N7822A

Part: BRACKET — LOOSE (GIRT BAR) · airframe 68,703 hrs · 35,150 cycles

AFT ENTRY DOOR GIRT BAR BRACKET LOOSE<[01] TIGHTEND BRACKET PER SIP

Part: SEAL — CRACKED (ZONE 300) · airframe 68,472 hrs · 35,010 cycles

L/H HORIZONTAL UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED SLIDER PER AMM 53-31-31.

Part: SEAL — CRACKED (ZONE 300) · airframe 68,472 hrs · 35,010 cycles

L/H HORIZONTAL LOWER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED LOWER SLIDER PER AMM 53-31-31.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,391 hrs · 34,337 cycles

LH AFT EXTERIOR EMER EXIT LIGHT OUT<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801-NG (SLIDE/OVERWING LIGHT - LAMP REPLACEMENT - PERMANENT)]

Part: SLIDE — UNSECURE (PAX DOOR) · airframe 66,881 hrs · 34,028 cycles

FWD ENTRY EMER SLIDE CASING CAME LOOSE WHEN OPENING DOOR<[01] ACCOMPLISHED MT 725-61-06 REM/INSTL PER M/M 25-66-01

Part: GIRT BAR — EXPOSED (ZN 800 DOOR) · airframe 65,740 hrs · 33,354 cycles

AFT LEFT SERVICE DOOR SLIDE EXPOSED<[01] ADJUSTED AFT SERVICE DOOR SLIDE GIRT BAR AND FLAP; REF AMM 25-66-01. A/C OK FOR SERVICE

Part: FLANGE — DAMAGED (ZN 300 STABILIZE) · airframe 65,627 hrs · 33,285 cycles

OUT OF ROUND HOLE WITH ADJACENT GOUGE TO FLANGE SURFACE; LH HORIZONTAL STAB RIB AT STAB STA 129.50; LOWER OB FLANGE 23.5' FROM FWD EDGE.<[01] REPAIRED DAMAGE IAW EA 23-155-02777

Part: WEB — CORRODED (ZN 100 FUS LOWER) · airframe 65,627 hrs · 33,285 cycles

FCB SUB THRESHHOLD WEB IS CORRODED FROM BS 480+1 - 460+11; RBL 32; WL 32 CORRECT WL 157<[01] UPDATED STEP 5;[02] UPDATED STEP 6;[03] UPDATED STEP 6 AND 7;[04] SRM 53-30-15-1A-1 FOUND TO BE APPLICABLE; BLENDED MULTIPLE CORROSION AT FBC SUB THRESHOLD WEB BS 480+1 - 460+11; RBL 32; WL 157; WORK AREA; L 1.5' X W 1.0' X D 0.009'; ORIGINAL THICKNESS 0.045'; REMAINING THICKNESS 0.039; DEEPEST FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1; USE DEPTH GAUGE ID:ATS401 DUE:10/23; REMOVED SUB THRESHOLD FCB FROM BS 440 TO BS 492; IAW SRM 51-40-02-0G-0; INSTALLED NUTPLATES ON NEW SUBTHRESHOLD WEB IAW SRM 51-40-02-0G-0 AND DWG 143A8330; ID: 0013; REV: A ; APPLIED BMS 10-11 TYPE 2 ANAMEL IAW SOPM 20-41-02; APPLIED CIC IAW AMM 51-21-91-620-802; INSTALLED NEW SUB THRESHOLD ON FCB BETWEEN BS 440 TO BS 492; RBL 32; WL 157 IAW SRM 51-40-02-0G-0 AND DWG 143A8330; ID:: 0015; REV: A;[05] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 4 AND MEASUREMENT TABLE.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 65,627 hrs · 33,285 cycles

AFT CARGO BAY; AFT CORNER SCUFF PLATE CRACKED<[01] UPDATED STEP 5.;[02] COMPLETED STEP 5.;[03] COMPLETED STEP 6.;[04] REMOVED PROTECTIVE COATINGS FROM SCUFF PLATE PRIOR TO WELDING PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2) AND SOPM 20-30-02. WELDED CRACKED RADIUS OF SCUFF PLATE PER SRM 53-30-15-2R-1 PARAGRAPH 4.B. (4). PT INSPECTED AREA IAW SOPM 20-20-02. SANDED THE WELD REPAIR AREA PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(5). APPLIED CHEMICAL CONVERSION COATING IAW SOPM 20-43-03. APPLIED TWO COATS OF BMS 10-11 TY1 PRIMER IAW AMM 51-21-72-370-804.;[05] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 4.

Part: RETAINER — CRACKED (ZN 500 LEFT WING) · airframe 65,627 hrs · 33,285 cycles

L/W T/E PANEL 551GB AFT SEAL RETAINER IS CRACKED<[01] REPLACED L/W T/E PANEL 551GB AFT SEAL RETAINER PER AMM 20-50-11.;[02] CORRECTION: REPLACED L/W T/E PANEL 551GB AFT SEAL RETAINER PER AMM 20-50-11.;[03] CORRECTION: REPLACED L/W T/E PANEL 551GB AFT SEAL RETAINER PER AMM 20-50-11.<BR>SCREWGUN ID: ATS2589 EXP:08/2024;[04] UPDATED INSTALLED PART SIGN OFF;[05] UPDATED INSTALLED PART SIGN OFF;[06] VERIFIED CORRECTIVE ACTION 1-5

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 65,627 hrs · 33,285 cycles

LH HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 111.10; 3RD VERTICAL STIFFENER IS CRACKED.<[01] UPDATED STEP 2;[02] REPAIRED L/H HORIZONTAL STABILIZER INSPAR RIB; (STAB. STA. 111.10) 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4.;[03] VERIFIED STEPS 4 & 5 AND MEASUREMENT TABLE

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 65,627 hrs · 33,285 cycles

LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED.<[01] SRM 55-10-09-2R-4 STEP 4. E. INSPECTION FOUND DAMAGE ADJACENT TO REPAIR AREA; GENERATED TTG8Q00NBZEC; SEE SUB-STEP 9.;[02] REPAIR OF L/H HORIZONTAL STAB INSPAR RIB 3RD VERTICAL STIFFENER AT STAB STA 129.50 AND OUT OF ROUND HOLE ON LOWER FLANG ACCOMPLISHED ON FAULT TTG8Q00NBZEC REFERANCE EA 23-155-02777;[03] ?REFER TO FAULT TTG8Q00NBZEC WHERE EA 23-155-02777 WAS ADDED AS A SUBTASK?;[04] VERIFIED CORRECTIVE ACTION COMPLETE. VERIFIED MEASUREMENT TABLE.

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 65,627 hrs · 33,285 cycles

WING CENTER SECTION HAS A CRACKED CABLE INTERCOSTAL ATTACH ANGLE AT BS 685+7; LBL 24; WL 203<[01] UPDATED STEPS 1-4;[02] INSTALLED NEW ANGLE AT BS 685+7; LBL 24; WL 203 PER SRM 51-40-02-0G-0 AND DWG 273A9110;[03] VERIFIED CORRECTIVE ACTION #2.<BR>VERIFIED MEASUREMENTS.

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 65,627 hrs · 33,285 cycles

WING CENTER SECTION HAS A CRACKED CABLE INTERCOSTAL ATTACH ANGLE AT BS 685+7; RBL 24; WL 203<[01] UPDATED STEPS 1-4;[02] INSTALLED NEW ANGLE AT BS 685+7; RBL 24; WL 203 PER SRM 51-40-02-0G-0 AND DWG 273A9110;[03] VERIFIED CORRECTIVE ACTION #2.<BR>VERIFIED MEASUREMENTS.

Part: SKIN — CRACKED (ZN 300 STABILIZE) · airframe 65,627 hrs · 33,285 cycles

LH HORIZONTAL STABILIZER LOWER SKIN - .7' CRACK FOUND 27' FROM FWD EDGE AT RIB STA 184.70<[01] REPAIRED PER EA 23-155-02717 WITH REPETITIVE INSPECTION PROGRAM DEFINED IN EA 23-155-02717-INSP.';[02] TASK CARD COMPLETE.

Part: FRAME — CORRODED (ZN 100 FUS LOWER) · airframe 65,627 hrs · 33,285 cycles

CORROSION ON FRAME CHORD AT AREA AFT OF FWD CARGO BAY BS500D RBL8 WL151.<[01] VERIFIED CORROSION REMOVED; THE REQUESTED NDT INSPECTIONS IS FOR ENGINEERING SUPPORT.;[02] COMPLETED STEP 6.;[03] REJECTED: SEE TTG8Q00NJT8E AND TTG8Q00NJTH5;[04] ACCOMPLISHED EA 23-153-02719 (N7822A - ATS(PAE) - REPAIR TO FAILSAFE CHORD BS 500D WL 151;[05] VERIFIED.<BR>VERIFIED MEASUREMENTS.

Part: PANEL — CRACKED (ZN 500 LEFT WING) · airframe 65,627 hrs · 33,285 cycles

WING CENTER SECTION HAS A CRACKED BREAK PANEL AT BS 540; LBL 1; WL 207<[01] UPDATED STEPS 1;2;[02] UPDATED STEP 3;[03] UPDATED STEP 3 ADDED REFERENCE;[04] CERTIFIED CHANGE TO STEP 3;[05] UDATED STEP 4 INSTALLED BREAK PANEL;[06] UPDATED MEASUREMENT TABLE;[07] UPDATED PARTS;[08] TASK COMPLETE

Part: SKIN — CRACKED (ZN 300 STABILIZE) · airframe 65,627 hrs · 33,285 cycles

LH HORIZONTAL STABILIZER LOWER SKIN - .7' CRACK FOUND 18' FROM FWD EDGE AT RIB STA 193.90<[01] REFER TO FAULT TTG8Q00N5DVD WHERE EA 23-155-02717 WAS ADDED AS A SUBTASK;[02] VERIFIED CORRECTIVE ACTION 1

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 65,627 hrs · 33,285 cycles

CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-22R WL172. MARKED<[01] UPDATED STEPS 2-3;[02] UPDATED STEPS 6-8;[03] PARTIAL STEPS 6-7-8;[04] PARTIAL UPDATE STEPS 6 AND 7;[05] COMPLETED STEP 7 AND 8.;[06] STEP 3 COMPLETE;[07] REMOVED DAMAGED STR SECTION BETWEEN BS 500D+10 AND BS 540 S-22R; REPAIRED STRINGER 22R SRM 53-00-03-2R-1 AND EA#23-153-02702;[08] VERIFIED MEASUREMENT TABLE.;[09] VERIFIED CORRECTIVE ACTION 7.

Part: PRESSURE DECK — CRACKED (ZN 100 FUS LOWER) · airframe 65,627 hrs · 33,285 cycles

HORIZONTAL PRESSURE DECK CRACKED BS664.5; WL 202; LBL52 APPROX 1 INCH IN LENGTH. MARKED WITH BLACK SHARPIE.<[01] REPAIRED HORIZONTAL BEADED PRESSURE DECK WEB BETWEEN STA 663.75 TO 675 LBL 30 TO LBL 60 PER SRM 53-40-51-2R-2. FIG. 203.;[02] VERIFIED CORRECTIVE ACTION #1;[03] REPAIRED CRACK IN HORIZONTAL PRESSURE DECK BS 664.5; WL 202; LBL 52 PER SRM 53-40-51-2R-2.

Part: FRAME — CRACKED (ZN 200 FUS TOP) · airframe 65,627 hrs · 33,285 cycles

FED CUTOUT SURROUND STRUCTURE - CRACK ON UPPER CHORD FRAME ASSY BS 312 STR-5L<[01] REQUEST NDI TO VERIFY CRACK AND IF CRACKED MARK ENDS OF CRACK BS 312 STR 5L UPPER RADIUS OF FRAME;[02] ACCOMPLISHED HFEC SURFACE SCAN IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. CRACK CONFIRMED; MEASURED AT L: 0.2' MARKED.<BR><BR>EQUIPMENT USED: NORTEC 600 ID: ATS1465 CAL DUE: 09/2023;[03] UPDATED MEASUREMENT TABLE;[04] REPAIRED CRACK BS 312 STR 5L ON M-22-153-01244; TTG8Q00N56CS;[05] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 4 AND MEASUREMENT TABLE.

Part: RETAINER — CRACKED (ZN 600 RIGHT WIN) · airframe 65,627 hrs · 33,285 cycles

RIGHT WING T/E VERTICAL SEAL RETAINER IS CRACKED AT ORSS 268 JUST ABOVE AFT PYLON FAIRING TIP<[01] REMOVED AND REPLACED RIGHT WING T/E VERTICAL SEAL RETAINER IAW SRM 51-40-02-0G-0;[02] JOB COMPLETE.;[03] VERIFIED MEASUREMENTS.

Part: WEB — CRACKED (ZN 600 RIGHT WIN) · airframe 65,627 hrs · 33,285 cycles

RIGHT WING T/E ORSS 280 TRANSVERSE WEB O/B L-CLIP ATTACHED TO DEFLECTION CONTROL RIB IS CRACKED<[01] PARTIAL UPDATE STEPS 1 AND 2;[02] COMPLETED STEPS 1 AND 2;[03] TASK COMPLETE.

Part: VALVE — OVERSERVICED (ZN 100 FUS LOWER) · airframe 65,525 hrs · 33,220 cycles

DURING DESCENT AT APPROXIMATELY 27;000 FEET CREW NOTICE ABNORMAL SMELL THROUGHOUT COCKPIT AND CABIN. SMELL DESCRIBED AS WAXY OR OILY.<[01] COMPLIED WITH SMOKE AND FUMES CONDITIONAL INSPECTION PER MM O5-51-56. FOUND A HYD SYSTEM SERVICED T0 96% AND B SYSTEM AT 106%. DRAINED AND SERVICED PER AMM 12-12-00. REPLACED A&B RESERVOIR CROSS FITTING CHECK VALVES PER AMM 29-09-04. REPLACED RECIRC FAN FILTER PER MM 21-25-01 AND WATER SEPARATOR SOCKS PER MM 21-51-05.

Part: GIRT BAR — LOOSE (ZN 200 FUS TOP) · airframe 65,475 hrs · 33,187 cycles

F/A REPORTS L1 GIRT BAR LOOSE<[01] RESECURED GIRT BAR BRACKET PER SIP

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 64,495 hrs · 32,549 cycles

RIGHT WING - FIXED LOWER TE PANEL WIGGLE PLATE OTB OF #6 FLAP SUPPORT CRACKED.<[01] REMOVED AND REPLACED RIGHT WING T/E PANEL WIGGLE PLATE PER AMM 57-50-02.;[02] REMOVED AND REPLACED RIGHT WING T/E PANEL WIGGLE PLATE PER AMM 57-50-02.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,495 hrs · 32,549 cycles

MULTIPLE EMERGENCY LIGHT BATTERIES FAILED CAPACITY CHECK.<[01] PERFORMED DEEP CYCLE AND RECHECKED CAPACITY FOR FAILED BATTERIES IAW AMM 33-51-06. FOUND BATTERY AT M1672 TO BE THE ONLY ONE TO FAIL AFTER DEEP CYCLE. REMOVED AND REPLACED BATTERY AT M1672 LOCATION REFERENCING AMM 33-51-06. OPS CHECK GOOD.

Part: BEAM — CRACKED (ZN 500 LEFT WING) · airframe 64,495 hrs · 32,549 cycles

LEFT WING- AFT FLAP DEFLECTION SUPPORT BEAM UPPER BRACKET CRACKED<[01] ACCOMPLISHED OF L/H WING AFT FLAP FIXED TRAILING EDGE DEFLECTION SUPPORT BEAM UPPER TAB PER SRM 57-51-02-2R-3 REPAIR 3.

Part: BRACKET — CRACKED (ZN 500 LEFT WING) · airframe 64,495 hrs · 32,549 cycles

LEFT WING-AFT TRAILING EDGE UPPER PANEL SUPPORT BRACKET CRACKED JUST OUTBOARD OF #3 FLAP TRACK<[01] REMOVED AND REPLACED LEFT WING-AFT TRAILING EDGE UPPER PANEL SUPPORT BRACKET PER SRM 51-40-02.

Part: BEAM — CRACKED (ZN 600 RIGHT WIN) · airframe 64,495 hrs · 32,549 cycles

RIGHT WING - AFT FLAP DEFLECTION BEAM UPPER TAB CRACKED.<[01] REMOVED DAMAGED UPPER TAB FROM DEFLECTION CONTROL RIB; LOCATED AND DRILLED REPAIR PART PER SRM 57-51-02-2R REPAIR 3.;[02] REPAIRED RH WING AFT FLAP DEFLECTION BEAM UPPER TAB IAW SRM 57-51-02-2R-3

Part: RADOME — CRACKED (ZN 100 FUS LOWER) · airframe 64,019 hrs · 32,235 cycles

DURING INTERNAL DVI ON NOSE RADOME FOUND A 3 CRACK AT THE 10 O CLOCK POSITION LOOKING FROM AFT.<[01] REMOVED 14 OUT OF 16 RADOME BOLTS.;[02] R/R NOSE RADOME PER AMM 53-52-00.

Part: LIGHT — LOOSE (OVERWING EXIT) · airframe 61,093 hrs · 30,307 cycles

EMERGENCY EXIT SIGN LOOSE OVER WING EXIT AIRCRAFT RIGHT / [01] REINSTALLED EMERGENCY LIGHT COVER AT OVER WING EXIT SIGN PER AMM 33-51-04

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 60,782 hrs · 30,107 cycles

R/H OVERWING EXTERIOR EMERGENCY LIGHT INOP ; / [01] RELAMPED R/H EXTERIOR OVERWING EMERGENCY EXIT LIGHT IAW B737 AMM 33-51-04.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 60,732 hrs · 30,078 cycles

PANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES. ; / [01] REPLACED PANEL 193B PER SRM 51-40-02

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 60,082 hrs · 29,665 cycles

SUPPLEMENTAL INFORMATION: FWD ENTRY DOOR SLIDE GIRT BAR HARD TO RELEASE FROM FROM FLOOR ATTACHMENTS ; / [01] REMOVED DEBRIS FROM FWD ENTRY DOOR GIRT BAR FLOOR ATTACH POINTS PER SIP AND LUBED LATCHES

Part: SLIDE — DETACHED (L1 DOOR) · airframe 60,034 hrs · 29,640 cycles

FRONT ENTRY EMERGENCY SLIDE DETACHED FROM ITS COMPARTMENT AFTER FLIGHT ATTENDANT CORRECTLY SECURED GIRT BAR FROM ITS ARMED POSITION. FRONT ENTRY DOOR WAS UNABLE TO BE FULLY OPENED ; / [01] CW MT 725-61-06

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,949 hrs · 29,584 cycles

EMERGENCY EXIT AISLE LIGHTS AT SEAT ROWS 9CBA AND 17CBA ARE INOP ; / [01] REMOVED; REPLACED AND PERFORMED GOOD OPERATIONAL CHECK OF EMERGENCY EXITS AISLE LIGHT LAMPS AT SEAT ROWS 9CBA AND 17CBA PER AMM 33-51-03-960-801; [02] VERIFIED REMOVED; REPLACED AND PERFORMED GOOD OPERATIONAL CHECK OF EMERGENCY EXITS AISLE LIGHT LAMPS AT SEAT ROWS 9CBA AND 17CBA PER AMM 33-51-03-960-801.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 59,949 hrs · 29,584 cycles

RIGHT OVERDOOR EXIT SIGN DOES NOT ILLUMINATE; OTHER LIGHTS RELATED TO M1675 BATT PACK OPERATE CORRECTLY. ; / [01] FOUND 7822 CAME IN WITH D40042J CONNECTOR PART NUMBER BACC65AK221P SHOULD BE BACC65AK211P PER WDM EQUIPMENT LIST. CONNECTOR DID NOT MATE PROPERLY WITH THE PLUG-SIDE CONNECTOR AND THUS WOULD HAVE ONLY WORKED INTERMITTENTLY. REMOVED AND REPLACED D40042J INSTALLING CORRECT PN CONNECTOR PER WDM 33-1-12 AND SWPM 20-72-24. PERFORMED A GOOD OPS CHECK OF L1063 PER AMM 33-51-00-710-801; [02] VERIFIED CORRECTIVE ACTION 1. CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,949 hrs · 29,584 cycles

LEFT EMERGENCY LIGHTING SYSTEM GROUND ILLUMINATION LIGHT DOES NOT ILLUMINATE ; / [01] RELAMPED LEFT GROUND ILLUMINATION LIGHT; LIGHT STILL DOES NOT ILLUMINATE PER TASK 33-51-04-960-801<BR>.; [02] VERIFIED RELAMPED LEFT GROUND ILLUMINATION LIGHT; LIGHT STILL DOES NOT ILLUMINATE PER TASK 33-51-04-960-801; [03] UPON FURTHER INVESTIGATION; FOUND CONN D10716 DISCONNECTED FROM EMERGENCY EXIT LIGHT BATT PACK M1670. CONNECTED D10716 PER SWPM 20-60-06. PERFORMED GOOD TEST OF EMERGENCY LIGHTING GROUND ILLUMINATION LIGHTS PER AMM 33-51-00-710-801.<BR>ACCESSED AND RESTORED AIR RETURN GRILLE AT STA 727C+13 WL 212 LBL 68 PER AMM 21-23-03-000-801 AND AMM 21-23-03-400-802;

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO BAY ANGLE CRACKED BS 867 LBL 15 WL 156 ; / [01] UPDATED MEASUREMENTS; [02] LOCATED AND DRILLED ANGLE BS 867 LBL 15 WL 156; OK TO INSTALL PER SRM 51-40-02-0G-0 AND DWG 149A8102; [03] REMOVED CRACKED CLIP BS 867 LBL 15 WL 156 PER SRM 51-40-02-0G-0; [04] AFT CARGO BAY CRACKED ANGLE BS 867 LBL 15 WL 156 FOUND OUT OF LIMITS DUE TO NO LIMITS ESTABLISHED IN SRM; [05] LOCATED AND DRILLED ANGLE BS 867 LBL 15 WL 156; OK TO INSTALL PER SRM 51-40-02-0G-0 AND DWG 149A8102; [06] VERIFIED CORRECTIVE ACTIONS 2-5. OK TO INSTALL.; [07] INSTALLED ACB ANGLE BS 867 LBL 15 WL 156 PER DWG 149A8102 ;DWG 149A8104 AND SRM 51-40-02-0G-0; [08] VERIFIED INSTALLED ACB ANGLE BS 867 LBL 15 WL 156 PER DWG 149A8102 ;DWG 149A8104 AND SRM 51-40-02-0G-0

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

ACB R/H FLOOR TO SIDEWALL SUPPORT BS 887-947 HAS OVERSIZED HOLES AT SPLICE LOCATION BS 887 RBL 25 WL 156 ; / [01] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS887 - BS947; RBL25; WL156 PER SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED ACB FLOOR TO SIDEWALL SUPPORT AT BS887 - BS947; RBL25; WL156 PER SRM 51-40-05-0G-0 AND DWG 147A7500; [03] NEW FLOOR TO SIDEWALL SUPPORT BS 887-847 RBL 25 TO BE INSTALLED ON CUST CARD# TTG8Q006DC17; [04] VERIFIED CORRECTIVE ACTION 2 & 3.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

FWD CARGO BAY BULKHEAD R/H SIDEWALL SUPPORT ANGLE AT 500D LOWER FLANGE I/B FASTENER HOLE ELONGATED ; / [01] ELONGATED HOLE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS; [03] REMOVED FWD CARGO BAY BULKHEAD SUPPORT ANGLE AT BS 500D STR 18R TO 26R PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW FCB BULKHEAD SUPPORT ANGLE P/N: 143A9485Y34 LOT #1464138-1 AT BS 500D STR 18R TO 26R IAW. SRM 51-40-05 DWG 143A7902 ID:0174 REV:- .; [05] RECEIVED PART; [06] VERIFIED CORRECTIVE ACTION ENTRY 5.; [07] OK TO INSTALL BULKHEAD BS 500D STR 18R TO 26R; [08] VERIFIED OK TO INSTALL BULKHEAD BS 500D STR 18R TO 26R; [09] INSTALLED FWD CARGO BAY BULKHEAD R/H SIDEWALL SUPPORT ANGLE AT BS 500D STR 18R TO 26R PER SRM 51-40-02-0G-0; DWG 143A7902 AND DWG 143A9481; [10] VERIFIED INSTALLED FWD CARGO BAY BULKHEAD R/H SIDEWALL SUPPORT ANGLE AT BS 500D STR 18R TO 26R PER SRM 51-40-02-0G-0; DWG 143A7902 AND DWG 143A9481

Part: SUPPORT ANGLE — ELONGATED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

FWD CARGO BAY BULKHEAD L/H SIDEWALL SUPPORT ANGLE AT 500D LOWER FLANGE I/B FASTENER HOLE ELONGATED ; / [01] ELONGATED HOLE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS; [03] REMOVED FWD CARGO BAY BULKHEAD SUPPORT ANGLE AT BS 500D STR 18L TO 26L; [04] REMOVED FWD CARGO BAY BULKHEAD SUPPORT ANGLE AT BS 500D STR 18L TO 26L PER SRM 51-40-02-0G-0; [05] LOCATED AND DRILLED NEW FCB BULKHEAD SUPPORT ANGLE P/N: 143A9485U30 LOT:1463858-1 AT BS 500D STR 18L TO IAW. SRM 51-40-05 AND DWG: 143A7902 ID:0174 REV:-; [06] VERIFIED CORRECTIVE ACTION ENTRY 5.; [07] OK TO INSTALL BULKHEAD BS 500D STR 18L TO 26L; [08] VERIFIED OK TO INSTALL BULKHEAD BS 500D STR 18L TO 26L; [09] INSTALLED FWD CARGO BAY BULKHEAD L/H SIDEWALL SUPPORT ANGLE AT BS 500D STR 18L TO STR 26L PER SRM 51-40-02-0G-0 DWG 143A7902 AND DWG 143A9481; [10] VERIFIED INSTALLED FWD CARGO BAY BULKHEAD L/H SIDEWALL SUPPORT ANGLE AT BS 500D STR 18L TO STR 26L PER SRM 51-40-02-0G-0 DWG 143A7902 AND DWG 143A9481

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 59,949 hrs · 29,584 cycles

FORWARD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. WELDED CRACKED FCB AFT CORNER SCUFF PLATE PER SRM 53-30-15-2R-1 PARA 4. B.(2) AND (4) ACCOMPLISHED FPI INSPECTION TO SCUFF PLATE IAW BOEING SOPM 20-20-02. NO CRACKS NOTED. SANDED REPAIR WELD AREA IAW SRM 53-30-15-2R-1 PARA 4.B.(5) SCUFF PLATE WAS REPAIRED PER SRM 53-30-15-2R-1 PARA 4. B. (2) AND (4). SCUFF PLATE WILL BE INSTALLED ON FAULT TTG8Q003G2EG VERIFIED COMPLETION OF STEP 7.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

SEAT TRACK ATTACH ANGLE FOR SADDLE CRACKED BS 500D-520 LBL 45 WL205 ; / [01] LOCATED AND DRILLED HOLES ON NEW SEAT TRACK ANGLE FOR SADDLE BS 500D-520 LBL 45 WL 205 IAW SRM 51-40-05 AND DWG 143A5410 ID:0013 REV:B.; [02] CORRECTION FOR CORRECT DWG: DWG 143A5034 ID:006 REV:A; [03] VERIFIED STEP 1AND 2; [04] UPDATED MEASUREMENT TABLE; [05] VERIFIED LOCATE AND DRILL OF NEW ANGLE FOR SADDLE; BS 500D-520; LBL 45; WL 205; PER SRM 51-40-05 AND DWG 143A5410; OK TO INSTALL; [06] INSTALLED NEW ANGLE FOR SADDLE AT BS 500-520; LBL 45; WL 205 DWG 143A5034<BR>ID:006 REV:A.; [07] UPDATED PARTS TABLE; [08] VERIFIED STEP 6; [09] VERIFIED INSTALLED NEW ANGLE FOR SADDLE AT BS 500-520; LBL 45; WL 205 DWG 143A5034 ID:006 REV:A. AND SRM 51-40-02-0G-0; [10] ADDED REFERENCE SRM 51-40-02

Part: PANEL — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

PANEL 191AL INNER SURFACE; FWD LOWER CORNER IS CRACKED AT CORE ; / [01] IDENTIFIED PANEL 191AL IAW SRM 53-30-70-0I-1.FIG 2; ITEM [1]. FOUND DAMAGE AT 3' FROM FWD EDGE; 2'FROM LOWER EDGE TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-30-70-1A-1.PARA 4.A.(1). REQUIRES REPAIR PER SRM 51-70-05-2R-1 IAW SRM 53-30-70-2R-1.TABLE 201.<BR>REMOVED APPROX. 3'X3' DAMAGED PLIES IAW SRM 51-70-05-2R-1.PARA 4.A-B.; [02] VALIDATED APPLICABILITY OF SRM 51-70-05-2R-1 IAW SRM 53-30-70-2R-1.; [03] INSPECTED AND VERIFIED CORRECTIVE ACTION ITEMS 1 AND 2. OKAY TO PROCEED PER SRM 51-70-05-2R-1.; [04] APPLIED VACUUM BAG FOR MOISTURE REMOVAL; CHECKED FOR LEAKS. LEAK CHECK GOOD. SET TO CURE USING HEATCON ID:ATS532 S/N:15092117 IAW SRM 51-70-05-2R-1.PARA 4.B.; [05] COMPLETED MOISTURE REMOVAL; NO CONTAMINATION NOTED; REMOVED VACUUM BAG; FABRICATED REPAIR PLIES OUT OF BMS 8-79 ST 120 LOT#1458373-1; BMS 8-79 ST 1581 LOT#1466502-1; AND BMS 5-129 GR5 LOT#1464324-2; INSTALLED; VACUUM BAGGED; CHECKED FOR LEAKS AND SET TO CURE USING HEATCON HOTBONDER ID:ATS532 S/N:15092117 IAW SRM 51-70-05-2R-1 PAR 4B-E.; [06] CURED; UNBAGGED; LIGHTLY SANDED; AND CLEANED REPAIR PLIES IAW SRM 51-70-05-2R-1 PAR 4E-G.; [07] VERIFIED CORRECTIVE ACTIONS 4-6; [08] UT INSPECTED POST CURE IAW 737 NDTM PART 4 51-00-02; NO DISBONDS NOTED. EQUIP ID#: ATS2341 S/N: 190848104; [09] REFINISHED REPAIR AREA IAW SRM 51-70-05-2R-1 PAR 4G AND AMM 51-21-99-300-802 PAR 3C(1).<BR><BR>COMPLETED SRM REPAIR 51-70-05-2R-1.; [10] VERIFIED CORRECTIVE ACTION 9

Part: STRINGER — CRACKED · airframe 59,949 hrs · 29,584 cycles

CRACK ON END OF STRINGER 26 LEFT B.S. 520+17. ; / REMOVED DAMAGED AREA S-26L BS 500D+10'-540 IAW SRM 53-00-03-2R-1 REP.1; [02] REQUIRED NDI INSPECTION S-26L BS 500D+10' CUT OUT CRACK FREE IAW SRM 53-00-03-2R-1 REP.1 RECEIVED STR REPAIR SECTION FROM OSS FABRICATED FROM 7075-0 .045 LOT #1464744-1 HEAT TREATED TO T6 CONDITION ON SWA PO# 835676 REPAIR HAT SECTION RECEIVED FROM OSS FABRICATED FROM 7075-0 .050 LOT #1457313-101 HEAT TREATED TO T6 CONDITION ON SWA PO#835675 ALL DATED 03 SEP 21;TRIMMED LOCATED AND DRILLED NEW STR AND HAT SECTION FOR STR REPAIR AT STR 26L BS 500D+10 TO 540 APPLIED CHEMICAL CONVERSION COAT TO PARTS AND REPAIR AREA ALL IAW SRM 53-00-03-2R-1 STEPS 4 E F G H AND I FIG 205 OK TO PRIME INSTALLED STR REPAIR AT STR 26 L/H BS 500D+10 TO 540 APPLIED FAY SEAL AND CIC ALL IAW SRM 53-00-03-2R-1 STEPS 4 K AND L AND BOEING DWG 143A3230

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON INTERCOSTAL AT B.S. 500D+1; L.B.L. 7; W.L. 151. ; / [01] CORROSION ON INTERCOSTAL WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-04-1A-1 FIGURE 102 DETAIL E.; [02] VERIFIED DAMAGE OUT LIMITS PER SRM 53-00-04-1A-1; [03] LOCATED AND DRILLED NEW INTERCOSTAL P/N 143A9803-15 IAW SRM 51-40-05-0G-0 AND DWG 143A7902. OK TO INSTALL.; [04] VERIFIED LOCATED AND DRILLED NEW INTERCOSTAL P/N 143A9803-15 IAW SRM 51-40-05-0G-0 AND DWG 143A7902. OK TO INSTALL.; [05] INSTALLED NEW INTERCOSTAL P/N 143A9803-15 IAW SRM 51-40-05-0G-0 AND DWG 143A7902.; [06] AND SRM 51-40-02-0G-0; [07] VERIFIED INTERCOSTAL INSTALLED PER SRM 51-40-05-0G-0 AND DWG 143A7902 AND SRM 51-40-02-0G-0; [08] UPDATED MEASUREMENTS; [09] TASK COMPLETE

Part: NONE — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CRACKED UPPER ANGLE ON SUPPORT WEB BS 927-947 BL 0 WL 208 ; / [01] REMOVED UPPER ANGLE FROM WEB SUPPORT BS 927-947 BL 0 WL 208 PER SRM 51-40-02; [02] LOCATED AND DRILLED NEW UPPER ANGLE ON SUPPORT WEB BS 927-947 BL 0 WL 208 PER SRM 51-40-05-0G-0 AND DWG 147A5430. OK TO INSTALL.; [03] VERIFIED LOCATION AND DRILL UP PER SRM 51-40-05 AND DWG 147A5430; [04] INSTALLED NEW UPPER ANGLE ON SUPPORT WEB BS 927-947 BL 0 WL 208 PER SRM 51-40-02-0G-0 AND DWG 147A5400.; [05] CORRECTION- VERIFIED LOCATION AND DRILL UP PER SRM 51-40-05 AND DWG 147A5430. OK TO INSTALL; [06] VERIFIED INSTALLATION UPPER ANGLE ON SUPPORT WEB BS 927-947 BL 0 WL 208 PER SRM 51-40-02 AND DWG 147A5400; [07] TASK COMPLETE

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CRACKED FLOOR SUPPORT BS 277-294 BL 0 WL 208 ; / [01] REMOVED CRACKED SUPPORT AT BS 277-294 BL0 WL 208; LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-02 SRM 51-40-05. REQUEST OKAY TO INSTALL; [02] VERIFIED REMOVED CRACKED SUPPORT AT BS 277-294 BL0 WL 208; LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-02 SRM 51-40-05. REQUEST OKAY TO INSTALL; [03] INSTALLED NEW INTERCOSTAL PER SRM 51-40-02 AND DWG 141A5400; [04] VERIFIED INSTALLATION OF NEW INTERCOSTAL PER SRM 51-40-02 AND DWG 141A5400; [05] VERIFIED INSTALLATION OF NEW INTERCOSTAL PER SRM 51-40-02 AND DWG 141A5400

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CRACKED FLOOR SUPPORT BS 344-360 BL 0 WL 208 ; / [01] ET INSPECTED SUSPECTED CRACK IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; VERIFIED CRACK EXISTS.<BR>CAL ID IS000450 N500D; [02] REMOVED INTERCOSTAL AT BS344-360 BL0 WL 208; PER SRM 51-40-02. LOCATED AND DRILLED NEW INTERCOSTAL PER SRM 51-40-05 AND DWG141A5400. REQUEST OK TO INSTALL.; [03] VERIFIED LOCATION AND DRILL UP PER SRM 51-40-05 AND DWG 141A5400. FLOORBOARD HOLES STILL REQUIRED; [04] INSTALL NEW INTERCOSTAL BS 344-360 BL 0 WL208 IAW SRM 51-40-02 AND DWG 141A5400; [05] VERIFIED INSTALLATION AND DRILLING OF FLOORBOARD HOLES IN INTERCOSTAL PER SRM 51-40-02 AND DWG 141A5400.

Part: NONE — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON BS 986 FLOOR BEAM UPPER CHORD RBL 44 WL 208 ; / [01] REMOVED CORROSION ON BS986 FLOOR BEAM UPPER CHORD RBL44 WL208 IN AREA OF 0.9' BY 1.1' BY A DEPTH OF 0.065' PER SRM 51-10-02-0G-0 AND SRM 53-70-51-1A-1. OUT OF LIMITS PER SRM 53-70-51-1A-1.; [02] VERIFIED REMOVED CORROSION ON BS986 FLOOR BEAM UPPER CHORD RBL44 WL208 IN AREA OF 0.9' BY 1.1' BY A DEPTH OF 0.065' PER SRM 51-10-02-0G-0 AND SRM 53-70-51-1A-1. OUT OF LIMITS PER SRM 53-70-51-1A-1.; [03] REMOVED ANGLE UNDER MOPSILL BS 986-1001 RBL 44 WL 207 FOR ACCESS PER SRM 51-40-02-0G-0.; [04] REMOVED ANGLE UNDER MOPSILL BS 967-986 RBL 48 WL 207 FOR ACCESS PER SRM 51-40-02-0G-0.; ALL I.A.W 53-70-51-2R-4 STEP 4.G-4.M.OK TO INSTALL.; [13] FABRICATED REPAIR PARTS ITEMS(1)T-CHORD1EA;(2)ANGLE 2EA;(3)ANGLE 2EA;(4)STRAP 2EA;PARTS OBTAINED FROM SOUTHWEST KIT BS986 SI#7530799;APPLIED CHEMICAL CONVERSION COATING AND PRIMED REPAIR PARTS AND BARE SURFACE OF THE REWORKED AREAS ALL I.A.W SRM 53-70-51-2R-4 STEP 4.G-4.M.OK TO INSTALL; [INSTALLED INTERCOSTAL, ITEM(8)2EA CORNER FITTINGS, ITEM (6) FILLERS 2EA BS986-1006 RBL38 WL208-WL200 I.A.W SRM 53-70-51-2R-4 STEP 4.N,O AND BOEING DWG 147A5730

Part: NONE — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON BS 986 FLOOR BEAM UPPER CHORD LBL 44 WL 208 ; / [01] WORK COMPLETED ON CARD NO. M-21-153-00612 (2529).; [02] VERIFIED WORK COMPLETED ON CARD NO. M-21-153-00612 (2529).

Part: SHIELD — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON AFT CARGO BAY DOOR CUT-OUT FWD SHIELD FROM STA 767 TOO STA 787+7; RBL22; WL 154 ; / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [03] REMOVED ACB FWD SHIELD AT BS767 - BS787; RBL22; WL154 PER SRM 51-40-02-0G-0; [04] LOCATED/DRILLED ACB FWD SHIELD AT BS767 - BS787; RBL22; WL154 PER SRM 51-40-05-0G-0 AND DWG 146A0081; [05] VERIFIED CORRECTIVE ACTION ENTRY 4.; [06] OK TO INSTALL; [07] OK TO INSTALL; [08] INSTALLED PER SRM 51-40-02-0G-0 AND DWG 146A0081; [09] UPDATED PART USE; [10] INSTALLED AFT CARGO BAY FWD SHIELD BS 767 TO 792 RBL 22 WL 154 PER SRM 51-40-02-0G-0 AND DWG 146A0081; [11] VERIFIED INSTALLATION OF ACB FWD SHIELD; BS 767-792; RBL 22; WL 154; PER SRM 51-40-02 AND DWG 146A0081; [12] VERIFIED ALL WORK COMPLETE THIS TASK

Part: SIDEWALL SUPPORT — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM STA 727 TO STA 847; LBL 22; WL 154 ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [03] VERIFIED CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [04] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS847; LBL22; WL154 PER SRM 51-40-02-0G-0; [05] FABRICATED; LOCATED AND APPLIED CHEMICAL CONVERSION COATING TO ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS847 AND SPLICE REPAIR AT BS727E+8 - BS 727E+18 USING BAC1496-377#7075T62 LOT#1467164-1 PER SRM 51-40-05-0G AND DWG 146A7500; SRM 53-00-53-2R-5; AMM 51-21-41-370-80; [11] VERIFIED APPLIED PRIMER TO FLOOR TO SIDEWALL SUPPORT PER AMM 51-21-72-370-804.; PER SRM 51-40-02 AND DWG 146A7502; [18] ALL WORK COMPLETE; [19] VERIFIED ALL WORK COMPLETE; [20] THE CORRECT SELECT REF IS 53-00-53-2R-5-A00957. NO FOLLOW ON REQUIREMENTS REQUIRED.; [21] CERTIFY STEP 20

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM STA 727 TO STA 767; RBL 22; WL 154. ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLE PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [03] UPDATED STATEMENT OF CORRECTIVE ACTION BLOCK 1. CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [04] UPDATED STATEMENT OF CORRECTIVE ACTION BLOCKS 2 AND 3. CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [05] VERIFIED CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [06] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS767; RBL22; WL154 PER SRM 51-40-02-0G-0; [07] LOCATED AND DRILLED ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS767; RBL22; WL154 PER SRM 51-40-05-0G-0 AND DWG 146A7500; [08] VERIFIED CORRECTIVE ACTION 7.; [09] OK TO INSTALL RH FLOOR-TO-SIDEWALL SUPPORT; [10] INSTALLED FLOOR TO SIDEWALL SUPPORT BS 727 TO 767; RBL22; WL154 IAW SRM 51-40-02 AND DWG 146A0061; DWG 146A7502 AND DWG 146A7502; [11] VERIFIED INSTALLATION OF RH FLOOR-TO-SIDEWALL SUPPORT; BS 727-767; RBL 22; WL 154; PER SRM 51-40-02 AND DWG 146A0061 AND DWG 146A7502; [12] VERIFIED ALL WORK COMPLETE THIS TASK

Part: WEB — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

WHILE ACCOMPLISHING HFEC INSPECTION, FOUND A 1 INCH CRACK AT BS 673 RBL 40 WL 203, COMMON TO THE HORIZONTAL PRESSURE DECK WEB. REMOVED ADDITIONAL 0.040IN FROM EDGE OF THE WEB CUTOUT IAW SRM 53-40-51-2R-2 PAR 4.D(4). VERIFIED .040' INSURANCE CUT AND PERFORMED DVI INSPECTION IAW SRM 53-40-51-2R-2, NO DEFECTS OR DAMAGE NOTED FABRICATED A DOUBLER AND STIFFENERS AND WEB. LOCATED AND DRILLED ALL REPAIR PARTS IAW SRM 53-40-51-2R-2. INSTALLED ALL FASTENERS TO REPAIR IAW SRM 53-40-51-2R-2.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT STA 867+15; RBL 22; WL 157 ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D.; [02] VERIFIED CORROSION OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] UPDATED MEASUREMENT; [04] VERIFIED UPDATED MEASUREMENTS; [05] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS867 - BS887; RBL22; WL157 PER SRM 51-40-02-0G-0; [06] LOCATED AND DRILLED ACB FLOOR TO SIDEWALL SUPPORT AT BS867 - BS887; RBL22; WL157 PER SRM 51-40-05-0G-0 AND DWG 146A7500; [07] VERIFIED CORRECTIVE ACTION 6.; [08] OK TO INSTALL.; [09] OK TO INSTALL; [10] INSTALLED FLOOR TO SIDEWALL SUPPORT AT BS 887- 867 RBL 22 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 147A7500; 146A7502;147A0060.; [11] VERIFIED INSTALLED FLOOR TO SIDEWALL SUPPORT AT BS 887- 867 RBL 22 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 147A7500; 146A7502;147A0060.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 59,949 hrs · 29,584 cycles

#1 ENGINE O/B T/R AFT FIRE SEAL LABRYNTH BRACKET ON PYLON IS CRACKED ; #1 ENGINE O TR AFT FIRE SEAL LARYNTH RACKET ON PYLON IS CRACKED / [01] REMOVED AND REPLACED #1 ENG O/B T/R AFT FIRE SEAL LABRYNTH BRACKET ON PYLON PER SRM 51-40-02-0G-0 STEP 4. AND PER IPC 54-54-00-03; [02] CERTIFIED ACTION 1; [03] VERIFIED INSTALLATION OF #1 ENG O/B T/R AFT FIRE SEAL LABYRINTH BRACKET ON PYLON PER SRM 51-40-02-0G-0 STEP 4. AND PER IPC 54-54-00-03; [04] CORRECTED MESURMENTS; [05] TASK COMPLETE

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

AFT CARGO SIDEWALL SUPPORT BRACKET STA 727; LBL-26; WL-157; HAS SURFACE CORROSION ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO NO DAMAGE IS ALLOWED AT THIS LOCATION PER SRM 53-40-08-1A-3 FIGURE 102.; [02] VERIFIED CORROSION OUT OF LIMITS PER SRM 53-40-08-1A-3; [03] REMOVED SIDEWALL SUPPORT BRACKET BS 727 LBL 26 WL 156 IAW SRM 51-40-02-0G-0; [04] LOCATED; DRILLED; DEBURRED NEW AFT CARGO SIDEWALL SUPPORT BRACKET BS 727 LBL26 WL 157 IAW SRM 51-40-05. OK TO INSTALL; [05] VERIFIED LOCATE; DRILL AND DEBURR OF NEW ACB SIDEWALL SUPPORT BRACKET; BS 727; LBL 26 WL 157; PER SRM 51-40-05; OK TO INSTALL; [06] INSTALLED NEW AFT CARGO SIDEWALL SUPPORT BRACKET BS 727 LBL26 WL 157 IAW SRM 51-40-02 AND DWG 144A2600; [07] VERIFIED INSTALLATION OF NEW AFT CARGO SIDEWALL SUPPORT BRACKET BS 727 LBL26 WL 157 IAW SRM 51-40-02 AND DWG 144A2600.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

AFT CARGO SIDEWALL SUPPORT BRACKET STA 727; RBL-22; WL-156; HAS SURFACE CORROSION. ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO NO DAMAGE IS ALLOWED AT THIS LOCATION PER SRM 53-40-08-1A-3 FIGURE 102.; [02] VERIFIED CORROSION OUT OF LIMITS PER SRM 53-40-08-1A-3; [03] REMOVED SIDEWALL SUPPORT BRACKET BS 727 RBL 22 WL 156 IAW SRM 51-40-02-0G-0; [04] LOCATED; DRILLED; DEBURRED NEW AFT CARGO SIDEWALL SUPPORT BRACKET BS 727 RBL22 WL 156 IAW SRM 51-40-05. OK TO INSTALL; [05] VERIFIED LOCATE; DRILL AND DEBURR OF NEW ACB SIDEWALL SUPPORT BRACKET; BS 727; RBL 22 WL 156; PER SRM 51-40-05; OK TO INSTALL; [06] INSTALLED NEW AFT CARGO SIDEWALL SUPPORT BRACKET BS 727 RBL22 WL 156 IAW SRM 51-40-02 AND DWG 144A2600; [07] VERIFIED INSTALLATION OF NEW AFT CARGO SIDEWALL SUPPORT BRACKET BS 727 RBL22 WL 156 IAW SRM 51-40-02 AND DWG 144A2600.

Part: NONE — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION NEAR FASTENER HOLE ON BULKHEAD FLANGE UPPER SURFACE AT BS 260 RBL 9.5 WL 208. ; / [01] REMOVED CORROSION NEAR FASTENER HOLE BS260 RBL9.5 WL208 1'X1' AREA I.A.W SRM 51-10-02-0G-0; [02] REMOVED NUTPLATE BS260 RBL10 WL208 I.A.W SRM 51-40-02-0G-0; [03] VERIFIED CORROSION REMOVED PER SRM 51-10-02.; [04] REQUEST UT INSPECTION;HFEC OPEN HOLE INSPECTION AND HFEC SURFACE INSPECTION.; [05] UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.089'<BR>ET INSPECTED BLEND AND HOLE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23 AND PROCEDURE 16; NO CRACKS NOTED.<BR>CAL ID IS000450 N500D<BR>CAL ID ATS2031 E650; [06] REQUEST G.V.I OF THE DAMAGED AREA; ADJACENT AND UNDERLYING STRUCTURES TO VERIFY NO ADDITIONAL DAMAGE; [07] ACCOMPLISHED GVI; NO ADDITIONAL DAMAGE AT REPAIR AREA; ADJACENT AND UNDERLYING STRUCTURE; OK TO PROCEED. PER SRM 51-10-02.; [08] EDIT TO CORRECTIVE ACTION #5:<BR>ERRANTLY WROTE 0.089' AS REMAINING THICKNESS.<BR><BR>REMAINING THICKNESS IS ACTUALLY 0.087'; [09] VERIFIED COMPLETION OF EA 21-153-02555; [10] VERIFIED ALL STEPS ARE COMPLETE.; [11] VERIFIED ALL RII STEPS ARE COMPLETE.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

AFT CARGO SIDEWALL SUPPORT BRACKET CRACKED, BS 947, RBL 40, WL 200. REMOVED THE SUPPORT BRACKET IAW SRM 51-40-02-0G-0. FABRICATED, LOCATED, DRILLED, & CHEMICAL CONVERSION COAT, PRIMER AND NUTPLATE INSTALLATION IAW SRM 51-40-05-0G-0;51-40-02-0G-0 AND DWGS 149A9490, 149A9491. INSTALLED THE NEW SUPPORT BRACKET IAW SRM 51-40-02, DWGS 149A9490, 149A9491, 147A9109, 147A0060 AND AIPC 53-11-51-01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 RBL25 WL155. ; / [01] FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS DUE TO NO SRM LIMITS; [03] LOCATED AND DRILLED NEW ANGLE P/N 143A7502U154 LOT 1448645-4 IAW DWG 143A7505 ID:0002 REV:B REQUEST OK TO INSTALL.; [04] VERIFIED LOCATED AND DRILLED NEW ANGLE P/N 143A7502U154 LOT 1448645-4 IAW DWG 143A7505 ID:0002 REV:B.<BR>VERIFIED OK TO INSTALL.; [05] INSTALLED NEW ANGLE P/N 143A7502U154 LOT 1448645-4 IAW SRM 51-40-02 DWG 143A7505 ID:0002 REV:B; [06] VERIFIED INSTALLED NEW ANGLE P/N 143A7502U154 LOT 1448645-4 IAW SRM 51-40-02 DWG 143A7505.; [07] VERIFIED ALL STEPS COMPLETE.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 59,949 hrs · 29,584 cycles

FLOOR PANEL 221GF FWD OUTBD CORNER CRACKED. REPLACED FLOOR PANEL 221GF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-68 ITEM 370.

Part: NONE — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON TRACK TIEDOWN AT FWD CARGO BAY BS500B RBL13 WL156. ; / [01] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [02] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [03] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687ZQ; CARD COMPLETE.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500B FWD SIDE LBL25 WL155. ; / [01] FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS DUE TO NO SRM LIMITS; [03] LOCATED AND DRILLED NEW ANGLE P/N: 143A7502U159 LOT: 1461470 . IAW SRM 51-40-05 AND DWG:143A7505 ID: 0005 REV:B REQUEST OK TO INSTALL; [04] UPDATED PART RECEIVING.; [05] VERIFIED CORRECTIVE ACTION 3. OK TO INSTALL.; [06] VERIFIED OK TO INSTALL.; [07] INSTALLED NEW ANGLE P/N: 143A7502U159 LOT: 1461470 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0005 REV:B; [08] VERIFIED INSTALLED NEW ANGLE P/N: 143A7502U159 LOT: 1461470 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0005 REV:B; [09] VERIFIED ALL STEPS COMPLETE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C AFT SIDE LBL25 WL155. ; / [01] FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS DUE TO NO SRM LIMITS; [03] LOCATED AND DRILLED NEW ANGLE P/N: 143A7502U155 LOT: 1458822-5 . IAW SRM 51-40-05 AND DWG:143A7505 ID: 0009 REV:A REQUEST OK TO INSTALL; [04] VERIFIED LOCATED AND DRILLED NEW ANGLE P/N: 143A7502U155 LOT: 1458822-5 . IAW SRM 51-40-05 AND DWG:143A7505 ID: 0009 REV:A.<BR>VERIFIED OK TO INSTALL;.; [05] INSTALLED NEW ANGLE P/N: 143A7502U155 LOT: 1458822-5 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0009 REV:A; [06] VERIFIED INSTALLED NEW ANGLE P/N: 143A7502U155 LOT: 1458822-5 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0009 REV:A.; [07] VERIFIED ALL STEPS COMPLETE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25 WL155. ; / [01] FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS DUE TO NO SRM LIMITS; [03] LOCATED AND DRILLED NEW ANGLE P/N: 143A7502U159 LOT: 1461470 . IAW SRM 51-40-05 AND DWG:143A7505 ID: 0005 REV:B REQUEST OK TO INSTALL; [04] UPDATED PART RECEIVING.; [05] VERIFIED LOCATED AND DRILLED NEW ANGLE P/N: 143A7502U159 LOT: 1461470 . IAW SRM 51-40-05 AND DWG:143A7505 ID: 0005 REV:B. <BR>VERIFIED OK TO INSTALL.; [06] INSTALLED NEW ANGLE P/N: 143A7502U159 LOT: 1461470 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0005 REV:B; [07] VERIFIED INSTALLED NEW ANGLE P/N: 143A7502U159 LOT: 1461470 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0005 REV:B.; [08] VERIFIED ALL STEPS COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS499 LBL24 WL156. ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D. NEW FLOOR TO SIDEWALL SUPPORT FROM BS 396 TO BS 500D LBL 24 WL 156 WILL BE INSTALLED ON FAULT TTG8Q00687YP.; [02] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687YP; JOB COMPLETE.

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 TO BS420 LBL23 WL156. ; / CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL REMOVED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 400 TO BS 420 LBL 23 WL 156 PER SRM 51-40-02-0G-0 FABRICATED NEW FLOOR TO SIDEWALL SUPPORT BS 396 TO 500D L/H; AND SPLICE REPAIR BS 480 TO 500 L/H FROM EXTRUSION CLAD BAC1496-444#7075T62 LOT# 1466509-1 PER SRM 53-00-53-2R-5; SRM51-40-05-0G-0; AND DWG 143A7501LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AND SPLICE REPAIR PER PER SRM 53-00-53-2R-5; SRM51-40-05-0G-0; AND DWG 143A7501] INSTALLED SPLICE REPAIR PER SRM 53-00-53--2R-5 AND DWG 143A7501] INSTALLED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BS 396 TO500D LBL 23 WL 156 PER SRM 51-40-02-0G-0; AND DWG 143A7500

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS411 RBL24 WL156. ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMIT DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D.; [02] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2.; [03] UPDATED MEASUREMENTS; [04] REMOVED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 396 TO 420 PER SRM 51-40-02-0G-0; [05] FABRICATED FCB FLOOR TO SIDEWALL SUPPORT BS 400-420; RBL 24 WL 156 IAW SRM 50-40-05 DWG# 143A7501. APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01. REQUEST OK TO APPLY PRIMER.; [06] VERIFIED FABRICATED FCB FLOOR TO SIDEWALL SUPPORT BS 400-420; RBL 24 WL 156 IAW SRM 50-40-05 AND DWG# 143A7501.<BR>VERIFIED APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01.<BR>VERIFIED OK TO PRIME.; [07] APPLIED PRIMER IAW SOPM 20-41-02; [08] VERIFIED CORRECTIVE ACTION ENTRY 7.; [09] OK TO INSTALL FCB RH FLOOR TO SIDEWALL SUPPORT BS 396 - 420; [10] OK TO INSTALL FCB RH FLOOR TO SIDEWALL SUPPORT BS 396-420 GIVEN.; [11] INSTALLED FCB RH FLOOR TO SIDEWALL SUPPORT ; BS 396-420; RBL24; IAW SRM 51-40-02-0G-0; DWG143A7500.; [12] VERIFIED INSTALLED FCB RH FLOOR TO SIDEWALL SUPPORT ; BS 396-420; RBL24; IAW SRM 51-40-02-0G-0; DWG143A7500.

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT AT FWD CARGO BAY BS500D LBL23 TO RBL23 WL156. ; / [01] CORROSION ON SUPPORT FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SPM.; [02] VERIFIED NO LIMITS; REPAIR BY REPLACEMENT OF PART.; [03] CORROSION ON SUPPORT FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [04] UPDATED MEASUREMENTS; [05] REMOVED AFT BULKHEAD TO FLOOR SUPPORT AT FWD CARGO BAY BS 500D LBL 23 TO RBL 23 WL 153 PER SRM 51-40-02-0G-0; [06] LOCATED/DRILL AFT BULKHEAD TO FLOOR SUPPORT AT FCB BS500D; LBL23 - RBL23; WL 156 PER SRM 51-40-05-0G-0 AND DWG 143A9481; DWG 143A7902; [07] VERIFIED CORRECTIVE ACTION ENTRY 6.; [08] OK TO INSTALL LOWER BULKHEAD BS 500D; [09] VERIFIED OK TO INSTALL REPLACEMENT SUPPORT BS 500D LBL 23 TO RBL 23 WL 156; [10] INSTALLED FWD CARGO BAY LOWER BULKHEAD SUPPORT ANGLE BS 500D LBL 23 TO RBL 23 WL 156 PER SRM 51-40-02-0G-0; DWG 143A9481; AND DWG 143A7902; [11] VERIFIED INSTALLED FWD CARGO BAY LOWER BULKHEAD SUPPORT ANGLE BS 500D LBL 23 TO RBL 23 WL 156 PER SRM 51-40-02-0G-0; DWG 143A9481; AND DWG 143A7902

Part: NONE — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON TRACK TIEDOWN AT FWD CARGO BAY BS400 RBL13 WL156. ; / [01] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [02] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [03] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687ZQ; CARD COMPLETE.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON FWD SHIELD AT FWD CARGO BAY BS420 - BS440 RBL23 WL156. ; / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED NO LIMITS; REPAIR BY REPLACEMENT OF PART.; [03] REMOVED FWD SHIELD AT FWD CARGO BAY BS 420 TO BS 440 RBL23 WL156 PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED FCB FWD SHIELD BS 420-440; RBL 23 IAW SRM 51-40-05; DWG# 143A0080.; [05] VERIFIED CORRECTIVE ACTION ITEMS 3 AND 4; [06] OK TO INSTALL FCB RH FWD SHIELD; BS 420-440. RBL23.; [07] VERIFIED OK TO INSTALL; [08] INSTALLED FCB RH FWD SHIELD;BS 420-440; RBL23 IAW SRM 51-40-02-0G-0; DWG 143A0080; [09] VERIFIED INSTALLED FCB RH FWD SHIELD;BS 420-440; RBL23 IAW SRM 51-40-02-0G-0; DWG 143A0080

Part: NONE — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON TRACK TIEDOWN AT FWD CARGO BAY BS436 RBL13 WL156. ; / [01] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [02] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [03] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687ZQ; CARD COMPLETE.

Part: TRACK — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CRACKED TRACK AT FWD CARGO BAY BS460 RBL13 WL155. ; / [01] CRACK ON TRACK IS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [02] VERIFIED CRACK ON TRACK IS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] REMOVED FCB TRACK BS 396-500D; RBL 13 IAW SRM 51-40-02. <BR>LOCATED AND DRILLED NEW TRACK PER SRM 51-40-05; DWG# 143A7500 ID 05.; [04] VERIFIED CORRECTIVE ACTION ITEM 3; [05] REQUEST OK TO INSTALL.; [06] VERIFIED OK TO INSTALL FCB TRACK BS396-500D RBL13.; [07] INSTALLED FCB TRACK BS 396-500D; RBL 13; WL 155 IAW SRM 51-40-02; DWG# 143A7500 ID 05.; [08] VERIFIED INSTALLED FCB TRACK BS 396-500D; RBL 13; WL 155 IAW SRM 51-40-02; DWG# 143A7500 ID 05.; [09] VERIFIED ALL STEPS COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL156. ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D.; [02] VERIFIED DAMAGE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [03] REMOVED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY 500A TO BS 500D RBL 23 WL 156 PER SRM 51-40-02-0G-0; [04] RECEIVED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY N/P: 143A7501U186 LOT:1465888-1 PO NUMBER:833400. LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A7500 ID: 0017 REV:A; [05] RECEIVED PART; [06] VERIFIED LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A7500 ID: 0017 REV:A.; [07] OK TO INSTALL FLOOR TO SIDEWALL SUPPORT; [08] OK TO INSTALL FLOOR TO SIDEWALL SUPPORT GIVEN.; [09] INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A7500 ID: 0017 REV:A.; [10] VERIFIED INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A7500 ID: 0017 REV:A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL25 WL155. ; / [01] FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS DUE TO NO SRM LIMITS; [03] LOCATED AND DRILLED NEW ANGLE P/N: 143A7502U155 LOT: 1458822-5 . IAW SRM 51-40-05 AND DWG:143A7505 ID: 0002 REV:B REQUEST OK TO INSTALL; [04] VERIFIED CORRECTIVE ACTION 3. OK TO INSTALL INTERCOSTAL ATTACH ANGLE (CLIP) IN FCB BS 400 LBL 25 WL 155.; [05] INSTALLED NEW ANGLE P/N: 143A7502U155 LOT:1458822-5 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0002 REV:B.; [06] VERIFIED INSTALLED NEW ANGLE P/N: 143A7502U155 LOT:1458822-5 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0002 REV:B.; [07] VERIFIED ALL STEPS COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500C TO BS500C+6 LBL23 WL156. ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D. NEW FLOOR TO SIDEWALL SUPPORT FROM BS 396 TO BS 500D LBL 24 WL 156 WILL BE INSTALLED ON FAULT TTG8Q00687YP.; [02] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687YP; JOB COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A+10 TO BS500A+15 LBL23 WL156. ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D. NEW FLOOR TO SIDEWALL SUPPORT FROM BS 396 TO BS 500D LBL 24 WL 156 WILL BE INSTALLED ON FAULT TTG8Q00687YP.; [02] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687YP; JOB COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS496 LBL24 WL156. ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D. NEW FLOOR TO SIDEWALL SUPPORT FROM BS 396 TO BS 500D LBL 24 WL 156 ON FAULT TTG8Q00687YP.; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D. NEW FLOOR TO SIDEWALL SUPPORT FROM BS 396 TO BS 500D LBL 24 WL 156 WILL BE INSTALLED ON FAULT TTG8Q00687YP.; [03] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687YP; JOB COMPLETE.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C AFT SIDE RBL25 WL155. ; / [01] CRACK FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED OUT OF LIMITS DUE TO NO SRM LIMITS; [03] LOCATED AND DRILLED NEW ANGLE P/N: 143A7502U154 LOT: 1456906-4 . IAW SRM 51-40-05 AND DWG:143A7505 ID: 0010 REV:A REQUEST OK TO INSTALL; [04] VERIFIED CORRECTIVE ACTION 3. OK TO INSTALL.; [05] INSTALLED NEW ANGLE P/N: 143A7502U154 LOT: 1456906-4 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0010 REV:A; [06] VERIFIED INSTALLED NEW ANGLE P/N: 143A7502U154 LOT: 1456906-4 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0010 REV:A; [07] VERIFIED ALL STEPS COMPLETE.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL156. ; / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED NO LIMITS IN THE SRM.; [03] REMOVED AFT SHIELD AT FWD CARGO BAY BS 500 TO 500A RBL 23 WL 156 PER SRM 51-40-02-0G-0; [04] RECEIVED NEW AFT SHIELD AT FWD CARGO BAY N/P: 143A8126U31ATSMRO LOT:1467243-1 PO NUMBER: 835328. LOCATED; DRILLED AND COUNTERSANK NEW AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A0080 ID:0019 REV:-; [05] RECEIVED PART; [06] VERIFIED LOCATED; DRILLED AND COUNTERSANK NEW AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A0080 ID:0019 REV:- .; [07] OK TO INSTALL.; [08] VERIFIED OK TO INSTALL; [09] INSTALLED NEW AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A0080; [10] VERIFIED INSTALLED NEW AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A0080.; [11] VERIFIED ALL STEPS COMPLETE.

Part: TIE DOWN — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON TRACK TIEDOWN AT FWD CARGO BAY BS420 RBL13 WL156. ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [03] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [04] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687ZQ; CARD COMPLETE.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500 RBL24 WL156. ; / [01] CORROSION ON SUPPORT/SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. NEW SHIELD WILL BE INSTALLED ON FAULT TTG8Q00686P2.; [02] VERIFIED NO LIMITS; REPLACEMENT ON TTG8Q00686P2; CARD COMPLETE.

Part: NONE — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON TRACK TIEDOWN AT FWD CARGO BAY BS500C+16 RBL13 WL156. ; / [01] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [02] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [03] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687ZQ; CARD COMPLETE.

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 59,949 hrs · 29,584 cycles

FWD SERVICE DOOR LOWER BEAM CRACKED AT I/B SIDE OF RADIUS ; / [01] WORK COMPLETED ON RO NO P0972344-1.; [02] VERIFIED WORK ACCOMPLISHED ON RO# P0972344-1

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,949 hrs · 29,584 cycles

CORROSION ON FUSELAGE EXTERIOR SKIN AT STA 1084 THROUGH STA 1090 AND LBL 12 THROUGH RBL6 ; / [01] UPDATED TABLE 1-13 ; 15 AND 16; [02] STRIPPED EXTERIOR FINISH PER AMM 51-21-11-150-801; [03] REMOVED 21 FASTENERS PER SRM 51-40-02-0G-0; [04] BLENDED CORROSION 19'X4' PER SRM 53-00-01-1A-1; [05] VERIFIED REMOVAL OF FASTENERS PER SRM 51-40-02 AND BLENDING OF CORROSION PER SRM 53-00-01-1A-1; [06] UT INSPECTED SKIN BLENDOUT AREA IAW B737 NDTM P4; 51-00-00 PROC 2. REMAINING MAT. 0.077 TOOL ID ATS2341; E650; [07] HFEC INSPECTED SKIN BLENDOUT AREA; IAW B737 NDTM P6; 51-00-00 PROC 23. NO CRACKS NOTED. TOOL ID ATS1465; N600; [08] ACCOMPLISHED HFEC HOLE INSPECTION TO OPEN FASTENERS REMOVED IN BLENDOUT AREA IAW B737 NDTM P6; 51-00-00 PROC 16. NO CRACKS NOTED. TOOL ID ATS1465; N600; TOOL ID ATS1411; MINIMITE; [09] ACCOMPLISHED HFEC COUNTERSINK INSP TO COUNTERSINKS IN BLENDOUT AREA IAW B737 NDTM P6; 53-30-00 PROC 3. NO CRACKS NOTED. TOOL ID ATS1465; N600; TOOL ID ATS1411; MINIMITE; [10] BLEND MEASURES 19'X4'X.003' ORIGINAL THICKNESS .080'; .077' FOUND OUT OF LIMITS DUE TO BLEND EXCEEDING 3 IN 10 FASTENERS PER SRM 53-00-01-1A-1 FIG D; [11] VERIFIED OUT OF LIMITS PER SRM 53-00-01-1A-1; [12] UPDATE TABLE; [13] REFER TO EA 21-153-02672 SUMMARY REQUIREMENT; BARCODE: TTG8Q006M0GH;

Part: LINK — CRACKED (RT MLG) · airframe 59,501 hrs · 29,318 cycles

RIGHT MLG SUPPORT BEAM ;LOWER O/B STABILIZER LINK CRACKED APPOX 1 INCH LONG . CRACK IS LOCATED AT FWD SIDE LUG NEAR ATTACHMENT POINT. ; / [01] REMOVED AND REPLACED THE R/H MLG SUPPORT BEAM LOWER STABILIZER LINK REF AMM 57-15-00

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 59,497 hrs · 29,315 cycles

RT MLG FWD TRUNNION SUPPORT FITTING ; RT MLG FWD TRUNNION SUPPORT FITTING; LOWER O/B LUG; I/B FACE HAS EVIDENCE OF CORROSION / REPAIRED AS PER EA-1-A57-3246 REV 12

Part: COVER — MISSING (R1 DOOR SLIDE) · airframe 59,379 hrs · 29,255 cycles

R1 DOOR SLIDE LENSE COVER MISSING REF LP# 1811387 MEL 25-10-01 AUTH# 13799 ; / INSTALLED R1 DOOR SLIDE COVER PER AMM 20-30-11.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 59,291 hrs · 29,203 cycles

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

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 59,291 hrs · 29,203 cycles

LEFT HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED ; /

Part: SEAL — BENT (HORIZONTAL STAB) · airframe 59,291 hrs · 29,203 cycles

LEFT HORIZONTAL STABILIZER LOWER SLIDING SEAL BENT ; /

Part: SCUFF PLATE — BENT (AFT CARGO) · airframe 57,862 hrs · 28,379 cycles

AFT CARGO CENTER THRESHOLD HAS AFT CORNER CURLED/BENT UP APPROXIMATELY .1875 X .1875. / REMOVED AND REPLACED CENTER SCUFF PLATE REF AMM 53-11-02.

Part: CEILING PANEL — LOOSE (CABIN) · airframe 57,714 hrs · 28,286 cycles

FORWARD GALLEY CEILING PANEL LOOSE. RESECURED FORWARD CEILING EMERGENCY EXIT SIGN PANEL, AS PER AMM 33-51-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,698 hrs · 28,273 cycles

EMERGENCY LIGHTS ON ROW 7 A/B/C AND 9 A/B/C INOPERABLE. REMOVED & REPLACED BATTERY AT LOC M2335. OPS CK GOOD, REF AMM 33-51-06 AT ROWS 7 A/B/C, 9 A/B/C, & .14 A/B/C

Part: LIGHT — UNSECURE (CABIN) · airframe 57,011 hrs · 27,837 cycles

FORWARD R/H SIDE AISLE PHOTOLUMINESCENT STRIP NOT SECURED. / SECURED PHOTOLUMINESCENT STRIP PER SIP.

Part: LIGHT — BROKEN (CABIN) · airframe 56,474 hrs · 27,473 cycles

FORWARD ENTRY DOOR EMERGENCY LIGHT COVER BROKEN OFF. / R&R LIGHT PER AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,187 hrs · 27,297 cycles

R/H SIDE FUSELAGE SKIN INNER SURFACE AROUND HOLES CORRODED STA 667, RBL 70. / REPAIRED SKIN IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,187 hrs · 27,297 cycles

FUSELAGE INNER SURFACE OF SKIN AROUND HOLES CORRODED AT BS. 667, LBL 70. / REPAIRED SKIN PER EA.

Part: FITTING — CORRODED · airframe 56,187 hrs · 27,297 cycles

KICK FITTING PN 112A1513-2 IS CORRODED AND REQUIRES REPLACEMENT. THIS NRC IS FOR CORROSION REPORTING PURPOSE. STA 666; RBL 73; WL 190 / FITTING WAS REPLACED BY BOEING AOG TEAM ON FRR-8. CORROSION FINDING # 20217.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,185 hrs · 27,296 cycles

LEFT HAND PICKLE IS CRACKED AT STA 663. / THE LH PICKLE FORK FRAME P/N 144A2410-7 WAS REMOVED AND REPLACED BY BOEING AOG UNDER AGREEMENT SWA-RE-1906934 IN VCV. REF. SWA EA 1-753-35957 REV IR FOR DETAILS OF THE BOEING AOG VISIT AND FOR DOCUMENTATION OF ASSOCIATED REPAIRS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,185 hrs · 27,296 cycles

REF LOG PAGE 1102696 LEFT HAND PICKLEFORK CRACKED AT STA 663 / THE LH PICKLE FORK FRAME P/N 144A2410-7 WAS REMOVED AND REPLACED BY BOEING AOG UNDER AGREEMENT SWA-RE-1906934 IN VCV. REF. SWA EA 1-753-35957 REV IR FOR DETAILS OF THE BOEING AOG VISIT AND FOR DOCUMENTATION OF ASSOCIATED REPAIRS. CLEARING# 5812

Part: FORK — CRACKED (FUSELAGE) · airframe 56,185 hrs · 27,296 cycles

L/H PICKLE FORK IS CRACKED AT STATION 663. / COMPLIED WITH EA 1-753-35800; ACCOMPLISH PERMANENT REPAIR OR REPLACEMENT OF DISCREPANT PARTS WITHIN 1 NON-REVENUE FERRY FLIGHT FLIGHT CYCLE FROM DAL-VCV. CONDITIONS FOR FERRY-KNOWN OR FORCAST TURBULANCE IS AVOIDED; FLIGHT IS NON-REVENUE WITH NO PASSENGERS AND NO-REVENUE CARGO-MINIMUM CREW. REFERENCE LP 1102699

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,086 hrs · 27,219 cycles

R1 DOOR EMERGENCY SLIDE LIGHT INOP AT M1674. R&R BATTERY PACK PER AMM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 56,086 hrs · 27,219 cycles

LOWER EMERGENCY LIGHT INOP. CONNECTED CONNECTOR PER WDM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,086 hrs · 27,219 cycles

R1 DOOR EMERGENCY EXIT LIGHT ON GALLEY INOP AT M1674. R&R BATTERY PACK PER AMM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 56,086 hrs · 27,219 cycles

AISLE LIGHT AT 13R INOP. CONNECTED CONNECTOR PER WDM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,086 hrs · 27,219 cycles

RT EMERGENCY AISLE LIGHTS INOP BETWEEN SEAT ROWS 3 TO ROW 6. R&R BATTERY PACK PER AMM.

Part: PANEL — CRACKED (LEFT WING) · airframe 56,086 hrs · 27,219 cycles

LT WING LWR L/E PNL 521FB FWD O/B CORNER HAS CRACK FROM FASTENER HOLE TO EDGE / REMOVED PANEL 521FB FROM AIRCRAFT IAW SOPM 20-50-01 59402U 22SEP19 8119C 22SEP19 LT WING LWR L/E PNL 521FB FWD O/B CORNER CRACK WAS REPAIRED IAW SRM 51-70-05-22-6 20021C 24SEP19 INSTALLED LT WING LWR L/E PNL 521FB PER SRM 2050-01

Part: ATTACH BRACKET — CRACKED (AFT SERVICE DOOR) · airframe 56,086 hrs · 27,219 cycles

AFT GALLEY DOOR PANEL; 844DZ; AFT ATTACH BRACKET IS CRACKED. / REPLACED AFT GALLEY DOOR PANEL; 844DZ; AFT ATTACH BRACKET IAW SRM 51-40-02-0G-0.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

SUPPORT CHANNEL CORRODED BETWEEN BS 259 TO BS 270, BETWEEN LBL 2.8 TO RBL 2.8. R&R SUPPORT CHANNEL IAW DWG AND SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

LATERAL INTERCOSTAL CORRODED AT BS 270, BETWEEN LBL 7.5 TO RBL 7.5. FORWARD FLANGE AROUND NUTPLATE. REMOVED INTERCOSTAL PER SRM & EA.

Part: FRAME — CRACKED (CABIN) · airframe 56,086 hrs · 27,219 cycles

BS 312 FRAME CRACKED AT END RADIUS ABOVE FWD ENTRY DOOR UPPER SILL WEB. / REPAIRED BS 312 FRAME AT END RADIUS ABOVE FWD ENTRY DOOR UPPER SILL WEB. PER ER# 19-04626 AND EA# 1-753-35556; REV IR.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

R2 DOOR MOP SILL CORRODED BETWEEN BS 960 TO BS 986, RBL 54. R&R MOPSILL IAW SRM & DWG.

Part: FRAME — CORRODED (CABIN) · airframe 56,086 hrs · 27,219 cycles

***CORROSION*** BS 540FRAME BETWEEN STR 8 AND 9 R/H RBL 58 WL 272. / REPAIRED DAMAGE ON BS 540 FRAME BETWEEN STR 8 AND 9 R/H; RBL. 58; WL 272 PER ER 19-04625 REV IR AND EA # 1-753-35582 REV IR.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

OUTBOARD OF MOP SILL ANGLE CRACKED AT BS 293, RBL 53. R&R ANGLE IAW EA AND SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS 540 TO BS 727B, RBL 45. R&R SEAT TRACK IAW SRM, AMM, & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS 540 TO BS 727B, LBL 25. R&R SEAT TRACK CROWN IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

SEAT TRACK CROWN CORRODED AT BS 500C+8-10 TO BS 520, LBL 25. REPAIRED SEAT TRACK IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO BS 328, RBL 30.5. R&R FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R&R FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 56,086 hrs · 27,219 cycles

CABIN PANEL 242UF HAS DAMAGED INSERTS. / CABIN FLOOR PANEL 242UF WITH DAMAGED INSERTS WAS REPAIRED IAW SRM 53-00-50-2R-1 59702U 09/02/19

Part: ANGLE — CORRODED (FSD THRESHOLD) · airframe 56,086 hrs · 27,219 cycles

***CORROSION*** ON FWD SERVICE DOOR THRESHOLD SUPPORT ANGLE BS 308-325 RBL55 WL208. / REMOVED AND REPLACED FWD SERVICE DOOR THRESHOLD SUPPORT ANGLE-CHORD BS291.5-328 RBL55 WL208 IAW SRM 51-40-05-0G-0 SRM 51-40-02-0G-0 AND BOEING DWG 141A6310

Part: SPLICE STRAP — CORRODED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

AFT CARGO BAY CARGO FLOOR SPLICE STRAP CORRODED AT BS 887, BETWEEN RBL 10 TO LBL 10. R&R SPLICE STRAP IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

AFT CARGO BAY, LOWER BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, BETWEEN LBL 10 TO RBL 20. R&R ANGLE IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

AFT CARGO BAY, VERTICAL WEB CORRODED BETWEEN BS 807 TO BS 827, RBL 6. R&R VERTICAL WEB PER SRM & DWG.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

AFT CARGO BAY, LT FLOOR TO SIDEWALL SUPPORT PLATE HAD AREAS CORRODED BETWEEN BS 727 TO BS 847, LBL 23. R&R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (AFT CARGO) · airframe 56,086 hrs · 27,219 cycles

AFT CARGO BAY INTERCOSTAL ANGLE BELOW SHIELD BS 767- 787 RBL 23 WL 156 IS CORRODED / INSTERCOSTAL ANGLE BELOW SHIELD BS 767-787 RBL 23 WL156 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. REMOVED REPLACED INTERCOSTAL ANGLE PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 146A8123.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

AFT CARGO BAY SHIELD FORWARD OF CARGO DOOR CORRODED BETWEEN BS 767 TO BS 787, RBL 23. R&R SHIELD PER SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

AFT CARGO BAY, VERTICAL WEB CORRODED BETWEEN BS 787 TO BS 807, RBL 6. R&R VERTICAL WEB PER SRM & DWG.

Part: PLATE — CORRODED (AFT CARGO) · airframe 56,086 hrs · 27,219 cycles

AFT CARGO BAY; R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION BS727 TO BS767 RBL23 WL156 / REMOVED & REPLACED ACB R/H FLOOR TO SIDEWALL SUPPORT PLATE BS 727-767; RBL 23; WL 156 IAW SRM 51-40-02; SRM 51-40-05; DWG #146A7500

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 500A TO BS 500B, RBL 23. R&R SUPPORT IAW SRM & DWG.

Part: GUSSET — CRACKED (FWD CARGO) · airframe 56,086 hrs · 27,219 cycles

FWD CARGO BAY AFT BULKHEAD GUSSET IS CRACKED AT BS500D STR19L / REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD GUSSET @ BS 500D STR19L IAW SRM 51-40-05; SRM 51-40-02; AND DWG 143A7902

Part: WEB — CORRODED (FUSELAGE) · airframe 56,086 hrs · 27,219 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 480, RBL 27. R&R WEB PER SRM & DWG.

Part: GUSSET — CRACKED (FWD CARGO) · airframe 56,086 hrs · 27,219 cycles

FWD CARGO BAY AFT BULKHEAD GUSSET IS CRACKED AT BS500D STR19R / REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD GUSSET @ BS500D STR19R IAW SRM 51-40-02; SRM 51-40-05 AND DWG 143A7902.

Part: PLATE — CRACKED (R/H WING) · airframe 56,086 hrs · 27,219 cycles

RIGHT WING TRAILING EDGE WIGGLE PLATE JUST O/B OF SWING DOWN PANEL CRACKED / REMOVED WIGGLE PLATE RIGH WING JUST O/B OF SWING DOWN PANEL IAW SRM 51-40-02-0G-01 89813U 08-31-19 LEAD 286 8/31/19 REPLACED WIGGLE PLATE RIGHT WING TRAILING EDGE JUST O/B OF SWING DOWN PANEL. IAW SRM 51-40-02-0G-0 89813U 09-01-19 FASTENERS IAW AIPC 57-50-00-22

Part: NUT PLATE — CRACKED (L/H WING) · airframe 56,086 hrs · 27,219 cycles

AT LEFT WING TRAILING EDGE NUT PLATE BEAM BELOW #5 SPOILER PANEL IS CRACKED / REMOVED AND REPLACED NUT PLATE BEAM AT LEFT WING TRAILING EDGE; BELOW #5 SPOILER PANEL IAW SRM 51-40-02-G0-0 AND DRAWINGS 115A3758; 115A3712 59796C 30AUG19

Part: PLATE — CRACKED (RT WING) · airframe 56,086 hrs · 27,219 cycles

RT WING TRAILING EDGE WIGGLE PLATE CRACKED AT RSS 293. R&R WIGGLE PLATE IAW SRM.

Part: FAIRING — CRACKED (LEFT WING) · airframe 56,086 hrs · 27,219 cycles

#3 CANOE FAIRING 542BB HAS A CRACKED INNER SKIN BELOW LINKAGE / #3 CANOE FAIRING 542BB WITH A CRACKED INNER SKIN BELOW LINKAGE WAS REPAIRED PER SWA EA 1-757-16542 REV IR AND ATS ER# 19-04575 REV IR DATED 10-SEP-19

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 56,086 hrs · 27,219 cycles

VAPOR BARRIER CRACKED AT BS 663, BETWEEN LBL 8 TO LBL 75. R&R VAPOR BARRIER PER SRM & DWG.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 55,533 hrs · 26,846 cycles

AIR CONDITIONING DISTRIBUTION BAY, FLOORBEAM CRACKED AT BS. 540, BETWEEN L/H AND R/H OF BL 0. R&R INTERCOSTAL PER SRM.

Part: SUPPORT — CRACKED (RIGHT WING) · airframe 55,533 hrs · 26,846 cycles

RIGHT WING AFT TRAILING EDGE SEAL SUPPORT CRACKED / REMOVED AND REPLACED RIGHT WING AFT TRAILING EDGE SEAL SUPPORT PER SRM 51-40-02 AND MM 20-50-11

Part: INTERCOSTAL — BROKEN (FUSELAGE) · airframe 54,384 hrs · 26,122 cycles

FLOORBEAM INTERCOSTAL BROKEN BETWEEN BS 312 TO BS 328 LT SIDE. R&R INTERCOSTAL IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,362 hrs · 26,105 cycles

LT EMERGENCY EXIT SIDEWALL LIGHT INOP. R&R LIGHT ASSEMBLY IAW AMM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,674 hrs · 25,642 cycles

FLOORBEAM WEB CRACKED BETWEEN BS 500A TO BS 500B, STR 26R. REPAIRED WEB IAW SRM.

Part: BRACKET — CRACKED (LOWER EXT FUSELA) · airframe 53,260 hrs · 25,389 cycles

FUSELAGE L/H FWD WING TO BODY FARING AFT SUPPORT BRACKET CRACKED. / REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02

Part: PLATE — CRACKED (RT WING) · airframe 51,221 hrs · 24,058 cycles

TRAILING EDGE FIXED PANEL 651GB FORWARD PANEL SUPPORT CRACKED. (WIGGLE PLATE.) / REMOVED AND REPLACED PER SRM 51-40-02

Part: WIRE HARNESS — UNSECURE (CABIN) · airframe 50,279 hrs · 23,484 cycles

RT EMERGENCY EXIT AFT LIGHT INOP. SECURED HARNESS IAW WDM.

Part: CARRIAGE — ELONGATED (LT WING) · airframe 49,368 hrs · 22,908 cycles

CCO 57-52-0048; LEFT HAND INBOARD FLAP CARRIAGE; OUTBOARD LOWER MOUNT BOLT HOLE IS NOT TRUE AND ROUND. / REMOVED AND REPLACED #4 INBOARD FLAP CARRIAGE IAW CCO 57-52-0048. REPLACED WITH SERVICABLE CARRIAGE. POS: 4 TAG/GRB NO.: 29420 P/N OFF: 113A2800-3 S/NON OFF: 7822 #4 P/N ON: 113A2800-3B S/N ON: 3H2326

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 49,368 hrs · 22,908 cycles

AFT CARGO PIT AFT CORNER SCUFF PLATE CRACKED / CRACKED AFT CARGO PIT AFT CORNER WELDED ON W/O 36201-1000-0001 AND SA EA 1-A53-2076 REV 11

Part: ANGLE — CRACKED (RT WHEEL WELL) · airframe 49,368 hrs · 22,908 cycles

RIGHT WHEEL WELL; STATION 663; RBL 16; HORSESHOE ANGLE ABOVE THE RIGHT PACK EXHAUST DUCT; IS CRACKED ON THE INBOARD FLANGE. / REMOVED AND INSTALLED NEW HORSESHOE ANGLE ON THE RIGHT WHEEL WELL; STATION 663 AT EXHAUST DUCT IAW DWG 111A1000 AND IAWSRM 51-40-02-0G ATAG#GW0931

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 49,368 hrs · 22,908 cycles

WING TO BODY FAIRING 195BR HAS AREA OF DELAMINATION AT TOP AFT END. / REPAIRED WING TO BODY FAIRING 195BR AT TOP AFT END I/A/W SRM 51-70-04-SR-1 PAR 4-B-F REV 62

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 49,368 hrs · 22,908 cycles

R\H HORZ STAB PANEL 343AB HAS METAL BLADE SEAL CRACKED. / REMOVED AND REPLACED STAB PNL SEAL ON PNL 343AB IAW SOPM 20-50-01 STEP 3F.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 49,368 hrs · 22,908 cycles

LT MAIN WHEEL WELL VERTICAL STIFFENER CRACKED AT BS 663, LBL 25. R&R STIFFENER IAW SRM AND DWG.

Part: ANGLE — CRACKED (LT WHEEL WELL) · airframe 49,368 hrs · 22,908 cycles

LEFT WHEEL WELL; STATION 663; LBL 16; HORSESHOE ANGLE ABOVE THE LEFT PACK EXHAUST IS CRACKED ON THE INBOARD ANGLE. / REMPOVED AND INSTALLED NEW HORSESHOE ANGLE IN THE LEFT WHEEL WELL; STATION 663 AT PACK EXHAUST DUCT IAW DWG 111A1000 AND IAW SRM 51-40-02-0G

Part: SKIN — CRACKED (LE SLAT) · airframe 49,368 hrs · 22,908 cycles

LT WING NR 1 SLAT LOWER SURFACE OF THE LEADING EDGE NOSE SKIN AT ACTUATOR CRACKED. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,274 hrs · 22,852 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R&R LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,274 hrs · 22,852 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,704 hrs · 22,482 cycles

L2 DOOR EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 48,285 hrs · 22,235 cycles

MID CABIN OVERHEAD EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 47,131 hrs · 21,561 cycles

EMERGENCY LIGHTING BATTERY PACK M1672 FAILED CAPACITY CHECK. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 47,131 hrs · 21,561 cycles

EMERGENCY LIGHTING BATTERY PACK M1669 FAILED CAPACITY CHECK. R&R BATTERY PACK PER AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 46,050 hrs · 20,949 cycles

L1 DOOR EMERGENCY SLIDE LIGHT LENS LOOSE. R & R THE LENS IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 44,912 hrs · 20,310 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 44,912 hrs · 20,310 cycles

RIGHT AFT SERVICE DOOR EMER EXIT LIGHT INOPERATIVE. R & R BATTERY CHARGER IAW MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 42,731 hrs · 19,027 cycles

FORWARD SERVICE DOOR EMER LIGHT INOPERATIVE. FOUND CONNECTOR LOOSE, RE-SEATED CONNECTOR IAW WDM & AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

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

Part: RETAINING CLIP — BROKEN (R2 DOOR) · airframe 42,731 hrs · 19,027 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR QUICK RELEASE RETAINER CLIP BROKEN. R & R CLIP IAW AMM.

Part: STRAP — CORRODED (CABIN) · airframe 42,731 hrs · 19,027 cycles

RIGHT EMER EXIT HATCH ESCAPE STRAP HOOK. R & R STRAP IAW AMM.

Part: HOOK — CORRODED (ESCAPE STRAP) · airframe 42,731 hrs · 19,027 cycles

LEFT EMER EXIT HATCH ESCAPE STRAP HOOK CORRODED. R & R STRAP IAW AMM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

R1 DOOR FWD FRAME LOWER STUB BEAM CRACKED AT INBD HOLE AT WL 208. REPAIRED STUB BEAM IAW ER & EA.

Part: SLIDE — WORN (R2 DOOR) · airframe 42,731 hrs · 19,027 cycles

R2 DOOR EMER EVAC SLIDE SKIRT WORN. R & R SLIDE IAW CARD.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

FORWARD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 420 TO 440, BETWEEN STRINGER 24L TO 25L. R & R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,731 hrs · 19,027 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO 294.5, UNDER FLOOR ACCESS PANEL 221AF. R & R INTERCOSTAL IAW SRM.