PER SRM 51-40-02-0G-0 AND DWG 147A7500; DWG 149A8117; DWG 1498110; [09] UPDATED PARTS TABLE; [10] REJECTED CORRECTIVE ACTION ENTRY 8.<BR><BR>IMPROPERLY INSTALLED DOME NUTPLATE ON FLOOR SUPPORT. FAULT CREATED; [11] PROPERLY INSTALLED DOME NUT PER SRM 51-40-02-0G-0 AND DWG 149A8117; [12] VERIFIED CORRECTIVE ACTIONS STEP 11.

Part: INTERCOOLER — CORRODED (BS 787 RBL7) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS788; BS787+8 RBL7. MARKED. ; / [01] EVALUATED CORROSION ON INTERCOSTAL; FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.; [03] REMOVED DAMAGED INTERCOSTAL;LOCATED AND DRILLED NEW INTERCOSTAL AT BS 787-807; RBL 7;STR 27R; IAW SRM 51-40-02-0G-0; 51-40-05-0G-0 AND DWG146A8130; [04] VERIFIED CORRECTIVE ACTION 3; [05] OK INSTALL INTERCOSTAL; [06] VERIFIED OK TO INSTALL; [07] INSTALLED NEW INTERCOSTAL AT BS 787-807; RBL7; STR27R; PER SRM 51-40-02-0G-0; AND DWG 146A8130; [08] VERIFIED CORRECTIVE ACTION ITEM 7.; [09] VERIFIED TASK IS COMPLETE.

Part: INTERCOSTAL — CORRODED (BS 767 RBL7) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS767+2 RBL7 ; / [01] EVALUATED CORROSION ON INTERCOSTAL; FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.; [03] REMOVED DAMAGED INTERCOSTAL AT BS 767-787;RBL7; STR 27R IAW SRM 51-40-02-0G-0.; [04] RECEIVED INTERCOSTAL FROM HEAT TREAT PO# 846710; [05] LOCATED AND DRILLED ACB INTERCOSTAL AT BS767 - BS787; RBL7; STR27 PER SRM 51-40-05-0G-0 AND DWG 146A8130. <BR>APPLIED CHEMICAL CONVERSION COATING TO INTERCOSTAL PER AMM 51-21-41-370-802; [06] VERIFIED CORRECTIVE ACTION ITEM 4 & 5.; [07] APPLIED CHEMICAL CONVERSION COATING TO INTERCOSTAL PER AMM 51-21-72-370-804. OK TO INSTALL; [08] APPLIED PRIMER TO INTERCOSTAL PER AMM 51-21-72-370-804. OK TO INSTALL; [09] VERIFIED ACTIONS 7 AND 8 OK TO INSTALL; [10] INSTALLED NEW INTERCOSTAL AT BS 767-787; RBL7; STR27R; PER SRM 51-40-02-0G-0; AND DWG 146A8130; [11] VERIFIED CORRECTIVE ACTION ITEM 10.; [12] VERIFIED TASK IS COMPLETE.

Part: SUPPORT CHANNEL — CORRODED (BS 261-268) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON MULTIPLE AREAS ON TOP SURFACE OF VIEWPORT CHANNEL BS 261.5 TO BS 268.5; LBL 2.6 TO RBL 2.6; WL 207.5. ; / [01] REMOVED CORROSION ON VIEWPORT CHANNEL SUPPORT BS261.5-BS268.5 LBL3-RBL3 WL207 ON NUTPLATES HOLES LOCATION REMAINING MATERIAL THICKNESS IS 0.032' ORIGINAL MATERIAL THICKNESS IS 0.040'AND FOUND TO BE OUT LIMITS PART TO BE REMOVED AND REPLACED ALL I.A.W SRM 51-10-02-0G-0;SRM 53-10-51-0I-2 ;SRM 53-10-51-1A-1 PAR 4.B(2)(A) FIGURE E.; [02] REMOVED DAMAGED VIEWPORT CHANNEL SUPPORT BS259-BS270 LBL3-RBL3 WL207.5 I.A.W SRM 51-40-02-0G-0; [03] VERIFIED CORRECTIVE ACTION ENTRIES 1. AND 2.; [04] LOCATED AND DRILLED NEW VIEWPORT CHANNEL SUPPORT BS259-BS270 LBL3-RBL3 WL207.5 I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 141A5210.OK TO INSTALL; [05] VERIFIED CORRECTIVE ACTION 4 OK TO INSTALL; [06] INSTALLED NEW VIEWPORT CHANNEL SUPPORT BS259-BS270 LBL3-RBL3 WL207.5 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5210.; [07] VERIFIED CORRECTIVE ACTION 6; [08] VERIFIED CARD COMPLETE

Part: SUPPORT — CORRODED (BS 747-807 LBL21) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS807 - BS747 LBL21. MARKED ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 767 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS1225 S/N UNKNOWN; SIDEWALL SUPPORT WILL BE REPLACED ON FAULT TTG8Q009EERR; [02] VERIFIED CORROSION OUT OF LIMITS PER SRM 53-00-53-1A-2 AND PART TO BE REPLACED ON FAULT #TTG8Q009EERR

Part: SHIELD — CORRODED (BS 847 RBL21) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON AFT SHIELD AT AFT CARGO BAY BS847+9 RBL21. ; / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED CORROSION FOUND OUT OF LIMITS DUE TO NO STATED LIMITS IN SRM; [03] LOCATED AND DRILLED NEW AFT SHIELD AT AFT CARGO BAY BS 847 TO 867 RBL 21 PER SRM 51-40-05-0G-0 AND DWG 146A0081; [04] VERIFIED STEPS 1-3.; [05] ASSIGNED PARTS; [06] VERIFIED LOCATED AND DRILLED NEW AFT SHIELD AT AFT CARGO BAY BS 847 TO 867 RBL 21 PER SRM 51-40-05-0G-0 AND DWG 146A0081

Part: WEB — CORRODED (BS 803-831 RBL26) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS803 - BS831 RBL26. MARKED. ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 810 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.045' FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING ATS TOOL ID ATS1225 S/N UNKNOWN; [02] VERIFIED DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1; [03] LOCATED ;DRILLED; DEBURRED AND INSTALLED NUTPLATES ON NEW ACB SUBTHRESHOLD WEB PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0;DWG 146A8340.; [04] VERIFIED LOCATED ;DRILLED; DEBURRED AND INSTALLED NUTPLATES ON NEW ACB SUBTHRESHOLD WEB PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0;DWG 146A8340.

Part: SUPPORT — CORRODED (BS 727D-767) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727D+7 - BS767 RBL21. MARKED ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 747 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS1225 S/N UNKNOWN; [02] VERIFIED DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] LOCATED; DRILLED; AND DIBERRED NEW FLOOR TO SIDEWALL SUPPORT AFT CARGO BAY BS 727+4-767; RBL 21 IAW DWG 146A7500; SRM 51-40-05-0G-0.; [04] VERIFIED LOCATED; DRILLED; AND DIBERRED NEW FLOOR TO SIDEWALL SUPPORT AFT CARGO BAY BS 727+4-767; RBL 21 IAW DWG 146A7500; SRM 51-40-05-0G-0.; [05] VERIFIED COMPLETED

Part: SUPPORT — CORRODED (BS 727-727C) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727+8; BS727+12; BS727B+10; BS727B+14; BS727C+14 LBL21. MARKED ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727C+7' REMOVED 0.020' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS1225 S/N UNKNOWN; [02] VERIFIED DAMAGE OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] LOCATED AND DRILLED ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS847; LBL21; WL156 PER SRM 51-40-05-0G-0 AND DWG 146A7500; [04] ASSIGNED PARTS; [05] VERIFIED LOCATED AND DRILLED ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS847; LBL21; WL156 PER SRM 51-40-05-0G-0 AND DWG 146A7500

Part: CARGO TRACK — CORRODED (BS 727C-747) · airframe 55,382 hrs · 27,558 cycles

CORROSION ON TRACK AT AFT CARGO BAY BS727C+17; BS747 LBL17. MARKED. ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727C+17; FOUND 0.015 REMOVED FROM ORIG 0.071 IN A 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [02] VERIFIED CORRECTIVE ACTION 1; [03] REMOVED ACB FLOOR TRACK BS 727+4- BS 867; LBL 17; WL 155 IAW SRM 51-40-02-0G-0.; [04] LOCATED; DRILLED; AND DEBURRED NEW ACB CARGO TRACK BS 727+4- BS 867; LBL 17; WL 155 IAW SRM 51-40-05-0G-0; DWG# 146A7500.; [05] VERIFIED CORRECTIVE ACTION 3 AND 4; [06] OK TO INSTALL CARGO TRACK; [07] OKAY TO INSTALL; [08] INSTALLED NEW ACB CARGO TRACK BS727+4 - BS867; LBL 17; WL 155 IAW SRM 51-40-02-0G-0 AND DWG# 146A7500.; [09] ADDED PARTS; [10] VERIFIED - INSTALLED NEW ACB CARGO TRACK BS727+4 - BS867; LBL 17; WL 155; [11] VERIFIED - INSTALLED NEW ACB CARGO TRACK BS727+4 - BS867; LBL 17; WL 155

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 55,382 hrs · 27,558 cycles

LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] CUT AND REMOVED CRACK DAMAGE LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER L=0.55IN X W=0.35IN IAW SRM 55-10-09-2R-4 STEP 4.B.[10] FABRICATED REPAIR PARTS; T-SECTION 7075-T76511 0.063IN THICK LOT # 1463116-1; ANGLE BAC 1490 7075-T62 0.063IN THICK LOT # 1464923-1; AND SHIM 2 (E.A) 7075-T6 0.016IN THICK LOT # 1439717-1 IAW SRM 55-10-09-2R-4 STEP 4.F - J.; [11] APPLIED CHEMICAL CONVERSION COATING TO REPAIR PARTS; BARE SURFACES AND CUT EDGES OF THE RIB IAW SRM 55-10-09-2R-4 STEP 4.K.; [12] VERIFIED CORRECTIVE ACTION ENTRIES 9.; 10. AND 11.<BR><BR>OK TO PRIME REPAIR PARTS; [13] APPLIED PRIMER TO REPAIR PARTS; BARE SURFACES AND CUT EDGES OF THE RIB IAW SRM 55-10-09-2R-4 STEP 4.L. OK TO INSTALL.; [14] VERIFIED CORRECTIVE ACTION ENTRY 13.<BR><BR>OK TO INSTALL REPAIR PARTS; [15] INSTALLED AND FILLET SEALED REPAIR PARTS IAW SRM 55-10-09-2R-4 STEP 4.M - Q.; [16] VERIFIED CORRECTIVE ACTION ENTRY 15.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 55,382 hrs · 27,558 cycles

LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 4TH VERTICAL STIFFENER IS CRACKED. ; / [01] CUT AND REMOVED CRACK DAMAGE LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 129.50; 4TH VERTICAL STIFFENER L=0.35IN X W=0.35IN IAW SRM 55-10-09-2R-4 STEP 4.B.;; [05] REMOVED 2 EACH CRACKS MARKED BY HFEC INSPECTION IAW SRM 55-10-09-2R-4 STEP 4.C. NEW DIMENSION ARE L=0.55IN X W=0.50IN.; [06] 1 EACH FASTENER HOLE NOT CRACKED; CRACKED HOLE ON 2ND VERTICICAL STIFFENER TASK CARD TTG8Q009E9ZL.; [08] REQUEST HFEC INSPECTION AFTER 2 EACH CRACK DAMAGE REMOVAL MARKED BY HFEC INSPECTION STEP 4 FOR CRACK FREE CONDITION IAW SRM 55-10-09-2R-4 STEP 4.C.; [09] ACCOMPLISHED HFEC INSP OF CUTOUT IAW B737 NDTM PART 6 51-00-00 PROC 23; NO CRACKS NOTED. <BR>TOOL ID ATS 1465 SN60004150296; [10] PERFORMED A GVI OF ALL AREAS WITHIN THE REPAIR AREA FOR CORROSION; EXISTING REPAIRS OR ANY OTHER DEFECTS IAW SRM 55-10-09-2R-4 STEP 4.E. NO DISCREPANCIES FOUND.; [11] FABRICATED REPAIR PARTS; T-SECTION 7075-T76511 0.063IN THICK LOT # 1463116-1; ANGLE BAC 1490 7075-T62 0.063IN THICK LOT # 1464923-1; AND SHIM 2 (E.A) 7075-T6 0.016IN THICK LOT # 1439717-1 IAW SRM 55-10-09-2R-4 STEP 4.F - J.;

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 55,382 hrs · 27,558 cycles

LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 2ND VERTICAL STIFFENER IS CRACKED. ; / [01] REMOVED LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STA 129.50 TO ACCESS REPAIRS IAW SRM 51-40-02-0G-0.; [02] CUT AND REMOVED CRACK DAMAGE LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 129.50; 2ND VERTICAL STIFFENER L=0.35IN X W=0.35IN IAW SRM 55-10-09-2R-4 STEP 4.B.; [03] VERIFIED CORRECTIVE ACTION 2; [04] REQUEST HFEC INSPECTION OF CUT EDGES OF STIFFENER; WEB AND EXISTING FASTENER HOLES WITHIN REPAIR AREA FOR CRACK FREE CONDITION IAW SRM 55-10-09-2R-4 STEP 4.C & D.; [05] ACCOMPLISHED HFEC INSP OF CUTOUT IAW B737 NDTM PART 6N 51-00-00 PROC 23; NO CRACKS NOTED. ACCOMPLISHED HFEC INSP OF FASTENER HOLES IN REPAIR AREAS IAW B737 NDTM PART 6 51-00-00 PROC 16; 1 EACH CRACK NOTED MARKED IN RED. <BR>TOOL ID ATS 1465 SN60004150296; [06] REMOVED 1 EACH CRACKS MARKED BY HFEC INSPECTION AT FASTENER HOLE LOWER CHORD IAW SRM 55-10-09-2R-5 STEP 4.C. NEW DIMENSION ARE L=0.90IN X W=0.60IN.; [11] FABRICATED REPAIR PARTS; T-SECTION 7075-T76511 0.063IN THICK LOT # 1463116-1; ANGLE BAC 1490 7075-T62 0.063IN THICK LOT # 1464923-1; FILLER 7075-T6 0.050IN THICK LOT # 1376846-2 AND SHIM 2 (E.A) 7075-T6 0.016IN THICK LOT # 1439717-1 IAW SRM 55-10-09-2R-5 STEP 4.G - K.;

Part: PANEL — CRACKED · airframe 55,382 hrs · 27,558 cycles

PANEL 195CL AFT EDGE RADIUS CORNER IS CRACKED. ; / FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4.B (6)REPAIR WILL BE ACCOMPLISHED IAW SRM 51-70-05-2R-6 AS DIRECTED PER SRM 53-40-70-2R-1 PAR 4.B (2) AND TABLE 202;REMOVED DAMAGED PLIES AND TAPER SANDED REPAIR AREA. NO CONTAMINATION OR WATER NOTED IAW SRM 51-70-05-2R-6.PARA 4.A-C. FABRICATED REPAIR PLIES ; THEN LAID UP TOOL SIDE PLIES FOR TWO STAGE CURE . VACUUM BAGGED ; LEAK CHECKED ; THEN SET TO CURE IAW SRM 51-70-05-2R-6 PARA 4 STEPS D - F; [07] REMOVED TOOL SIDE REPAIR DO TO VACUUM BAG FAILURE THEN PERFORMED DAMAGE REMOVAL & SURFACE PREPARATION PROCEEDURES IAW SRM 51-70-05-2R-6 PARA 4 STEPS A-C REF C REPAIR SRM 51-70-04-2R-6 FABRICATED REPAIR PLIES ;THEN LAID UP THE REPAIR & VACUUM BAGGED FOR PLY COMPACTION IAW SRM 51-70-04-2R-6 PARA 4 STEPS D-F; COMPLETED PLY COMPACTION; RE BAGGED THE REPAIR LEAK CHECKED & CURED THE TOOL SIDE REPAIR PLIES IAW SRM 51-70-04-2R-6 PARA 4 STEPS F & G . REF CAL TOOL HOT BONDER ID IS000678 SN 12071586. FABRICATED REPAIR PLIES ;THEN LAID UP THE BAG SIDE REPAIR ;VACUUM BAGGED LEAK CHECKED & SET TO CURE IAW SRM 51-70-04-2R-6 PARA 4 STEPS D-F CURED REPAIR PLIES USING HEATCON HOTBONDER ID: IS000678 S/N: 12071586; UNBAGGED IAW SRM 51-70-04-2R-6 PAR 4G-SEALED INNER SURFACE REPAIR PLIES USING 3501 LOT#1183B1111W; CURED; SANDED SMOOTH; CLEANED; AND REFINISHED BAG SIDE SURFACE IAW SRM 51-70-04-2R-6 4I AND AMM 51-21-99-300-802 PAR 3C(1).

Part: SUPPORT — CORRODED (BS 500 RBL 23) · airframe 55,382 hrs · 27,558 cycles

FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT CORRODED RBL23; BS 500+50; +52 ; / [01] CORRECT LOCATION OF DAMAGE IS BS 500C+10 AND 500C+12; RBL 23 WL 156. EVALUATED CORROSION AND FOUND DEEPEST LOCATION TO BE AT BS 500C+12 IN A 1'X1' AREA REMOVED 0.015 FROM ORIG 0.040. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ID ATS 2678 S/N UNKNOWN. FLOOR TO SIDEWALL SUPPORT TO BE REPLACED ON CUST CARD #TTG8Q009DVR6; [02] VERIFIED CORRECTIVE ACTION 1. <BR><BR>OUT OF LIMITS.<BR><BR>PART TO BE REPLACED ON TTG8Q009DVR6

Part: ANGLE — BROKEN (FUSELAGE) · airframe 55,382 hrs · 27,558 cycles

LOWER KEEL BEAM PANEL ATTACH ANGLE BROKEN; BS552; LBL6; WL140 ; / [01] REPLACED KEEL BEAM PANEL ATTACH ANGLE BS 552 LBL 6 IAW SRM 51-40-02-0G-0;IPC 53-12-11-25; [02] VERIFIED CORRECTIVE ACTION 2

Part: SUPPORT FITTING — CRACKED (ECS BAY) · airframe 55,382 hrs · 27,558 cycles

RIGHT ECS BAY AIR DUCT HANGER SUPPORT FITTING CRACKED; WL160; RBL6; BS545; AFT ATTACH POINT ; / [01] REMOVED AND REPLACED RIGHT ECS BAY AIR DUCT HANGER SUPPORT FITTING CRACKED;WI160;RB16;BS545;AFT ATTACH POINT PER SRM 51-40-02-0G-0 AND AIPC 36-13-01-01.; [02] VERIFIED CORRECTIVE ACTION 1

Part: SUPPORT — CORRODED (BS 500A RBL 23) · airframe 55,382 hrs · 27,558 cycles

FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT CORRODED RBL23; BS500A+2; +4; +6; +10;+14.5; +18.5; +26.5; +43; +45.5; +47.5; ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500A+6 RBL 23 WL 156. FOUND 0.015 TO BE REMOVED FROM ORIG 0.040 IN 1'X1' AREAS. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ID ATS 2678 S/N UNKNOWN; [02] VERIFIED CORRECTIVE ACTION 1.<BR><BR>OUT OF LIMITS.; [03] FABRICATED NEW FCB RH FLOOR TO SIDEWALL SUPPORT; BS 500A-500D; RBL23. LOCATED AND DRILLED; AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-40-05-0G-0; SRM 51-20-01-0G-0; DWG 143A7500. MATERIAL; BAC1496-444; #7075T62; LOT# 1457271-1. AND OK TO PRIME.; [04] VERIFIED CORRECTIV

Part: WEB — CORRODED (CARGO THRESHOLD) · airframe 55,382 hrs · 27,558 cycles

FWD CARGO BAY SUB THRESHOLD CORROSION; MEASURED BS440 TO AFT; BS440+14; +16; +18; +21-29; +30-31; +33; +36.5; AND +38.5 ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 440+18 RBL 29 WL 156. FOUND 0.015 TO BE REMOVED FROM ORIG 0.045 IN 1'X1' AREAS. FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DIAL DEPTH GAUGE ID ATS 2678 S/N UNKNOWN; [02] VERIFIED CORRECTIVE ACTION 1. <BR><BR>OUT OF LIMITS.; [03] LOCATED ;DRILLED ; DEBURRED; INSTALLED NUTPLATES ON NEW FWD CARGO BAY SUB THRESHOLD WEB PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 143A8330.; [04] VERIFIED LOCATED ;DRILLED ; DEBURRED; INSTALLED NUTPLATES ON NEW FWD CARGO BAY SUB THRESHOLD WEB PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 143A8330.

Part: SHIELD — CORRODED (BS 500 RBL 23) · airframe 55,382 hrs · 27,558 cycles

FWD CARGO BAY AFT FLOOR TO SIDEWALL SHIELD; RBL23; BS500+2; +6; +10; +18 ; / [01] EVALUATED CORROSION ON SHIELD; 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. <BR><BR>NO LIMITS PER SRM. PART TO BE REPLACED.; [03] LOCATED AND DRILLED NEW FWD CARGO BAY AFT FLOOR TO SIDEWALL SHIELD BS 500A TO 492 RBL 23 PER SRM 51-40-05-0G-0 AND DWG 143A0080; [04] VERIFIED STEPS 1-3; [05] ASSIGNED PARTS; [06] VERIFIED LOCATED AND DRILLED NEW FWD CARGO BAY AFT FLOOR TO SIDEWALL SHIELD BS 500A TO 492 RBL 23 PER SRM 51-40-05-0G-0 AND DWG 143A0080

Part: SUPPORT ANGLE — CORRODED (BS 460-500 LBL23) · airframe 55,382 hrs · 27,558 cycles

FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT ANGLE CORROSION; LBL23; BS460+10; BS480+6; BS500-2 ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 460+10 LBL 23 WL 156. FOUND 0.015 TO BE REMOVED FROM ORIG 0.040 IN 1'X1' AREAS. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ID ATS 2678 S/N UNKNOWN; [02] VERIFIED CORRECTIVE ACTION 1.<BR><BR>OUT OF LIMITS.; [03] RECEIVED NEW FCB LH FLOOR TO SIDEWALL SUPPORT; LOCATED AND DRILLED; FCB LH FLOOR TO SIDEWALL; BS396-500D; IAW SRM 51-40-05-0G-0; DWG 143A7500.; [04] VERIFIED RECEIVED NEW FCB LH FLOOR TO SIDEWALL SUPPORT; LOCATED AND DRILLED; FCB LH FLOOR TO SIDEWALL; BS396-500D; IAW SRM 51-40-05-0G-0; DWG 143A7500.

Part: SUPPORT FITTING — CRACKED (LT ECS BAY) · airframe 55,382 hrs · 27,558 cycles

LEFT ECS BAY AIR DUCT HANGER SUPPORT FITTING CRACKED; WL160; LBL6; BS545; AFT ATTACH POINT ; / [01] REMOVED AND REPLACED LEFT ECS BAY AIR DUCT HANGER SUPPORT FITTING CRACKED;WI160;RB16;BS545;AFT ATTACH POINT PER SRM 51-40-02-0G-0 AND AIPC 36-13-01-01.; [02] VERIFIED CORRECTIVE ACTION 1

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 54,950 hrs · 27,280 cycles

L1 DOOR SLIDE PARTIALLY FELL OUT OF CASE. / R&R SLIDE IAW MT.

Part: BRACKET — CRACKED · airframe 54,225 hrs · 26,821 cycles

LEFT HAND WHEEL WELL AT FROUNT SPAR BRACKET TO UPPER SHELF PANEL IS CRACKED / REMOVED AND REPLACED FRONT SPAR BRACKET PER SRM. 51-40-02

Part: LENS — MISSING (CABIN) · airframe 53,985 hrs · 26,657 cycles

R/H SIDE EMERGENCY EXIT ROW LIGHT LENS MISSING AT ROW 13. / INSTALLED EGRESS LIGHT COVER IAW SIP.

Part: FAIRING — ELONGATED (LWR FUSELAGE) · airframe 53,432 hrs · 26,296 cycles

193B PANEL HOLES ENLARGED OUT OF LIMITS / REMOVED AND REPLACED 193B PANEL REF B737 AMM 53-51-21 & SRM 51-20-07; TASK 14108

Part: GIRT BAR — INOPERATIVE (R1 DOOR) · airframe 53,188 hrs · 26,136 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR WILL NOT ARM. SECURED BAR PER AMM.

Part: SCUFF PLATE — CRACKED (FWD ENTRY DOOR () · airframe 52,353 hrs · 25,599 cycles

R1 DOOR SCUFF PLATE FOUND CRACKED / REMOVED R1 DOOR SCUFF PLATE IAW AMM 53-11-01-000-801 LEAD33 09MAY19. OK TO INSTALL INSP391 09MAY19 INSTALLED R1 DOOR SCUFF PLATE IAW AMM 53-11-01-420-801

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,353 hrs · 25,599 cycles

EMERGENCY LIGHT BATTERY M1675 FAILED CAPACITY CHECK. R&R BATTERY PACK IAW AMM.

Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

FLOORBOARD PANEL 221BF CRACKED FACE PLIES AND CORE AT AFT LEFT CORNER CUTOUT. REPAIRED FLOORBOARD PANEL 221BF PER SRM.

Part: SKIN — OUT OF TOLERANCE (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

(SKYLINE DTIP) INTERNAL SKIN REPAIR FROM STA 658-668 STR 6L - STR 7L REQUIRES REMOVAL AND REPLACEMENT / REPAIRED (SKYLINE DTIP) INTERNAL SKIN REPAIR FROM STA. 658-668 STR 6L - STR. 7L IAW EA 1-753-34740 REV IR AND ER 19-02723 REV IR

Part: VAPOR BARRIER — OUT OF TOLERANCE (WHEEL WELL LH) · airframe 52,353 hrs · 25,599 cycles

EXCESSIVE OIL CANNING AT THE L/H 663 VAPOR BARRIER LBL 32 WL 155 / L/H 662 VAPOR BARRIER FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0 REC'D NEW VAPOR BARRIER FRO OSS P/N 111A1151-3-ATSH7AB-101-201 TO BE INSTALLED ON WORK CARD N187950

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 52,353 hrs · 25,599 cycles

(SKYLINE DTIP) PASSENGER CABIN FLOOR PANEL 221EF REQUIRES REPLACEMENT ( REF: ESR 19-02402) OR REPAIR / REPAIRED (SKYLINE DTIP) PASSENGER CABIN FLOOR PANEL 221EF (REF:ESR 19-02402) IAW SRM 737 53-00-50-2R-1 PARA. 1. 57507R 2APR19

Part: COVER — CRACKED (ELEVATOR LH) · airframe 52,353 hrs · 25,599 cycles

LEFT HAND ELEVATOR HINGE COVER 334NT CRACKED / REMOVED + REPLACED LEFT HAND ELEVATOR HINGE COVER 334NT IAW SRM 51-40-05-0G-0 FIG 6; SRM 51-40-02-0G-0 PAR 9; AND DWG 183A3010 REV E

Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 52,353 hrs · 25,599 cycles

LOWER VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, RBL 9. / REPAIRED LOWER VAPOR BARRIER ATTACH ANGLE IAW ATS ER AND SWA EA

Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 52,353 hrs · 25,599 cycles

LOWER VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, LBL 9 / REPAIRED LOWER VAPOR BARRIER ATTACH ANGLE PER ATS ER AND SWA EA

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

FORWARD CARGO COMPARTMENT INTERCOSTAL BAFFLE CRACKED BETWEEN BS 440 TO BS 460, LBL 22. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

FORWARD CARGO COMPARTMENT INTERCOSTAL BAFFLE CRACKED BETWEEN BS 460 TO BS 480, LBL 22. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

FORWARD CARGO COMPARTMENT INTERCOSTAL BAFFLE CRACKED BETWEEN BS 410 TO BS 420, LBL 22. R&R INTERCOSTAL IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,353 hrs · 25,599 cycles

RT WING NR 5 SLAT NOSE SKIN CRACKED AT THE ACTUATOR RIB SLAT. REPAIRED SKIN IAW SRM.

Part: WEB — DAMAGED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

AFT CARGO DOOR SURROUND WEB DAMAGED BETWEEN BS 767 TO BS 787, RBL 21. R&R WEB IAW SRM AND DWG.

Part: STIFFENER — CRACKED (LT WHEEL WELL) · airframe 52,353 hrs · 25,599 cycles

FOUND CRACKED L/H VERTICAL STIFFENER BS 663 LBL 26 WL145 / LOCATED + DRILLED NEW L/H VERTICAL STIFFENER BS 663 LBL 26 WL 145 IAW SRM 51-40-05 + DWG 111A1001. PO# 737827. ISNTALLED NEW VERTICAL STIFFENER IAW SRM 51-40-02-0G-0 + DWG 111A1000. 56379U 03APR19

Part: STIFFENER — CRACKED (RT WHEEL WELL) · airframe 52,353 hrs · 25,599 cycles

FOUND CRACK R/H HORIZONTAL STIFFENER BS 663 RBL 20 WL152. / LOCATED AND DRILLED NEW STIFFNER ITEM 7530305 PO# 737827 PER SRM 51-10-02-0G-0; SRM 51-40-05-0G-0 AND BOEING DWG 111A1001 REV B 57335U 8/25/19 TO BE INSTALLED ON DEFECT# N187951 AT R/H BS663 RBL 20 WL 152.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

L1 DOOR THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 320 TO BS 346, LBL 63. R&R ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 308-343) · airframe 52,353 hrs · 25,599 cycles

L1 DOOR THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS. 308 TO BS. 343, LBL 60. / R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

RT WING-TO-BODY SUPPORT CRACKED AT BS 500D, OUTBOARD OF STR 19R. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

R1 DOOR THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 301 TO BS 323, RBL 58. R&R ANGLE PER SRM & DWG.

Part: SKIN — CRACKED (LT WING) · airframe 52,353 hrs · 25,599 cycles

WORKING FASTENERS ON #4 SLAT LEADING EDGE SKIN AT ATTACH POINT FOR ACTUATOR. / DUE TO CRACKS ON SKIN ONLY AT SLAT #4 LEADING EDGE SKIN ATTACH POINT FOR ACTUATOR SRM 57-42-01-2R-8 REPAIR 8 WAS PERFORMED 92385U 03/12/19

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

FLOORBEAM CORRODED AT BS. 986, BETWEEN LBL 35 TO LBL 45. REPAIRED CHORD IAW ER, SRM, AND EA.

Part: STRUCTURE — CORRODED (BS 951-992) · airframe 52,353 hrs · 25,599 cycles

R/H INNER CORD CORRODED BETWEEN BS. 951 TO BS. 992.8, RBL 52. / R&R CHORD IAW SRM AND DWG.

Part: BRACKET — CRACKED (LEFT WING) · airframe 52,353 hrs · 25,599 cycles

L/H I/B FLAP SEAL BRACKET ON T/E OF WING AT APPROX ORSS 261 IS CRACKED / REMOVED AND REPLACED L/H I/B FLAP SEAL BRACKET ON T/E OF WING AT APPROX ORSS 261 IAW SRM 51-40-02-0G-0 PAR 4 AND DWG 115A2930 REV B

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

STRINGER CLIP CRACKED AT BS 277, STR 10R. R&R STRINGER CLIP IAW SRM & DWG.

Part: STRUCTURE — CORRODED (BS 967-979) · airframe 52,353 hrs · 25,599 cycles

L2 DOOR INNER CHORD CORRODED BETWEEN BS. 967 TO BS. 979, LBL 53. / R&R CHORD IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

AFT CARGO R/H AFT ZEE CHANNEL CORRODED BETWEEN BS 867 TO BS 891, RBL 21. R&R ZEE ANGLE IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

AFT CARGO FORWARD SHIELD CORRODED BETWEEN BS 767 TO BS 787, RBL 21. R&R SHIELD IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

AFT CARGO LT ZEE CHANNEL CORRODED BETWEEN BS 727C TO BS 787, LBL 21. R&R ANGLE IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

AFT CARGO AFT SHIELD CORRODED AT BS 852, RBL 21. R&R SHIELD IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

FORWARD CARGO FOUND SHIELD CORRODED AT BS 432, RBL 21. R&R SHIELD IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

RT SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 21. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

FORWARD CARGO AFT SHIELD CORRODED BETWEEN BS 500 TO BS 514, RBL 21. R&R SHIELD IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

AFT CARGO RT FORWARD ZEE CHANNEL CORRODED BETWEEN BS 727C TO BS 767, RBL 21. R&R ZEE ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

FORWARD CARGO LT SIDEWALL SUPPORT CORRODED BETWEEN BS 459 TO BS 466, LBL 22. R&R ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 52,353 hrs · 25,599 cycles

INTERCOSTAL CRACKED FROM BS 344-360, LBL 11, WL 208. REMOVED AND REPLACED INTERCOSTAL IAW SRM-

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

L1 DOOR CUTOUT LOWER INNER CHORD CORRODED BETWEEN BS 312 TO BS 344, LBL 54. R&R CHORD IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

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

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 52,353 hrs · 25,599 cycles

INTERCOSTAL CRACKED FROM BS 344-360, BL 0, WL 208. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

FLOORBEAM CORRODED AT BS. 344, BETWEEN BL 0 TO LBL 45. REPAIRED FLOORBEAM PER ER AND EA.

Part: SKIN — CRACKED (RT WING LE FLAP) · airframe 52,353 hrs · 25,599 cycles

INBOARD CORNER ON RIGHT WING #3 L/E FLAP IS CRACKED. / REPAIRED-FLAP IAW ATS ER

Part: PANEL — CRACKED (LOWER EXT FUSELA) · airframe 52,353 hrs · 25,599 cycles

PANEL P191FR HAS A CRACKED CORNER / REPAIRED CRACKED CORNER OF WTB PANEL P191FR I.A.W 737 SRM 53-30-70-2R-1 PARA 1; 4D TABLE 202; 250 DEGREES FAHRENHEIT CURE PER 737 SRM 51-70-05 REPAIR 10; DAMAGE WAS PAST ALLOWABLE LIMITS I.A.W 737 SRM 53-30-70-1A-1 PARA 4B (1)

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 52,353 hrs · 25,599 cycles

AFT PASSENGER FLOOR BOARD 242XF CRACKED / REPAIRED CRACK IN AFT PASSENGER FLOOR BOARD 242XF PER SRM 53-00-50-2R-1 DAMAGE WAS BEYOND ALLOWABLE LIMITS PER SRM 53-00-50-1A-1 PARA 4F

Part: GUSSET — CRACKED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 52,353 hrs · 25,599 cycles

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

Part: SKIN — CRACKED (LT WING) · airframe 52,353 hrs · 25,599 cycles

L/WING #2 SLAT NOSE SKIN AT THE ACTUATOR RIB SLAT STN 322.71 HAS WORKING FASTENERS / REMOVED WORKING FASTENERS #2 SLAT NOSE SKIN AT ACTUA ACTUALOR RIB SLAT SKIN AND REPAIR AREA; PERFORMED HFEC OPEN HOLES AND COUNTERSINKS. 1 CRACK FOUND IN RIB SLAT STA 322.71 IN AFT HOLE. FABRICATED DOUBLER FROM 7075-T6. .071 AND FILLER 7075-T6. 063 AND PREFORMED REPAIR IAW SRM 57-42-01-2R-8

Part: SKIN — CRACKED (LT WING SLAT) · airframe 52,353 hrs · 25,599 cycles

L/H WING #1 SLAT NOSE SKIN AT THE ACTUATOR RIB SLAT STA. 451.97 CRACKED. / REPAIRED #1 SLAT NOSE SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,353 hrs · 25,599 cycles

RT WING LOWER SURFACE OF THE WING LEADING EDGE SLAT NOSE SKIN AT THE ACTUATOR RIB SLAT STATION 322.71 CRACKED AT FASTENER. REPAIRED NR 7 SLAT IAW SRM.

Part: VAPOR BARRIER — CRACKED (RT WHEEL WELL) · airframe 52,353 hrs · 25,599 cycles

'CUSTOMER REQUEST' REPAIR RH 663 VAPOR BARRIER AS REQUIRED / REPAIRED R/H 663.75 VAPOR BARRIER IAW 737-700 SRM 57-10-10-2R2 AND SRM 51-70-04-2R-0 AND 51-70-04-2R-10 DUE TO CRACK TOTAL SUM OUT OF ALLOWABLE LIMITS IAW SRM 57-10-10-1A-2 PARA 2J7 AND PARA 4D1 FIG 101

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 52,353 hrs · 25,599 cycles

'CUSTOMER REQUEST' REPAIR LH 663 VAPOR BARRIER AS REQUIRED / REPAIRED LH 663 VAPOR BARRIER PER SRM 57-10-10-2R-2 PARA 1C AND SRM 51-70-04-2R-10. DAMAGE WAS BEYOND ALLOWABLE LIMITS PER SRM 57-10-10-1A-2 PARA 4D(1)

Part: HANDLE — UNSECURE (L1 DOOR) · airframe 51,802 hrs · 25,230 cycles

L1 DOOR ASSIST HANDLE PULLED OFF. ATTACHED HANDLE PER AMM.

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 51,517 hrs · 25,039 cycles

LH MLG WW FWD WALL OB SIDE OF EXHAUST DUCT VAPOR BARRIER CRACKED. CRACK NOW MEASURES 11' LONG. TRANSFERRED FROM G577933. / APPLIED INTERIM REPAIR IAW SRM 57-10-10-1A-2.

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 51,517 hrs · 25,039 cycles

CRACK MEASURING 7' LONG ON VAPOR BARRIER IN LH WW; IB OF EXHAUST DUCT BETWEEN LBL 8 AND LBL 14. / APPLIED INTERIM REPAIR SEAL IAW SRM 57-10-10-1A-2.

Part: COVER — UNSECURE (CABIN) · airframe 51,194 hrs · 24,825 cycles

RT OVERWING EMERGENCY EXIT LIGHT COVER CAME OFF. SECURED COVER IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,136 hrs · 24,788 cycles

RT BULLNOSE EMERGENCY LIGHT INOP AT ROW 16. RELAMPED LIGHT PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 50,657 hrs · 24,475 cycles

FORWARD LT EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. R&R BATTERY PER AMM & DWG.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 50,657 hrs · 24,475 cycles

L1 DOOR SLIDE GIRT OUT OF ADJUST. ADJUSTED GIRT PER MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 50,511 hrs · 24,388 cycles

R1 DOOR EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 46,870 hrs · 22,041 cycles

RT EMERGENCY EXIT SIGN COVER LOOSE. R&R LIGHT ASSEMBLY PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,588 hrs · 21,255 cycles

L1 DOOR AFT EXTERNAL EMERGENCY EXIT LIGHT INOP. R&R BULB PER AMM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 45,588 hrs · 21,255 cycles

R1 DOOR CRACKED ON INTERNAL STRUCTURE ON HORIZONTAL BEAM. R&R DOOR IAW AMM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 45,588 hrs · 21,255 cycles

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

Part: SKIN — CRACKED (RT WING SLAT) · airframe 45,588 hrs · 21,255 cycles

RIGHT WING NR 6 SLAT SKIN AT ACTUATOR RIB CRACKED, INBD AFT HOLE. REPAIRED THE SKIN IAW SRM.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 44,642 hrs · 20,693 cycles

RIGHT STOW BIN EMERGENCY LIGHT CONNECTOR PIN NR 1 LOOSE AT ROW 22. SECURED PIN IAW SWPM.

Part: SIGN — LOOSE (CABIN) · airframe 44,324 hrs · 20,497 cycles

OVERWING DOOR OVERHEAD EMERGENCY EXIT SIGN LOOSE. R & R SIGN IAW AMM.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 43,073 hrs · 19,744 cycles

L1 DOOR SLIDE GIRT BAR OUT OF ADJUSTMENT. ADJUSTED GIRT BAR ASSEMBLY IAW AMM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 42,381 hrs · 19,321 cycles

R1 DOOR SLIDE LOOSE. SECURED SLIDE IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,060 hrs · 18,550 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 8. RELAMPED LIGHT IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500 - 500A, LBL 24. R & R INTERCOSTAL IAW SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 40,062 hrs · 17,967 cycles

RIGHT WING FIXED TE AFT OF PYLON LOWER SURFACE VERTICAL BRACKET CRACKED AT FWD ATTACH POINT LOWER FASTENER. R & R BRACKET IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

LEFT NR 1 COCKPIT WINDOW FRAME CRACKED IN UPPER AFT CORNER. REPAIRED FRAME IAW ER & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727B - 747, RBL 22. R & R SUPPORT IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

FORWARD CARGO BAY ON LOWER BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN LBL 24 TO RBL 24. R & R ANGLE IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 500 - 500D, LBL 24. R & R PLATE IAW SRM.

Part: HANDLE — CRACKED (EMERGENCY EXIT) · airframe 40,062 hrs · 17,967 cycles

RIGHT OVERWING EXIT DOOR LINER HANDLE HOUSING CRACKED. R & R HANDLE IAW AMM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 500A - 500D, RBL 24. REPAIRED SUPPORT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

RIGHT LOWER FRAME WEB HOLE NEXT TO INNER CHORD CRACKED AT BS 727, WL 200. REPAIRED WEB IAW EA.

Part: HANDLE — CRACKED (EMERGENCY EXIT) · airframe 40,062 hrs · 17,967 cycles

LEFT OVERWING EXIT DOOR LINER HANDLE HOUSING CRACKED. R & R HANDLE IAW AMM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

FORWARD CARGO BAY ATTACH ANGLE FOR INTERCOSTAL CRACKED AT BS 400, STRINGER 26L. R & R ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

AIR CONDITIONING BRACKET FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

AIR CONDITIONING BRACKET FRAME CRACKED AT BS 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

AIR CONDITIONING BRACKET FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

AIR CONDITIONING BRACKET FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

AIR CONDITIONING BRACKET FRAME CRACKED AT BS 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

FRAME CRACKED AT BS 360, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

AIR CONDITIONING BRACKET FRAME CRACKED AT BS 727A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: SPLICE PLATE — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

SEAT TRACK HORIZONTAL FLANGE SPLICE PLATE CRACKED AT BS 727B, LBL 45. REPAIRED SPLICE PLATE IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 40,062 hrs · 17,967 cycles

INTERIOR SEAT TRACK FLANGE FWD CRACKED AT BS 727B, RBL 25, INBD FWD HOLE. REPAIRED FLANGE IAW ER & EA.

Part: RETAINER — LOOSE (L1 DOOR) · airframe 40,062 hrs · 17,967 cycles

L1 DOOR EMER EVAC SLIDE COVER GIRT BAR RETAINER LOOSE. R & R RETAINER IAW SRM.