N8308K

Part: LENS — MISSING (ZONE 200) · airframe 45,163 hrs · 21,101 cycles

R2 SERVICE DOOR VERTICAL EXIT/SALIDA VERTICAL LENS COVER MISSING. REPLACED WITH NEW PER M/M SIP

Part: LIGHT — CRACKED (ZONE 200) · airframe 44,526 hrs · 20,780 cycles

PHOTO LUMINESCENT DAMAGED, CRACKED IN SEVERAL AREAS. REMOVED AND REPLACED THE PHOTO LUMINESCENT THAT WAS DAMAGED THROUGH OUT CABIN IAW AMM 33-51-15-960-801.

Part: HANDLE — LOOSE (ZONE 800) · airframe 44,526 hrs · 20,780 cycles

ASSIST HANDLE ON L2 DOOR LINER LOOSE. SECURED L2 DOOR ASSIST HANDLE IAW AMM 52-13-31.

Part: HANDLE — LOOSE (ZONE 800) · airframe 44,526 hrs · 20,780 cycles

ASSIST HANDLE LOOSE FWD. SIDE OF R2 DOOR. SECURED THE R2 DOOR ASSIST HANDLE IAW AMM 52-41-31.

Part: FILLER — BROKEN (ZONE 100) · airframe 44,526 hrs · 20,780 cycles

GPD LOWER LATCH LANDING HAS FILLER BROKEN OUT. THE DAMAGE WAS REPAIRED PER SRM 53-10-15-2R-4 REPAIR 4 AND EA 25-153-02815.

Part: HANDLE — LOOSE (ZONE 800) · airframe 44,526 hrs · 20,780 cycles

R1 DOOR ASSIST HANDLE LOOSE. SECURED THE R1 DOOR ASSIST HANDLE IAW AMM 52-41-31.

Part: STRAP — BROKEN (ZONE 200 SEAT) · airframe 44,251 hrs · 20,628 cycles

SEAT 16C WEB STRAP BROKEN. REMOVED AND REPLACED IAW CMM 25-23-60-NG.

Part: TAIL CONE — PULLED (ZONE 500 FLAP) · airframe 43,908 hrs · 20,452 cycles

NUMBER 3 FLAP FAIRING TAIL CONE HAS SIX PULLED RIVETS ON THE OUTBOARD SIDE. REMOVED AND REPLACED NR 3 FLAP TAIL CONE CANOE PER SRM 51-40-02. APPLIED SEALANT PER SRM 51-40-02.

Part: RECEPTACLE — FIRE (ZONE 200) · airframe 43,766 hrs · 20,380 cycles

GROUND POWER RECEPTACLE ARCED AND CAUGHT FIRE. PERFORMED POWER RECEPTACLE INSPECTION. NO DEFECTS NOTED IAW AMM 24-41-11 OPS CHECK GOOD IAW AMM 24-22-00

Part: SIGN — MISSING (ZONE 200) · airframe 43,585 hrs · 20,282 cycles

L1 DOOR MISSING EMERGENCY EXIT/SALIDA SIGN. REMOVED AND REPLACED PER AMM 33-51-03-960-803-NG (EMERGENCY AISLE LIGHT (EAL) - LENS REPLACEMENT - PERMANENT)

Part: HOOK — OUT OF POSITION (ZONE 800) · airframe 42,827 hrs · 19,885 cycles

AFT ENTRY DOOR GIRT BAR HOOKS BENT <[01]. REPOSITIONED GRIT BAR HOOKS REF AMM 25-66-01 NO DEFECTS NOTED. AC OK FOR SERVICE.

Part: LENS — MISSING (ZONE 200) · airframe 41,393 hrs · 19,100 cycles

EMERGENCY LIGHT LENS CRACKED AT CEILING PANEL ABOVE 10DEF<[01] REMOVED AND REPLACED LENS PER M/M 33-51-03.

Part: SUPPORT — CARBONED (ZONE 400) · airframe 41,320 hrs · 19,055 cycles

#1 PYLON AFT STRUT FAIRING AFT O/B SUPPORT CRACKED; CRACK MEASURES APPROXIMATELY 1.8 INCHES LONG VERIFIED BY NDT<[01] ACCOMPLISHED EA M-23-154-01884. OK TO CONTINUE;[02] CORRECTED FAULT FAILURE TYPE.;[03] CORRECTED MEASUREMENT OF 'VISUAL CRACK' AND FAILURE CODE PER REQUEST OF BRADLEY HARTMAN AND JOCELYN NICKLE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,784 hrs · 18,252 cycles

L/H AFT EXTERIOR EMERGENCY LIGHT INOP<[01] OK TO CONTINUE PER MEL 33-14-01 SP#1 AUTHORIZATION #194505;[02] R+R?D BATTERY PACK & CHARGER (M1670) IAW AMM 33-51-06

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,784 hrs · 18,252 cycles

L/H AFT EXTERIOR EMERGENCY LIGHT INOP<[01] OK TO CONTINUE PER MEL 33-14-01 SP#1 AUTHORIZATION #194505;[02] R+R?D BATTERY PACK & CHARGER (M1670) IAW AMM 33-51-06

Part: SIGN — DETACHED (LT OVERWING) · airframe 39,585 hrs · 18,149 cycles

EMERGENCY EXIT ROW SIGN FELL OFF<[01] R/R EMERG. EXIT SIGN AT LEFT OVER WING EXIT IAW M/M 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,558 hrs · 18,134 cycles

EXTERIOR EMERGENCY EGRESS LIGHT INOP AT LH AFT OVER WING EXIT<[01] RELAMPED EXTERIOR EMERGENCY EGRESS LIGHT IAW AMM 33-51-04. OPS CHECKS GOOD

Part: CONNECTOR — INOPERATIVE (ZN 200 FUS TOP) · airframe 37,857 hrs · 17,208 cycles

MAIN PASSENGER CABIN R/H AFT FLIGHT ATTENDANT SEAT FLASHLIGHTS (2EA) ARE INOP.<[01] UPON FURTHER INVESTIGATION FOUND AFT ATTENDANT FLASHLIGHT CONNECTORS TO BE DISCONNECTED; RECONNECTED CONNECTOR AND INSTALLED ON THE MOUNTING BRACKET IAW AMM 25-64-00-900-806.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTS

Part: SIGN — INOPERATIVE (ZN 200 FUS TOP) · airframe 37,857 hrs · 17,208 cycles

FWD SERVICE DOOR CUTOUT LOWER EXIT SIGN LIGHT HAS BURNED OUT BULBS.<[01] RELAMPED FORWARD SERVICE DOOR EMERGENCY INDICATOR SIGN AND TESTED PER AMM 33-51-01-960-801; NO DEFECTS NOTED.;[02] VERIFIED CORRECTIVE ACTION #1

Part: SIGN — BURNED (ZN 200 FUS TOP) · airframe 37,857 hrs · 17,208 cycles

L/H FWD AND AFT OVER WING DOORS LOWER EXIT LIGHT SIGNS HAVE BURNED OUT BULBS.<[01] RELAMPED LEFT-HAND FORWARD AND AFT OVERWING EMERGENCY EXIT LOWER INDICATOR SIGNS AND TESTED PER AMM 33-51-01-960-801; NO DEFECTS NOTED.;[02] VERIFIED CORRECTIVE ACTION #1

Part: COVER PLATE — MISSING (ZN 200 FUS TOP) · airframe 37,857 hrs · 17,208 cycles

MAIN CABIN CEILING EMERGENCY EXIT LIGHT IS MISSING ACCESS COVER PLATE<[01] INSTALLED MAIN CABIN CEILING EMERGENCY EXIT LIGHT COVER PLATE PER AMM 33-51-01-960-802.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] VERIFIED MEASUREMENTS TABLE.;[04] UPDATED PARTS USED;[05] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

FWD CARGO BAY CUTOUT AFT CORNER SCUFF PLATE CRACKED<[01] SCUFF PLATE WAS FOUND CRACKED UPON REMOVAL. IT WAS SENT OUT FOR REPAIR. RECEIVED REPAIRED PART AND REINSTALLED IAW AMM 53-11-02; SOPM 20-50-19; SRM 53-30-15-2R-1; SRM 51-20-01; SOPM 20-20-02. SOPM 20-30-02.;[02] REJECT REF [TTG8Q00NYPW6];[03] CORRECTION TO LINE 1: SCUFF PLATE WAS FOUND CRACKED UPON REMOVAL. IT WAS SENT OUT FOR REPAIR. RECEIVED REPAIRED PART AND REINSTALLED IAW AMM 53-11-02 (F)2); SOPM 20-50-19; SRM 53-30-15-2R-1 B.(6)-(13); SRM 51-20-01; SOPM 20-20-02. SOPM 20-30-02.;[04] REJECT: SEE TTG8Q00NZG9P;[05] VERIFIED CORRECTIVE ACTION 2;3;4<BR>VERIFIED MEASUREMENTS TABLE.<BR>JOB COMPLETE.

Part: BAFFLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

FWD CARGO BAY BAFFLE CRACKED BS 500B - BS 500C RBL 25 WL 154<[01] UPDATED STEP 1.;[02] UPDATED MEASUREMENT TABLE.;[03] COMPLETE STEP 2.;[04] UPDATE STEP 1.;[05] UPDATED MEASUREMENT TABLE.;[06] COMPLETED STEP 1.;[07] TASK COMPLETE:<BR>REMOVED FWD CARGO BAFFLE AT BS 500B-500C IAW SRM 51-40-02-0G-0. LOCATE AND DRILLED NEW FWD CARGO BAFFLE IAW DWG 143A7505; DWG 143A7510; AND SRM 51-40-02-0G-0. INSTALLED NEW FWD CARGO BAFFLE IAW SRM 51-40-02-0G-0; DWG 143A7505; AND DWG 143A7510.;[08] VERIFIED CORRECTIVE ACTION COMPLETE; VERIFIED MEASUREMENT TABLE.

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

FWD CARGO BAY INTERCOSTAL BS 500F-500G LBL 25 IS CRACKED<[01] UPDATED STEP 1-3;[02] VERIFIED STEPS 1;2;3 COMPLETE.;[03] REMOVED AND REPLACED NEW INTERCOSTAL AT FCB AT BS 500F-500G LBL 25 IAW BOEING DWG 143A7505; SRM 53-30-53-2R-1 AND SRM 51-40-02;[04] COMPLETE

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY FWD SHIELD ATTACH ANGLE CRACKED BS 787 - BS 794 RBL 21 WL 163<[01] UPDATED STEP 1-3;[02] UPDATED STEP 3 AND 4;[03] REMOVED AFT CARGO BAY FWD SHIELD ATTACH ANGLE BS 787 - BS 794 RBL 21 WL 163 SRM 51-40-02-0G-0<BR><BR>RECEIVED NEW ATTACH ANGLE<BR>ITEM# : 146A8125-52<BR>PO#: 939552/1<BR><BR>LOCATED AND DRILLED NEW ATTACH ANGLE IAW SRM 51-40-05-0G-0; DWG 146A0081 ID:0046 REV:-; AND DWG 146A8123 ID:0019 REV:-<BR><BR>INSTALLED NEW SHIELD ATTACH ANGLE IAW SRM 51-40-02-0G-0; DWG 146A0081 ID:0046 REV:-; AND DWG 146A8123 ID:0019 REV:-;[04] UPDATED MEASUREMENTS TABLE;[05] UPDATED STEP 5;[06] COMPLETE

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY FWD SHIELD ATTACH ANGLE CRACKED BS 767 - BS 787 RBL 21 WL 163<[01] UPDATED STEP 1 - 3;[02] UPDATED STEP 3 AND 4;[03] REMOVED AFT CARGO BAY FWD SHIELD ATTACH ANGLE BS 767 - BS 787 RBL 21 WL 163 IAW SRM 51-40-02-0G-0<BR><BR>RECEIVED NEW ATTACH ANGLE<BR>ITEM # : 146A8125-53<BR>PO# : 935913/1<BR><BR>LOCATED AND DRILLED NEW ATTACH ANGLE IAW SRM 51-40-05-0G-0; DWG 146A0081 ID:0046 REV:- ;AND DWG 146A8123 ID:0016 REV:-<BR><BR>INSTALLED NEW SHIELD ATTACH ANGLE IAW SRM 51-40-02-0G-0; DWG 146A0081 ID:0046 REV:- ;AND DWG 146A8123 ID:0016 REV:-;[04] UPDATED MEASUREMENT TABLE;[05] UPDATED STEP 5;[06] COMPLETE

Part: PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

WING CENTER SECTION BREAK PANEL IS CRACKED AT BS 540; LBL 1; WL 208<[01] PANEL BREAK TO BE REPLACED ON FAULT TTG8Q00NH5O8.;[02] CORRECTION: PANEL BREAK TO BE REPLACED ON FAULT TTG8Q00NH508;[03] VERIFIED CORRECTIVE ACTION 2

Part: ATTACH ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 37,857 hrs · 17,208 cycles

WING CENTER SECTION HAS A CRACKED CABLE INTERCOSTAL ATTACH ANGLE AT BS 685+9; RBL 24; WL 203<[01] REMOVED AND REPLACED CABLE INTERCOSTAL ATTACH ANGLE AT BS 685+9; RBL 24; WL 203 PER SRM 51-40-02-0G; SRM 51-40-04 SOPM 20-50-01 AND BOEING DWG 273A9110. USED TOOL ID: ATS2686 DUE: 11/2023.;[02] VERIFIED CORRECTIVE ACTION 1.<BR>VERIFIED MEASUREMENTS.<BR>JOB COMPLETE.

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

O2 BOTTLE FWD SUPPORT BRACKET; LOWER ATTACH ANGLE IS CRACKED AT O/B FASTENER; BS 380+2; RBL 10; WL 157<[01] REMOVED AND REPLACED NEW O2 BOTTLE FWD SUPPOR P/N 3145 LOT. 1540115 AT BS 380 WL 157 IAW SRM 51-40-02;[02] VERIFIED STEP 1 COMPLETE; MEASUREMENT TABLE; CARD COMPLETE.

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

INTERCOSTAL BS 500G-500H RBL22 WL 156 IS CRACKED.<[01] UPDATE STEP #1;[02] UPDATE STEP#2-3;[03] EDITED MEASUREMENT TABLE;[04] REMOVED AND REPLACED INTERCOSTAL AT BS 500G-500H RBL 22 WL 156 IAW BOEING DWG 143A7505 AND SRM 51-40-02.;[05] VERIFIED CORRECTIVE ACTION 4;[06] VERIFIED MEASUREMENT TABLE

Part: WASHER — EXCESS PLAY (DOOR HANDLE) · airframe 37,857 hrs · 17,208 cycles

ASD; EXCESSIVE PLAY IN PLATE BEHIND INTERIOR DOOR HANDLE<[01] ELIMINATED EXCESSIVE PLAY BY REPLACING DAMAGED WASHERS BEHIND THE CONTROL CAM ASSY. PER CMM 52-41-04-81205;[02] VERIFIED CORRECTIVE ACTION 1

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

INTERCOSTAL CRACKED; BS312-328; LBL46; WL208<[01] REMOVED AND REPLACED INTERCOSTAL BETWEEN BS312 - BS328; LBL46; WL208 PER SRM 51-40-02-0G-0 AND BOEING DWG. 141A5400.

Part: STRAP — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

UPPER SUPPORT STRAP CRACKED AT I/B RIVET; BS538; RBL2; WL208<[01] UPPER SUPPORT STRAP (PLATE) TO BE INSTALLED; ATTACHED TO PANEL BREAK ON CARD #TTG8Q00NH415;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

INTERCOSTAL CRACKED; BS500I-520; BL0; WL208<[01] REMOVED DAMAGED ANGLE ON INTERCOSTAL AT BS 500I-BS 520 BL0 IAW SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL ANGLE IAW SRM 51-40-05-0G-0; DWG 143A5400 SHT 115 REV :A; OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION 2.<BR>OK TO INSTALL;[04] INSTALLED INTERCOSTAL ANGLE AT BS 500I-BS 520 BL0 IAW SRM 51-40-02-0G-0; DWG 143A5400 SHT 115 REV :A;[05] VERIFIED CORRECTIVE ACTION STEP 4.;[06] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727D+8 - 727D+17; LBL 22; WL 161<[01] STEP 1;[02] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BETWEEN 727+4 TO BS 847; LBL 22; WL 161 IAW SRM 51-40-02; DWG:145A7500;ID:0213;REV:- AND DWG:146A7502; ID:0031;REV:- .;[03] VERIFIED CORRECTIVE ACTION 2.<BR>VERIFIED MEASUREMENTS.<BR>JOB COMPLETE.

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

INTERCOSTAL CRACKED; BS344-360; WL208<[01] CORRECTION TO FALT LOCATION; BS344-360; BL0; WL208;[02] CERTIFIED STEP 1 AND 2;[03] REMOVED AND REPLACED INTERCOSTAL FROM BS 344 TO 360; BL 0; WL 208 PER SRM 51-40-02-0G-0 AND BOEING DWG 141A5400.;[04] CERTIFIED CORRECTIVE ACTION 3 AND STEP 2;[05] UPDATED MEASURMENTS;[06] VERIFIED CORRECTIVE ACTION #3

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

INTERCOSTAL CRACKED; BS380-400; LBL14; WL208<[01] CRACK FOUNDED ONLY ON THE UPPER CHORD AT BS 380-400 LBL 14 WL 208. REMOVED AND REPLACED UPPER CHORD AT BS 380-400 LBL 14 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A5400.;[02] UPDATE STEP 4. FAULT COMPLETE;[03] VERIFIED CORRECTIVE ACTION 1

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 787+7; LBL 22; WL 164<[01] STEP 1;[02] WORK WILL BE ACCOMPLISH ON CUSTOMER CARD NBR: TTG8QOONH4KV;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLE

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727I+4 - 747+19; RBL 22; WL 162<[01] STEP 1;[02] REMOVED AND EVALUATED CORROSION AT AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727I+4 - 747+19; RBL 22; WL 162 FOUND TO BE OUT OF LIMITS IAW SRM SRM 53-00-53-1A-2.<BR><BR>PART WILL BE REPLACED AT CUSTOMER CARD# TTG8Q00NH3V5;[03] VERIFIED CORRECTIVE ACTION 2

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727I+5; LBL 22; WL 162<[01] STEP 1;[02] WORK WILL BE ACCOMPLISH ON CUSTOMER CARD NBR: TTG8QOONH4KV;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLE

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

SUPPORT ANGLE CRACKED; BS538; RBL2; WL208<[01] REMOVED CRACKED ANGLE (PANEL BREAK) AT BS 538 RBL 2 WL 208 IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW SUPPORT ANGLE (PANEL BREAK) IAW SRM 51-50-05-0G-0; DWG 143A5240; OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION 2.<BR>OK TO INSTALL;[04] INSTALLED SUPPORT ANGLE (PANEL BREAK) AT BS 538 BL0-RBL 25 IAW SRM 51-40-02-0G-0; DWG 143A5240;[05] ADDED/ UPDATED MEASUREMENT TABLE. FAULT COMPLETE;[06] VERIFIED CORRECTIVE ACTION 4 AND MEASUREMENT TABLE

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

UPPER SUPPORT ANGLE CRACKED; BS538; LBL2; WL208<[01] INSTALLED NEW PANEL BREAK FROM BS 540; WL 208; LBL 1-24 PER SRM 51-40-02. COMPLETED STEP 1.;[02] REMOVED AND REPLACED CRACKED UPPER SUPPORT ANGLE AT BS538 LBL2 WL208 IAW SRM 51-40-02.;[03] VERIFIED CORRECTIVE ACTION 2;[04] VERIFIED MEASUREMENT TABLE

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727D+3 - 727D+13; RBL 22; WL 161<[01] STEP 1 APPLICABLY;[02] PARTIAL COMPLETION ON STEP 4;[03] PARTIAL COMPLETION ON STEP 5;[04] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BETWEEN BS 727+4 TO BS 767 IAW SRM 51-40-02 AND DWG:146A7500 ;ID:0213; REV:-;[05] VERIFIED CORRECTIVE ACTION 4.<BR>VERIFIED MEASUREMENTS.<BR>JOB COMPLETE.

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO FWD SHIELD HAS CORROSION AT BS 767+3 - 787; RBL 22; WL 163<[01] UPDATED STEP 1 AND 2;[02] UPDATED STEP 3 AND 4;[03] UPDATED STEP 3;[04] UPDATED MEASUREMENTS TABLE;[05] UPDATED STEP 5;[06] REMOVED ACB FWD SHIELD IAW SRM 51-40-02-0G-0<BR><BR>RECEIVED NEW SHIELD<BR>ITEM#: 146A8127U12ATSMRO<BR>PO# : 932411/1<BR><BR>LOCATED; DRILLED AND COUNTERSANK NEW ACB FWD SHIELD IAW SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 146A0081 ID:0046 REV:-<BR><BR>INSTALLED NEW AFT CARGO FWD SHIELD IAW SRM 51-40-02-0G-0 AND DWG 146A0081 ID:0046 REV:-;[07] VERIFIED CORRECTIVE ACTION 6.<BR>VERIFIED MEASUREMENTS.<BR>JOB COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 747+11 - 767+15; LBL 22; WL 163<[01] STEP 1;[02] WORK WILL BE ACCOMPLISH ON CUSTOMER CARD NBR: TTG8QOONH4KV;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLE

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 747+4; LBL 22; WL 162<[01] STEP 1;[02] PART WILL BE REPLACED AT CUSTOMER CARD# TTG8Q00NH4KV DUE TO COMMON AREAS OUT OF LIMITS.;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLE

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727G+9; RBL 22; WL 162<[01] STEP 1;[02] REMOVED AND EVALUATED CORROSION AT AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727G+9; RBL 22; WL 162 FOUND TO BE OUT OF LIMITS IAW SRM SRM 53-00-53-1A-2. <BR><BR>PART WILL BE REPLACED ON CUSTOMER CARD# TTG8Q00NH3V5;[03] VERIFIED CORRECTIVE ACTION 2

Part: TIE DOWN — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY TIE DOWN HAS CORROSION AT BS 787+3; LBL 17; WL 162<[01] UPDATED STEP 1;[02] UPDATED STEP 2 AND MEASUREMENT TABLE.;[03] UPDATED STEP 3;[04] EDITED MEASUREMENT TABLE;[05] REMOVED CORROSION FROM ACB TIE DOWN AT BS 787 + 3'; LBL 17; WL 162; IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2; MATERIAL REMOVED: 0.020' AND IS FOUND IN LIMITS IAW SRM 53-00-53-1A-2; DETAIL G. APPLIED CHEMICAL CONVERSION COATING ON REWORKED AREA AT BS 787+3; LBL 17; WL 162 IAW AMM 51-21-41-370-803 AND PRIMER IAW AMM 51-21-72-370-804.;[06] VERIFIED CORRECTIVE ACTION 5

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT; COMMON TO AFT BULKHEAD SUPPORT IS CRACKED IN RADIUS AT BS 947; RBL 22; WL 184<[01] SRM 53-00-53-1A-2 IS APPLICABLE; AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT INTERCOSTAL FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; PART WILL BY REPLACEMENT; REMOVED AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT INTERCOSTAL AT BS 927 AND BS 947; RBL 22; WL 18; IAW SRM 51-40-02-0G-0 AND DWG 147A7500; ID:0037; REV: -;LOCATED AND DRILLED NEW AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT INTERCOSTAL AT BS 927 AND BS 947; RBL 22; WL 18; IAW SRM 51-40-05-0G-0 AND DWG 147A7500; ID:0037; REV:-;REQUEST OK TO INSTALL;INSTALLED NEW AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT INTERCOSTAL BETWEEN BS 927 AND BS 947; RBL 22; WL 184; IAW SRM 51-40-02-0G-0 AND DWG 147A7500; ID:0037; REV: -.

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727E+17; RBL 22; WL 161<[01] STEP 1;[02] REMOVED AND EVALUATED CORROSION AT AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727E+17; RBL 22; WL 161 FOUND TO BE WITHIN LIMITS IAW SRM SRM 53-00-53-1A-2.<BR><BR>PART WILL BE REPLACED AT CUSTOMER CARD# TTG8Q00NH3V5 DUE TO COMMON AREAS OUT OF LIMITS.;[03] VERIFIED CORRECTIVE ACTION 2

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727H+16; RBL 22; WL 162<[01] STEP 1;[02] REMOVED AND EVALUATED CORROSION AT AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727H+16; RBL 22; WL 162 FOUND TO BE OUT OF LIMITS IAW SRM SRM 53-00-53-1A-2.<BR><BR>PART WILL BE REPLACED AT CUSTOMER CARD# TTG8Q00NH3V5;[03] VERIFIED CORRECTIVE ACTION 2

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

INTERCOSTAL CRACKED; BS294-277; BL0; WL208<[01] UPDATED STEP #1;[02] INTERCOSTAL IS PRIMARY STRUCTURE. LOCATED AND DRILLED IAW DWG 141A5400; SRM 51-40-05-0G-0;[03] CERTIFY EDIT TO ACTION #1;[04] COMPLETED INSTALLATION OF INTERCOSTAL IAW DWG 141A5400; SRM 51-40-02=0G-0.;[05] FOUND NO LIMITATIONS IN SRM FOR CRACKED INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 141A5400;[06] INSTALLED INTERCOSTAL IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 141A5400;[07] CERTIFY CORRECTIVE ACTION;[08] VERIFIED CORRECTIVE ACTION 4;5;6

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 37,857 hrs · 17,208 cycles

LH HORIZONTAL STAB REMOVABLE L/E 331B INNER RIB #9 IS CRACKED<[01] UPDATED MEASURMENT TABLE;[02] REMOVED AND REPLACED L/H HORIZONTAL STAB REMOVABLE L/E 331B INNER RIB # 9; LE STA 151.75.;[03] ADDED REFERENCE FOR CORRECTIVE ACTION. 2. : REMOVED AND REPLACED L/H HORIZONTAL STAB REMOVABLE L/E 331B INNER RIB # 9; LE STA 151.75; PER SRM 51-40-02-0G-0 AND BOEING DWG. 186A1001.;[04] VERIFIED CORRECTIVE ACTION #3;[05] VERIFIED MEASUREMENTS

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

LEFT WING-TO-BODY FAIRING - CRACKED BRACKET ASSY-DUCT SUPPORT; L/H PACK BAY (MARKED)<[01] LH PACK BAY SUPPORT BRACKET CRACKED NO ALLOWABLE DAMAGE NOTED ON SRM. PART TO BE REPAIR BY REPLACEMENT. PN 212A1116-1. IAW SRM 51-10-02-0G-0 PARA 9.;[02] REMOVED AND REPLACED NEW L/H PACK BAY DUCT SUPPORT BRACKET ASSY P/N 212A1116-1; PO # 939481/1; IAW SOPM 20-50-01. <BR>TOOL TORQUE WRENCH USED ID ATS2326; UNKNOWN S/N; DUE DATE: 04/2024.;[03] VERIFIED CORRECTIVE ACTION 1;2<BR>VERIFIED MEASUREMENTS.;[04] SIGNED FOR PART;[05] VERIFIED COMPLETE

Part: STRAP — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

CORROSION ON TENSION STRAP AT AFT WET AREA BS1016+12 LBL17 WL208.<[01] EDITED STATUS FROM PENDING TO PARTIAL;;[02] UPDATED MEASUREMENT TABLE;[03] REMOVED CORROSION FROM AFT WET AREA ON TENSION STRAP BS1016+12; LBL17; WL208; THE FINAL REPAIR PROCESS WILL BE ACCOMPLISHED ON CARD TTG8Q00NJ6UY.;[04] CORRECTED MEASUREMENT TABLE;[05] VERIFIED;[06] CORRECTION: UPDATED MEASUREMENT TABLE;[07] VERIFIED RII STEPS COMPLETE;[08] VERIFIED JOB COMPLETE<BR><BR>VERIFIED MEASUREMENT TABLE

Part: INTERCOSTAL — CORRODED (ZN 200 FUS TOP) · airframe 37,857 hrs · 17,208 cycles

CORROSION AROUND FASTENERS ON FLOOR SUPPORT AT AFT WET AREA BS947+4 LBL24 WL208.<[01] UPDATED STEP 1;[02] REMOVED AND REPLACED INTERCOSTAL AT BS 947.5 TO 967; LBL 24; WL 208 PER SRM 51-40-02-0G-0 AND BOEING DWG 147A5650.;[03] VERIFIED CORRECTIVE ACTION 2.<BR>VERIFIED MEASUREMENTS TABLE.

Part: SUPPORT ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FCB BS500I LBL23 TO RBL23 WL156.<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF FCB ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE 500I LBL 23 RBL 23 WL 156 IAW SRM 53-30-08-1A-1;[02] SRM 53-30-08-1A-1 IS FOUND TO BE APPLICABLE. EVALUATED 9 SPOTS OF CORROSION FROM BS500I LBL23-RBL23 WL 156 THE DEEPEST SPOT IS .L=2.' X W=1.8' DEPTH=17. ORIGINAL THICKNESS IS 0.071; REMINING THICKNESS IS 0.054 AND FOUND TO BE OUT LIMITS;ALLOWABLE DAMAGE 1 STEP 4 FIG#103 DETAIL 'C' IAW SRM 53-30-08-1A-1<BR>CAL TOOL ID: ATS2738 DUE: 04/2024;[03] REMOVED AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FCB BS500I LBL23 TO RBL23 WL156. IAW SRM 51-40-02;[04] VERIFIED CORRECTIVE ACTION STEPS 1-3.;[05] COMPLETED STEP 1.;[06] CORRECTION TO STEP 1 STATEMENT.;[07] CORRECTION TO STEP 1 STATEMENT.;[08] UPDATED STEP 2.;[09] VERIFIED STEP 2 IN PARTIAL.;[10] UPDATED STEP 2.;[11] COMPLETED STEP 2.;[12] TASK COMPLETE:<BR>LOCATED AND DRILLED NEW FWD CARGO AFT BULKHEAD TO FLOOR SUPPORT ANGLE IAW DWG 143A7902 AND SRM 51-40-02-0G-0. INSTALLED NEW FWD CARGO AFT BULKHEAD TO FLOOR SUPPORT ANGLE IAW SRM 51-40-02-0G-0; DWG 143A7902; AND DWG 143A9481.;[13] RII STEPS COMPLETE;[14] VERIFIED JOB COMPLETE<BR><BR>VERIFIED MEASUREMENT TABLE

Part: ATTACH ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 37,857 hrs · 17,208 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500G FWD SIDE LBL25 WL155.<[01] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BS500G FWD SIDE LBL25 WL155 IAW BOEING DWG 143A7505 AND SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION 1.;[03] TASK COMPLETE

Part: ATTACH ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 37,857 hrs · 17,208 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500F FWD SIDE RBL25 WL155.<[01] UPON FURTHER INVESTIGATION INTERCOSTAL ATTACH ANGLE AT FCB BS500E FWD SIDE RBL25 WL155 FOUND NOT TO BE CRACKED. CLEANED AREA IAW SOPM 20-30-03;[02] VERIFIED MEASUREMENT TABLE<BR><BR>VERIFIED JOB COMPLETE

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500I FWD SIDE RBL25 WL155. CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500H FWD SIDE RBL25 WL155<[01] UPDATE STEP #1;2;3;[02] UPON FURTHER INVESTIGATION CRACKED INTERCOSTAL ATTACH ANGLE IS LOCATED AT FCB BS500H FWD SIDE RBL25 WL155;[03] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BS500H FWD SIDE RBL25 WL155 IAW BOEING DWG143A7505 AND SRM 51-40-02;[04] VERIFIED CORRECTIVE ACTION 2 AND 3;[05] VERIFIED MEASUREMENT TABLE

Part: CHANNEL — CORRODED (ZN 200 FUS TOP) · airframe 37,857 hrs · 17,208 cycles

CORROSION ON ASD MOP SILL BS947 - BS991 RBL54 WL208.<[01] UPDATED STEP 1;[02] UPDATED STEP 2. ADDED ORIGINAL MATERIAL THICKNESS.;[03] REMOVED CORROSION FROM ASD MOP SILL BS947 - BS991 RBL54 WL208; FOUND TO BE WITHIN LIMITS PER SRM 53-70-15-1A-1; PAR. 4.D.(2). (A). FIG. 103; DETAIL D.

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500I S-21L WL177. MARKED<[01] UPDATED STEPS 1-2.;[02] UPDATED MEASUREMENT TABLE.;[03] UPDATED STEP 3.;[04] UPDATED STEP 4.;[05] UPDATED STEP 3.;[06] UPDATED STEP 3;[07] UPDATED STEP 2.;[08] UPDATED STEP 5.;[09] EDITED MEASUREMENT TABLE;[10] FCB AFT BULKHEAD SUPPORT GUSSET AT BS500I S-21L WL177; NO ALLOWED DAMAGE FOUND AND WAS REPLACED PER SRM 51-10-02-0G-0; NEW GUSSET P/N 143A9481-9 PO # 857169/4; IAW SRM 51-40-05-0G-0 AND DWG. 143A7902.;[11] VERIFIED CORRECTIVE ACTION 10

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500I AFT SIDE RBL25 WL155.<[01] UPON FURTHER INVESTIGATION CRACKED INTERCOSTAL ATTACH ANGLE WAS FOUND TO BE AT BS 500H AFT SIDE RBL 25 WL 155.;[02] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BS500H AFT SIDE RBL25 WL155 IAW BOEING DWG143A7505 AND SRM 51-40-02.;[03] VERIFIED CORRECTIVE ACTION 2;[04] VERIFIED MEASUREMENT TABLE

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500G FWD SIDE RBL25 WL155.<[01] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BS500G FWD SIDE RBL25 WL155 IAW BOEING DWG143A7505 AND SRM 51-40-02;[02] WORK WAS ACCOMPLISHED ON CUSTOMER CARD #TTG8Q00NFNQX;[03] VERIFIED JOB COMPLETE;[04] VERIFIED MEASUREMENT TABLE

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT BS500B+11 - BS500E; BS500G - BS500H RBL23 WL156.<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF FCB FLOOR TO SIDEWALL SUPPORT BS 500B+11-BS 500E;BS 500G-500H RBL 23 WL 156 IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[02] UPDATE STEP#1-4;[03] REMOVED FCB FLOOR TO SIDEWALL SUPPORT BS500A - BS500I RBL23 WL156 IAW SRM 51-40-02;[04] FABRIACATED LOCATED AND DRILLED FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT RBL 23 WL 156 MATERIAL USED BAC 1496-444#7075T62 LOT#509343-1 AND SPLICE BETWEEN BS 500'E' TO 500 'F'RBL 23 WL 156 MATERIAL USED BAC1496-444#7075T62 LOT#509343-1 IAW SRM 51-40-05 SRM 53-00-53-2R-6 REPAIR 6 AND DWG 143A7501 REV:- APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01;OK PRIMER;[05] UPDATE STEP 5-6;[06] UPDATE STEP#7-8;[07] UPDATE STEP 5.;[08] CORRECTION TO STEP 5.;[09] UPDATE STEP 5.;[10] COMPLETED STEP 5.;[11] TASK COMPLETE:<BR>REMOVED FLOOR TO SIDEWALL IAW SRM 51-40-02. FABRICATED; LOCATED; AND DRILLED NEW FLOOR TO SIDEWALL IAW SRM 51-40-05; SRM 53-00-53-2R-6 REPAIR 6; AND DWG 143A7501. APPLIED SURFACE TREATMENT IAW SRM 51-20-01 AND AMM 51-21-72-370-804. INSTALLED NEW FLOOR TO SIDEWALL SUPPORT IAW DWG 143A7505; DWG 143A7500; AND SRM 51-40-02-0G-0.;[12] VERIFIED RII STEPS COMPLETE;[13] VERIFIED JOB COMPLETE<BR><BR>VERIFIED MEASUREMENT TABLE

Part: ATTACH ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 37,857 hrs · 17,208 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500E FWD SIDE RBL25 WL155.<[01] UPON FURTHER INVESTIGATION INTERCOSTAL ATTACH ANGLE AT FCB BS500E FWD SIDE RBL25 WL155 FOUND NOT TO BE CRACKED. CLEANED AREA IAW SOPM 20-30-03;[02] VERIFIED JOB COMPLETE;[03] RII STEP ENTERED IN ERROR;[04] VERIFIED JOB COMPLETE<BR><BR>VERIFIED MEASUREMENT TABLE

Part: ATTACH ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 37,857 hrs · 17,208 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500I AFT SIDE LBL25 WL155.<[01] REMOVED AND REPLACED NEW ATTACH ANGEL IAW SRM 51-40-02-0G-0 AND DWG 143A7505 ID:0109 REV:-;[02] VERIFIED STEPS 1;2;3; COMPLETE AND MEASUREMENT TABLE; CARD COMPLETE.

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500I S-19R WL193. MARKED<[01] UPDATED STEP 1;[02] UPDATED STEP 2;[03] UPDATED MEASUREMENT TABLE.;[04] UPDATED STEPS 4-5.;[05] UPDATED STEP 2.;[06] UPDATED STEP 3.;[07] UPDATED STEP 6;[08] EDITED MEASUREMENT TABLE;[09] FCB AFT BULKHEAD SUPPORT GUSSET AT BS500I S-19R WL193; NO ALLOWED DAMAGE FOUND AND WAS REPLACED PER SRM 51-10-02-0G-0; NEW GUSSET P/N 143A9481-5 PO # 913599/4; IAW SRM 51-40-05-0G-0 AND DWG. 143A7902.;[10] VERIFIED CORRECTIVE ACTION 9

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500G AFT SIDE RBL25 WL155.<[01] UPDATED STEP#1;2;3;[02] UPON FURTHER INVESTIGATION CRACKED INTERCOSTAL ATTACH ANGLE IS LOCATED AT FCB BS500G FWD SIDE RBL25 WL155;[03] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BS500G FWD SIDE RBL25 WL155 IAW BOEING DWG143A7505 AND SRM 51-40-02;[04] VERIFIED JOB COMPLETE;[05] VERIFIED MEASUREMENT TABLE

Part: CHANNEL — CORRODED (ZN 200 FUS TOP) · airframe 37,857 hrs · 17,208 cycles

CORROSION ON AED MOP SILL BS947+4 LBL54 WL208.<[01] UPDATED STEP 1;[02] UPDATED STEP 2. ADDED ORIGINAL MATERIAL THICKNESS.;[03] REMOVED CORROSION FROM AED MOP SILL BS947+4 LBL54 WL208 FOUND TO BE WITHIN LIMITS PER RM 53-70-15-1A-1; PAR. 4.D.(2). (A). FIG. 103; DETAIL D.

Part: FLAP — DELAMINATED (ZN 600 RIGHT WIN) · airframe 37,857 hrs · 17,208 cycles

R/H OUTBOARD AFT FLAP LOWER SKIN IS DELAMINATED AT THE I/B EDGE. (MARKED)<[01] VERIFIED STEP 2 IN PARTIAL.;[02] REMOVED AND REINSTALLED R/H O/B AFT FLAP IAW AMM27-51-22-400-801.;[03] REMOVED AND REPLACED R/W O/B AFT FLAP IAW AMM 27-51-22;[04] COMPLETED MEASUREMENT TABLE;[05] CUSTOMER CARD COMPLETE

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500I FWD SIDE LBL25 WL155.<[01] RECEIVED NEW ATTACH ANGLE<BR>ITEM# : 143A7502U159<BR>PO# : 938941/1<BR><BR>REMOVED AND REPLACED NEW ATTACH ANGEL IAW SRM 51-40-02-0G-0 AND DWG 143A7505 ID:0109 REV:-;[02] VERIFIED STEPS 1;2;3; COMPLETE AND MEASUREMENT TABLE; CARD COMPLETE.

Part: HOLDER — BROKEN (ZN 200 FUS TOP) · airframe 37,857 hrs · 17,208 cycles

PANEL 843CZ AFT RH EMERGENCY ESCAPE HATCH ASSIST STRAP HOLDER IS BROKEN<[01] REMOVED AND REPLACED AFT RH EMERGENCY ESCAPE HATCH ASSIST STRAP HOLDER IAW SOPM 20-50-01;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE

Part: PANEL — CORRODED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

FORWARD CARGO DOOR PANEL 821BR HAS CORROSION ON EXTERIOR SURFACE.<[01] REMOVED CORROSION DAMAGE IN A 3.9L X 3.2W AREA; AND 9 DAMAGE FASTENERS; EVALUATED BLEND AREA AND FOUND THE BLEND 0.024 OF 0.040 TO BE (OUT OF LIMITS). REPAIR BY REPLACEMENT. RECEIVED NEW PART; INSTALLATION WILL BE COMPLETED ON TTG8Q00MPDDA.;[02] CORRECTION TO LINE 1:REMOVED CORROSION DAMAGE IN A 3.9L X 3.2W AREA; AND 9 DAMAGE FASTENERS; EVALUATED BLEND AREA AND FOUND THE BLEND 0.024 OF 0.040 TO BE (OUT OF LIMITS). REPAIR BY REPLACEMENT. RECEIVED NEW PART; INSTALLATION WILL BE COMPLETED ON TTG8Q00MPDDA. IAW SRM 52-30-01-1A-1; SRM 51-10-02; SRM 51-40-02.;[03] VERIFIED CORRECTIVE ACTION 2<BR>VERIFIED MEASUREMENTS TABLE.<BR>JOB COMPLETE.

Part: ATTACH ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 37,857 hrs · 17,208 cycles

RH WING; O/B UPPER FIXED TRAILING EDGE PANEL; O/B ATTACH ANGLE IS CRACKED O/B TRANSVERSE WEB ATTACH ANGLE CRACKED<[01] REMOVED AND REPLACED RH WING O/B UPPER FIXED T/E PANEL O/B ATTACH ANGLE IAW SRM 51-40-02-0G-0 PARA. 4.;[02] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED MEASUREMENTS TABLE AND TASK CARD COMPLETE.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 37,857 hrs · 17,208 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] UPDATED STEP 10;[02] SCUFF PLATE WAS FOUND CRACKED UPON REMOVAL. IT WAS SENT OUT FOR REPAIR. RECEIVED REPAIRED PART AND REINSTALLED IAW AMM 53-11-02; SOPM 20-50-19; SRM 53-30-15-2R-1; SRM 51-20-01; SOPM 20-20-02. SOPM 20-30-02.;[03] REJECTION REF [TTG8Q00NYPFV];[04] CORRECTION TO LINE 2: SCUFF PLATE WAS FOUND CRACKED UPON REMOVAL. IT WAS SENT OUT FOR REPAIR. RECEIVED REPAIRED PART AND REINSTALLED IAW AMM 53-11-02 (F)2); SOPM 20-50-19; SRM 53-30-15-2R-1 B.(6)-(13); SRM 51-20-01; SOPM 20-20-02. SOPM 20-30-02.;[05] REJECTED SEE: TTG8Q00NZFG6;[06] VERIFIED CORRECTIVE ACTION 3;4;5<BR>VERIFIED MEASUREMENTS TABLE.<BR>JOB COMPLETE.

Part: SLAT — DEBONDED (ZN 500 LEFT WING) · airframe 37,857 hrs · 17,208 cycles

#1 SLAT LOWER O/B SURFACE IS DISBONDED; (MARKED)<[01] REPAIRED AND REINSTALLED SLAT IAW AMM 27-81-21-400-801 AND CSD WORK ORDER #563768;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.

Part: FITTING — CRACKED (ZN 600 RIGHT WIN) · airframe 37,857 hrs · 17,208 cycles

PANEL 621GB O/B CTR LATCH FITTING IS BROKEN<[01] REMOVED AND REPLACED PANEL 621GB O/B CTR LATCH FITTING PER AMM 20-50-11910-801 <BR>CAL TOOL: ATS1731 DUE: 07/2024;[02] UPDATED PARTS;[03] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.

Part: PANEL — DELAMINATED (ZN 500 LEFT WING) · airframe 37,857 hrs · 17,208 cycles

LEFT WING L/E PANEL 521KB DELAMINATED AT CUTOUT CORNERS<[01] LEFT WING L/E PANEL 521KB WAS DELAMINATED AT CUTOUT CORNERS AND REPAIRED IAW SRM 51-70-05-2R-6. FINAL FINSIH WILL BE ACCOMPLISHED ON FAULT: TTG8Q00NQTZ;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLASHLIGHT — FAILED (ZN 200 FUS TOP) · airframe 36,150 hrs · 16,292 cycles

CREW REPORTS: LED NOT FLASHING ON FLASHLIGHT IN AFT GALLEY<[01] REPLACED BATTERY. ALL GOOD. REF AMM 25-64-00

Part: LIGHT — OUT OF ADJUST (CABIN) · airframe 35,732 hrs · 16,068 cycles

EMERGENCY PATH AISLE LIGHTING STRIP(AIRCRAFT RIGHT) LOOSE AT ROW 12<[01] INSTALLED NEW CARPET. TAPE AS REQUIRED PER S.I.P

Part: NONE — LOOSE (CABIN FLOOR) · airframe 34,732 hrs · 15,514 cycles

ROW 11DEF FLOOR EGRESS LIGHT STRIP LOOSE / [01] SECURED FLOOR EGRESS LIGHTS IAW AMM 33-51-15

Part: LENS — LOOSE (MID CABIN) · airframe 34,199 hrs · 15,222 cycles

MID CABIN OVERHEAD EMERGENCY EXIT SIGN BASE COVER FELL OFF EXIT SIGN LENS AND FU MID CABIN OVERHEAD EMERGENCY EXIT SIGN BASE COVER FELL OFF EXIT SIGN LENS AND FUNCTION NORMAL.MX... IF UNABLE TO FIX PLEASE GET PN SO WE CAN ORDER WHAT IS REQUIRED TO FIX THIS... / [01] RESECURED PER SIP

Part: SEAL — CRACKED (RH HOR STAB) · airframe 33,746 hrs · 14,988 cycles

RH HORIZONTAL STABILIZER UPPER SLIDING SEAL IS CRACKED / [01] R&R RH HORIZONTAL STABILIZER UPPER SLIDING SEAL PER AMM 53-31-31.

Part: SEAL — CRACKED (LH HOR STAB) · airframe 33,746 hrs · 14,988 cycles

LH HORIZONTAL STABILIZER UPPER SLIDING SEAL IS CRACKED / [01] R&R LH HORIZONTAL STABILIZER UPPER SLIDING SEAL PER MM REF 53-31-31

Part: LIGHT — INOPERATIVE · airframe 33,156 hrs · 14,661 cycles

R/H AFT OVER WING EMERGENCY LIGHT INOP. / [01] RELAMPED R/H AFT OVER WING EMERGENCY EXIT LIGHT & OPS CHECK GOOD REF AMM 33-51-04

Part: LIGHT — LOOSE (CABIN) · airframe 32,405 hrs · 14,305 cycles

EMERGENCY LIGHTING STRIP ON FLOOR-ROW 11 CAPTAIN\LEFT SIDE IS LOOSE ; / [01] RESECURED PER SIP

Part: BATTERY — POPPED (CABIN) · airframe 32,089 hrs · 14,155 cycles

ON PREFLIGHT CIRCUIT BREAKER P18-3 A-10 POPPED.(LIGHTING EMER CHGR L-AFT) ; / [01] REPLACED BATTERY PACK AND CHARGER ASSY PER AMM 33-51-06.

Part: CHARGER — POPPED (CABIN) · airframe 32,089 hrs · 14,155 cycles

ON PREFLIGHT CIRCUIT BREAKER P18-3 A-10 POPPED.(LIGHTING EMER CHGR L-AFT) ; / [01] REPLACED BATTERY PACK AND CHARGER ASSY PER AMM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 32,026 hrs · 14,124 cycles

RT SIDE EMERGENCY EXIT ROW SIGNS INOP ; / [01] R&R EMERGENCY LIGHT BATTERY PACK AT STATION 565RT. OPS CK GOOD. PER AMM 33-51-06

Part: RIB — CRACKED (LH WING)

WEB I/B OF L/H WING DEFLECTION CONTROL RIB IS CRACKED. / REMOVED AND REPLACED WEB PER SRM 51-40-02SA-M 326 A1362027INSP D142

Part: BATTERY PACK — INOPERATIVE (CABIN)

FWD EMER LIGHTS OFF M 1675 BATTERY PACK INOP / REMOVED & REPLACED EMER EXIT LT BATTERY PACK M 1675 PER AMM 33-51-06. TEST GOOD.

Part: RIB — CRACKED (RH WING)

R/H WING T/E DEFLECTION CONTROL RIB I/B SUPPORT ANGLE FOR UPPER SHELF PANEL IS CRACKED ; MRKD / REMOVED AND REPLACED ANGLE PER SRM 51-40-02.

Part: NONE — CRACKED (RH WING)

R/H WING T/E WAFFLE PLATE CRACKED AT RIVET HOLE APPROX. IRSS 220. MRKD / REMOVED AND REPLACED WAFFLE PLATE PER SRM 51-10-02; INSTALLED FASTENERS PER SRM 51-40-02

Part: STRUCTURE — CRACKED (POWER DOOR) · airframe 13,671 hrs · 30,931 cycles

EXTERNAL POWER DOOR LOWER CORNER CRACKED / C/W NDT OF CUTOUT AREA IAW 737 NDT PART 6; 51-00-00 PROD 23 NO DEFECT NOTED E75437 REPAIRED PER SRM 53-10-15-2E-4 REPAIR 4 ALTERNATIVE 2

Part: MEGAPHONE — WEAK (FWD CABIN) · airframe 13,655 hrs · 30,900 cycles

MEGA PHONE VOLUME WEAK / REPLACED FWD MEGAPHONE. AMM 25-64-00.

Part: SKIN — DELAMINATED (RT WING TE FLAP)

LEFT WING PTBD AFT FLAP LOWER SURFACE HAS A LARGE DELAMINATION AT INBD AREA. DELAM MEASURES 14' X 11' / R&R L/H O/B T/E AFT FLAP PER AMM 27-51-22 PN OFF/ON 113A700-25 SN OFF 004056 SN ON 00525AMT 11543 INSP 10886

Part: SIGN — LOOSE (OVERWING) · airframe 13,572 hrs · 30,727 cycles

EXIT SIGN ON FWD OW EXIT; CAPTAINS SIDE CAME OFF. / INSTALLED NEW EXIT SIGN PER AMM 33-51-01

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 30,663 hrs · 13,532 cycles

FOUND C/B TRIPPED - LIGHTING EMER CHGR LEFT AFT / RESET LIGHTING EMERGENCY CHARGER LEFT AFT C/B IAW AMM 20-60-01. OPS CHK EMERGENCY LIGHTS C/B STAYED IN. IAW AMM 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,577 hrs · 13,485 cycles

LH AFT EMERGENCY EXIT LIGHT; LH SLIDE OVERWING FUSELAFE LIGHT; AND AFT ENTRY EMERGENCY LIGHT INOP. / REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACKS AT LH OVERWING AND LH AFT CEILING REF AMM 33-51-06. OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 30,520 hrs · 13,458 cycles

FWD GALLEY EMERGENCY MEGAPHONE WORK INTERMITTENTLY. REPLACED MEGAPHONE BATTERIES (FWD) PER M.M. CH. 256400. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,928 hrs · 13,179 cycles

EXTERIOR EMER. EXIT LIGHT AFT OF R2 DOOR INOP. / RELAMPED IAW AMM 33-51-04. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,576 hrs · 13,045 cycles

LT FORWARD EMERGENCY EXIT EXTERNAL LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED LT FORWARD EMERGENCY LIGHT BATTERY PACK, REFERENCE AMM 33-51-06. OPERATIONS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,003 hrs · 12,781 cycles

RT OVERWING EMERGENCY EXIT & CENTER ISLE EMERGENCY EXIT LIGHTS ARE INOPERABLE. R & R BATTERY PACK & BATTERY PACK CHARGER, PER AMM 33-51-06 AND WDM 33-51-11. OPERATIONS CHECK NORMAL (M1695).

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,003 hrs · 12,781 cycles

RT OVERWING EMERGENCY EXIT & CENTER ISLE EMERGENCY EXIT LIGHTS ARE INOPERABLE. R & R BATTERY PACK & BATTERY PACK CHARGER, PER AMM 33-51-06 AND WDM 33-51-11. OPERATIONS CHECK NORMAL (M1695).

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,779 hrs · 12,015 cycles

R1 DOOR EMERGENCY LIGHTS INOP / REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 27,494 hrs · 11,885 cycles

CENTER RIGHT FLOOR SUPPORT INTERCOSTAL IS CRACKED AT STA 540 IN FWD CARGO A/C DISTRIBUTION BAY / REMOVED AND REPLACED CENTER RIGHT FLOOR SUPPORT AT STATION 540 PER SRM 51-40-02 AND AMM 53-21-00

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 27,202 hrs · 11,716 cycles

CENTER RIGHT FLOOR SUPPORT INTERCOSTAL CRACKED AT BS. 540 IN FORWARD CARGO A/C DISTRIBUTION BAY. / R&R INTERCOSTAL PER SRM AND AMM.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 27,494 hrs · 11,885 cycles

CENTER LEFT FLOOR SUPPORT INTERCOSTALS ARE CRACKED AT STA 540 IN FWD CARGO A/C DISTRIBUTION BY / REMOVED AND REPLACED CENTER LEFT FLOOR SUPPORT INTECOSTAL AT STATION 540 PER SRM 51-40-02 AND AMM 53-21-00.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 27,202 hrs · 11,716 cycles

CENTER LEFT FLOOR SUPPORT INTERCOSTAL WAS CRACKED AT BS. 540 IN FORWARD CARGO. / R&R INTERCOSTAL PER SRM AND AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,185 hrs · 11,709 cycles

RIGHT EMERGENCY EXIT GROUND ILLUMINATION LIGHT INOP. R & R THE BATTERY PACK M1671 IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EXTERIOR LIGHT) · airframe 27,185 hrs · 11,709 cycles

EXTERIOR AFT OVERWING HATCH LIGHT AT R/H AFT HATCH INOPERATIVE. R & R THE BATTERY PACK M1671 IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,185 hrs · 11,709 cycles

EMERGENCY EXIT LIGHTS AT AFT OF R/H AFT OVERWING EXIT INOP. R&R BATTERY PACK M1671 PER AMM.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 26,804 hrs · 11,527 cycles

L2 DOOR EXIT SIGN COVER NEAR AFT BOARDING DOCK FELL OFF. / R&R COVER PER AMM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 26,514 hrs · 11,392 cycles

FORWARD INBOARD EMERGENCY FLASHLIGHT DID NOT WORK. / R&R BATTERY IAW MM.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 26,333 hrs · 11,289 cycles

L/H EMERGENCY OVERWING ESCAPE GROUND ILLUMINATION LIGHT L547 INOP AT BS. 727F+11. / RESEATED CONNECTOR D11082 IAW WDM, SWPM, AND AMM.

Part: SCUFF PLATE — CORRODED (AFT CARGO THRESH) · airframe 26,512 hrs · 11,391 cycles

AFT CARGO COMPARTMENT UPPER AFT SCUFF PLATE CORRODED ON BOTTOM SIDE / VERIFIED AND REPLACED AFT CARGO COMPARTMENT UPPER AF SCUFF PLATE IAW AIPC 25-52-10-04. P/N 453A2611-2 ATAG A20769. INSTALLED AFT SCUFF PLATE TIE DOWN IAW AMM 25-52-10-400-801.

Part: SCUFF PLATE — CORRODED (AFT CARGO THRESH) · airframe 26,512 hrs · 11,391 cycles

AFT CARGO COMPARTMENT UPPER FWD SCUFF PLATE CORRODED ON BOTTOM SIDE / VERIFIED AND REPLACED AFT CARGO COMPARTMENT UPPER FWD SCUFF PLATE IAW AIPC 25-52-10-04. P/N 453A2611-1 ATAG 50601. INSTALLED FWD SCUFF PLATE TIE DOWN IAW AMM 25-52-00-400-801.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 26,512 hrs · 11,391 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED (P/N 146A9401-18); STATION 727D + 5.6; LBL 20 - RBL 20 / REMOVED CORROSION. NO LIMITS FOUND; REPAIRED BY REPLACEMENT I/A/W B737 SRM 51-10-02-0G-0; BOEING PL 146A9401-18 REV D.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 26,512 hrs · 11,391 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED (P/N 146A9401-16); STATION 767 + 6; LBL 20-RBL 20; WL 156. / REMOVED CORROSION; NO LIMITS FOUND; REPAIRED BY REPLACEMENT I/A/W B737 SRM 51-10-02-0G-0. BOEING PL 146A9401 REV D

Part: FLOORBEAM — CORRODED (BS 727D) · airframe 26,333 hrs · 11,289 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS. 727D+ 5.6, BETWEEN LBL 20 TO RBL 20. / R&R SUPPORT IAW SRM.

Part: WEB — CORRODED (AFT CARGO THRESH) · airframe 26,512 hrs · 11,391 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE DOOR CUTOUT WEB AT STA 787+7' TO 847 RBL 26 WL156 CORRODED / REMOVED CORROSION ON AFT CARGO COMPARTMENT FLOOR STRUCTURE DOOR CUT OUT WEB STA 787+7' TO 847 RBL 26 WL156 IAW SRM 51-10-02-0G-0. VERIFIED LIMITS IAW SRM 53-60-15-1A-1. ORIGINAL THICKNESS 0.050'; REMAINING THICKNES 0.016'; LOSS OF 0.034' FOUND TO BE OUT OF LIMITS. REMOVED; VERFIRIED; AND REPLACED AFT CARGO DOOR LOWER SILL WEB IAW PL 146A8123 PART # 146A8123-6 ATAG CC3287; DWG 146A8123 SHEET 6 REV C; DWG 146A8340 SHEET 21 REV-; SRM 51-40-05-0G-0; SRM 51-40-02-0G-0. APPLIED CIC IAW AMM 51-21-91-620-802. AAR 36306 DUE 06/26/20

Part: SIGN — BROKEN (CABIN) · airframe 26,333 hrs · 11,289 cycles

PASSENGER CABIN SIDEWALL PANEL 232ZLW HAD BROKEN EMERGENCY EXIT SIGN. / R&R SIGN IAW SRM.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 26,333 hrs · 11,289 cycles

AFT L/H EMERGENCY FLASHLIGHT HOLDER BROKEN. / R&R HOLDER IAW CMM.

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 26,512 hrs · 11,391 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE NUTPLATE STRIP ON BOTTOM SIDE 787+7' RBL 20 WL 156 CORRODED / REMOVED CORROSION ON NUT PLATE STRIP ON BOTTOM SIDE STA 787+7' RBL 20 NO PUBLISHED LIMITS REMOVED AND FABRICATED NEW NUT PLATE STRIP IAW SRM 51-40-02 SRM 51-40-05 AND DWG 146A8128 SHT 9 REV - INSTALLED STRIP IAW SRM 51-40-02 AND DWG 146A8128 REV -

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 26,512 hrs · 11,391 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE Z ANGLE CORRODED AT STA 727G TO 787+12' LBL 22 WL 156 / REMOVED CORROSION ON AFT CARGO Z ANGLE FROM STAITON 727G+12 TO 787+12 LBL 22 SL 156; STA 727G TO 747+1- FOUND WITHIN ALLOWABLE LIMITS WITH .038' MAT REMAINING; .040' ORIGINAL AND .10T MAX ALLOWABLE LOSS; STA 747+10 TO 787+12 FOUND OUT OF ALLOWABLE LIMITS WITH .022' MAX REMAINING; .040' ORIGINAL MAT AND .10T MAX ALLOWABLE LOSS; REPAIRED Z ANGLE FROM STA 747+10 TO 787+12 REF B737 SRM 53-00-53-1A-2; 53-00-53-2R-5 P/N 146A7502-9

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 26,512 hrs · 11,391 cycles

FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE CRACKED / RECIEVER NEW FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE; P/N 143A8331-3; TO BE INSTALLED ON CUSTOMER ORDER/CARD 753-140-00-01Y WO: 578708 A TAG CC3281

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 26,512 hrs · 11,391 cycles

FORWARD CARGO PIT FLOOR PANEL 120AF HAS CORROSION ON UPPER SURFACE ALONG FORWARD EDGE / RECEIVED NEW PANEL FOR FWD CARGO PIT PANEL 120AF MATERIAL ID FOR PANEL 120AF IS 453A1610 IAW BOEING DWG 453A1610 REV-F AND IPC 25-52-10-17 A TAG WN4251

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 26,512 hrs · 11,391 cycles

FORWARD CARGO PIT FLOOR PANEL 120DF HAS CORROSION ON UPPER SURFACE ALONG SIDE EDGES / RECEIVED NEW PANEL FOR FWD CARGO PIT PANEL 120DF PART #ID IS 453A1610-20 IAW BOEING DWG 453A1610 REV-F AND IPC 25-52-10-17 A TAG WN1835

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 26,512 hrs · 11,391 cycles

FORWARD CARGO PIT FLOOR PANEL 120CF HAS CORROSION ON UPPER SURFACE ALONG SIDE EDGES / RECEIVED NEW PANEL FOR FWD CARGO PANEL 120CF PART # ID IS 120AF IS 453A1610-103 IAW BOEING DWG 453A1610 REV:- AND IPC 25-52-10-17 A TAG WN2680

Part: LIGHT — BROKEN (CABIN) · airframe 26,333 hrs · 11,289 cycles

PASSENGER CABIN G-4 GALLEY R/H EMERGENCY EXIT LIGHT BROKEN. / R&R LIGHT IAW AMM.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,957 hrs · 11,135 cycles

R/H SIDE AFT OVERWING EMERGENCY EXIT SIGN INOP. R&R EMERGENCY EXIT SIGN ASSEMBLY PER MM.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 25,578 hrs · 10,946 cycles

R/H HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL CRACKED / R&R R/H HORIZONTAL STAB. UPPER FWD SLIDING SEAL REF AMM 53-31-31.AMT 67662INSP 43450

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 25,578 hrs · 10,946 cycles

L/H HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL CRACKED / R& L/H HORIZONTAL STAB. UPPER FWD SLIDING SEAL REF AMM 53-31-31.AMT 67662INSP 43450

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 24,749 hrs · 10,527 cycles

AFT GALLEY OUTBOARD EMERGENCY FLASHLIGHTS DID NOT BLINK. R&R BATTERY PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 234,210 hrs · 9,915 cycles

R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 22,157 hrs · 9,372 cycles

EMERGENCY LIGHT BATTERY M1672 FAILED TEST. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 22,157 hrs · 9,372 cycles

EMERGENCY LIGHT BATTERY M1673 FAILED TEST. R&R BATTERY PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 22,266 hrs · 9,423 cycles

CABIN RT AFT EMERGENCY FLASHLIGHTS INOP. R&R FLASHLIGHT PER AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 21,493 hrs · 9,075 cycles

LEFT EMERGENCY EXIT LIGHT LENS MISSING AT ROW 27. INSTALLED THE LENS IAW MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 208,700 hrs · 8,794 cycles

AFT FLASH LIGHT STRAP BROKEN. R&R STRAP PER AMM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 20,565 hrs · 8,643 cycles

RT SIDE OVERWING EMERGENCY "EXIT" SIGN LENS FELL OFF. INSTALLED LENS PER SIP.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 20,242 hrs · 8,499 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 20,036 hrs · 8,410 cycles

SUPPLEMENTAL INFORMATION: ***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT STA 727G-847; LBL20; WL155 / REMOVED DAMAGE ON STA727G; LBL20(1'X2') .030' DEEP FOUND TO BE OUT OF LIMITS PER SRM-53-00-53-1A-2; REMOVED SIDEWALL SUPPORT FROM STA 727F+8 TO BS787+6; LBL 20. IAW-SRM-53-00-53-2R-5; LOCATED AND DRILLED REPLACEMENT SIDEWALL FLOOR SUPPORT SRM-53-00-53-2R-5; TREATED AND PRIMED REPAIR PARTS PER SRM-51-20-01; INSTALLED NUT PLATES PER SRM-51-40-10-2R-0; INSTALLED SIDEWALL SUPPORT ON BS757+6; 727F+8 IAW SRM-53-00-53-2R-5; DWG. 146A7500

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 20,036 hrs · 8,410 cycles

***CORROSION*** ON AFT CARGO BAY SIDE SHIELD STA 767-787; RBL20; WL155 / REMOVED CORRODED SHIELD AT STA 767-787 RBL20 L/L 155; AFT CARGO BAY; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM; IAW SRM 51-40-02-0G-0; INSTALLED NEW SHIELD P/N 146A8127-12 IAW SRM 51-40-02-0G-0 & DWG# 146A0081 81146U 10/31/17

Part: BAFFLE — CRACKED (FWD CARGO LH) · airframe 20,036 hrs · 8,410 cycles

FORWARD CARGO. BAFFLE CRACKED AT BS 500A +19 LBL 25 / REMOVED CRACKED BAFFLE AT BS 500A+19; LBL 25 IAW SRM 51-40-02-0G-0. INSTALLED NEW BAFFLE; PO# 1055865 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7510

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 20,036 hrs · 8,410 cycles

SUPPLEMENTAL INFORMATION: ***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT STA 727G-767; RBL20; WL155 / REMOVED DAMAGE FROM SIDEWALL SUPPORT BS727G; RBL 70 1X2X.025' DEEP TO BE OUT OF LIMITS; IAW SRM 53-00-53-1A-2; REMOVED SIDEWALL SUPPORT PORTION FROM STA 727E+6 TO STA 767; RBL20; IAW SRM-53-00-53-2R-5; LOCATED AND DRILLED REPLACEMENT FLOOR SIDEWALL SUPPORT IAW-SRM-53-00-53-2R-5. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-20-01; INSTALLED NUT PLATES IAW-SRM-51-10-10-2R-0; ON SIDEWALL SUPPORT;

Part: SIDEWALL SUPPORT — CORRODED (BS 727G-847) · airframe 19,301 hrs · 8,067 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727G TO 847, LBL 20. REPAIRED THE SIDEWALL SUPPORT IAW SRM & DWG.

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 20,036 hrs · 8,410 cycles

***CORROSION*** ON AFT CARGO BAY SIDE SHIELD STA 847-867; RBL20; WL162 / REMOVED CORRODED SHIELD AT STA 847-867 RBL 20 WL162 IAW SRM 31-40-02-0G-0; FOUND TO BE OUT OF LIMITS DUE TOO NO LIMITS IN SRM; LOCATED & DRILLED NEW SHIELD P/N 146A8127-10 IAW SRM 51-40-05-0G-0; INSTALLED SHIELD IAW SRM 51-40-02-0G-0 & DWG #146A0081 81146U 11/1/17

Part: BAFFLE — CRACKED (FWD CARGO RH) · airframe 20,036 hrs · 8,410 cycles

FORWARD CARGO. BAFFLE CRACKED AT BS 500C +8 RBL 25 / REMOVED CRACKED BAFFLE AT BS 500C RBL 25 IAW SRM 51-40-02-0G-0; INSTALLED NEW BAFFLE P/N 143A7510-24 IAW SRM 51-40-02-0G-0 & DWG # 143A7510 81146U 11/2/17

Part: SHIELD — CORRODED (BS 847-867) · airframe 19,301 hrs · 8,067 cycles

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

Part: SHIELD — CORRODED (BS 767-787) · airframe 19,301 hrs · 8,067 cycles

AFT CARGO BAY SIDE SHIELD CORRODED BETWEEN BS 767 TO 787, RBL 20. R & R THE SHIELD IAW SRM & DWG.

Part: TRANSITION PANEL — CORRODED (FWD CARGO BAY) · airframe 20,036 hrs · 8,410 cycles

FWD CARGO BS 500A+11 TO BS 500 I LBL 22 TRANSITION PANEL IS CORRODED AROUND NUT PLATES. / EVALUATED CORROSION ON LBL22 FWD CARGO TRANSITION PANEL; FOUND TO BE OUT OF LIMIST PER SRM-53-00-53-1A-2; REMOVED SECTION OF THE TRANSITION PANEL FROM STA 500A+11 TO BS 500I; IAW-SRM-53-00-53-2R-5; LOCATED AND DRILLED NEW REPLACEMENT SECTION OF TRANSITION PANEL; IAW-SRM-53-00-53-2R-5/DWG 143A7501; TREAT AND PRIME REPAIR PARTS SRM-51-20-01; INSTALLED NEW SECTION OF TRANSTION PANEL 500A+11-500I IAW SRM-53-00-53-2R-5 DWG. 143A7501

Part: TRANSITION PANEL — CORRODED (FWD CARGO BAY) · airframe 20,036 hrs · 8,410 cycles

FWD CARGO BS 500C+6 TO BS 500 I RBL 22 TRANSITION PANEL IS CORRODED AROUND NUT PLATES. / AFTER EVALUATION CORROSION RBL 22 FWD CARGO TRANSITION PANEL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 4A; REMOVED TRANSITION PANEL FROM BS5009 +8 TO 500I IAW SRM -51-40-02; FABRICATED NEW TRANSITION PANEL PER SRM 53-00-53-2R-5 TREATED AND PRIMED REPAIR PART PER SRM -51-21-41-370-802; AMM -51-21-72-370-804; INSTALLED REPAIR PARTS ON BS 500B+8 TO 500I PER-SRM-51-40-02-06-0; DWG. 143A7501

Part: ATTACH ANGLE — CORRODED (FWD CARGO BAY) · airframe 20,036 hrs · 8,410 cycles

FWD CARGO BS 500 I LBL 22 TO RBL 22 LOWER BULKHEAD ATTACH ANGEL IS CORRODED. / FIVE CORROSION SPOTS APPROX. 1' X 1' X .026' DEPTH FOUND TO BE OUT OF ALLOWABLE LIMITS. REMOVED CORRODED LWR RAIL ASSY AND INSTALLED NEW RAIL ASSY. SI# 7530142 IAW SRM 53-00-53-1A-2; 51-40-02; AND BOEING DWG 143A9481 57575U 11/03/17

Part: GUSSET — CRACKED (FWD CARGO RH) · airframe 20,036 hrs · 8,410 cycles

FWD CARGO GUSSET CRACKED RH STA500I STR 19 / REMOVED AND REPLACED CRACKED GUSSET AT STA 500I IAW SRM 57-40-42-0G-0 AND BOEING DWG 143A7902 SH171 RA11

Part: GUSSET — CRACKED (BS 500I) · airframe 19,301 hrs · 8,067 cycles

FORWARD CARGO GUSSET CRACKED AT BS 500I, STRINGER 19R. R & R THE GUSSET IAW SRM AND DWG.

Part: LENS — CRACKED (CABIN) · airframe 19,301 hrs · 8,067 cycles

RT CEILING EMERGENCY LIGHT LENS CRACKED AT ROW 14. R&R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 19,301 hrs · 8,067 cycles

LT CEILING EMERGENCY LIGHT LENS CRACKED AT BETWEEN ROW 9 TO ROW 12. R&R LENS IAW AMM.

Part: SIDEWALL SUPPORT — CORRODED (BS 727G-767) · airframe 19,301 hrs · 8,067 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727G TO 767, RBL 20. REPAIRED THE SUPPORT IAW SRM.

Part: ATTACH ANGLE — CORRODED (BS 500I) · airframe 19,301 hrs · 8,067 cycles

FORWARD CARGO LOWER BULKHEAD ATTACH ANGLE CORRODED AT BS 500I, BETWEEN LBL 22 TO RBL 22. R & R THE ATTACH ANGLE IAW SRM AND DWG.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 19,435 hrs · 8,127 cycles

RIGHT HORIZONTAL STABILIZER UPPER SLIDER SEAL CRACKED / REMOVED & REPLACED RIGHT HORIZONTAL STABILIZER UPPER SLIDER SEAL IAW M/M 53-31-31. INSPECTOR H55

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 19,435 hrs · 8,127 cycles

LEFT HORIZONTAL STABILIZER UPPER SLIDER SEAL CRACKED / REMOVED & REPLACED L/H HORIZONTAL UPPER SLIDER SEAL PER AMM 53-31-31. INSPECTOR H55

Part: ANGLE — CRACKED (LT WING) · airframe 19,122 hrs · 7,985 cycles

LEFT WING TRAILING EDGE PANEL ANGLE CRACKED. R & R THE ANGLE IAW SRM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,393 hrs · 7,670 cycles

CENTER AISLE EMERGENCY EXIT SIGN L1070 INOPERATIVE. R & R THE POWER SUPPLY IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,393 hrs · 7,670 cycles

CENTER AISLE EMERGENCY EXIT SIGN L1070 INOP. R&R BATTERY PACK PER MM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,047 hrs · 6,613 cycles

RIGHT EMERGENCY EXIT ROW AISLE LOCATOR LIGHT INOPERATIVE. R & R THE BATTERY CHARGER ASSEMBLY IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 15,281 hrs · 6,275 cycles

LT DOOR LOWER EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED EXIT COVER IAW SIP.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 13,693 hrs · 5,576 cycles

FORWARD FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 12,549 hrs · 5,085 cycles

LEFT OVERHEAD EMER LIGHT LENS CRACKED, BETWEEN ROW 15 - 23. REPAIRED LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 12,549 hrs · 5,085 cycles

RIGHT OVERHEAD EMER LIGHT LENS CRACKED, BETWEEN ROW 25 - 27. REPAIRED LENS IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 10,945 hrs · 4,438 cycles

L1 DOOR EXIT LIGHT COVER LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: SIGN — MISSING (CABIN) · airframe 10,627 hrs · 4,311 cycles

MID CABIN EXIT SIGN MISSING. INSTALLED SIGN IAW SIP.

Part: SIGN — LOOSE (CABIN) · airframe 10,586 hrs · 4,295 cycles

OVERWING EXIT SIGN LOOSE FROM CEILING. SECURED EXIT SIGN IAW MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 10,586 hrs · 4,295 cycles

OVERWING EXIT SIGN LOOSE INOPERATIVE. R & R POWER SUPPLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,623 hrs · 1,729 cycles

RT EMERGENCY LIGHT AT FWD EMERGENCY WINDOW INOPERATIVE. RELAMPED LIGHT IAW AMM.