N8697C

Part: LENS — BROKEN (ZONE 200) · airframe 29,706 hrs · 14,821 cycles

AFT SERVICE DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED AFT SERVICE DOOR EMERGENCY EXIT SIGN LENS PER AMM 33-51-01.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 29,706 hrs · 14,821 cycles

LT AND RT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED PER AMM 33-51-06-960-805-NG.

Part: STRAP — UNSECURE (ZONE 800) · airframe 29,706 hrs · 14,821 cycles

ESCAPE HATCH; LEFT SIDE PANEL 833 ESCAPE STRAP RED VELCRO COVER NOT ATTACHED TO DOOR SURROUND FRAME STRUCTURE. SECURED ESCAPE STRAP RED VELCRO COVER TO DOOR SURROUND FRAME STRUCTURE PER SOPM 20-50-12.

Part: STRAP — OUT OF ADJUST (ZONE 800) · airframe 29,706 hrs · 14,821 cycles

ESCAPE HATCH; RIGHT SIDE PANEL 843 ESCAPE STRAP RED VELCRO COVER NOT ATTACHED TO DOOR SURROUND FRAME STRUCTURE.<[01] SECURED ESCAPE STRAP RED VELCRO COVER TO DOOR SURROUND FRAME STRUCTURE PER SOPM 20-50-12.;[02] VERIFIED SECURED ESCAPE STRAP RED VELCRO COVER TO DOOR SURROUND FRAME STRUCTURE PER SOPM 20-50-12.

Part: BEZEL — BROKEN (ZONE 800) · airframe 29,706 hrs · 14,821 cycles

ESCAPE HATCH; LEFT SIDE PANEL 833 CLOSING STRAP BEZEL ATTACHED TO DOOR LINER IS BROKEN. SECURED CLOSING STRAP BEZEL TO THE LEFT OVERWING EXIT DOOR 833 PANEL PER SOPM 20-50-12.

Part: ANGLE — CRACKED (ZONE 400) · airframe 29,706 hrs · 14,821 cycles

NUMBER 1 ENGINE INBD FAN COWL ANGLE AT AFT SIDE OF OIL SERVICE DOOR OPENING CRACKED AT UPPER CORNER. REMOVED AND REPLACED THE NR 1 ENGINE INBD FAN COWL WEB AT OIL SERVICE DOOR IAW AMM 51-40-02.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 29,706 hrs · 14,821 cycles

CRACK FOUND AT BS 663, RBL 34, ON VAPOR BARRIER ATTACH ANGLE. REMOVED VERTICAL ATTACHED FASTENERS ON RT 663 CHORD IAW SRM 51-40-02. REMOVED FUEL TANK FASTENERS AT BS 663 ON VAPOR BARRIER ATTACH ANGLE RBL 6 TO RBL 43 IAW SRM 51-40-02. REMOVED AND REPLACED VAPOR BARRIER ATTACH ANGLE IAW SRM 51-40-02 AND EA 25-157-02319 AND EA 25-157-02305. REF DWG 111A1000. FUEL TANK FASTENERS IN CONJUNCTION WITH VAPOR BARRIER ATTACH ANGLE LEAK CHECKED IAW AMM 28-11-00. NO LEAKS NOTED.

Part: PLATE — CRACKED (ZONE 500) · airframe 29,706 hrs · 14,821 cycles

HFEC SHOWS EVIDENCE OF CRACK IN WIGGLE PLATE ON FWD INBD CORNER OF PANEL 551EB ATTACH POINT.<[01] HFEC WIGGLE PLATE PER NDT MANUAL 51-00-00 PROCEDURE 23;[02] REMOVED DAMAGED WIGGLE PLATE PER SRM 51-40-02.;[03] REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02.;[04] INSPECTED WORK PERFORMED REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02.

Part: SKIN — DELAMINATED (ZONE 500) · airframe 29,706 hrs · 14,821 cycles

LEFT WING OTBD AFT FLAP HAS LARGE AREA OF DELAMINATION ON UPPER SURFACE ON INBD CORNER. REMOVED LT WING OTBD AFT FLAP IAW AMM 27-51-22. INSTALLED LT WING OTBD AFT FLAP IAW AMM 27-51-22.

Part: LENS — MISSING (ZONE 200) · airframe 27,488 hrs · 13,638 cycles

BOTH AFT GALLEY EXIT SIGN LENSES MISSING<[01] REINSTALLED GALLEY EXIT SIGN LENSES IAW AMM 33-51-01

Part: SLIDE — DISLODGED (ZONE 800) · airframe 26,486 hrs · 13,079 cycles

L1 DOOR SLIDE IS COMING OUT OF ITS CASE<[01] REPOSITION L1 DOOR ESCAPE SLIDE IAW MT 725-61-06

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 26,284 hrs · 12,972 cycles

AFT LEFT EMERGENCY LIGHTS BATTERY PACK INOP. R&R BATTERY PACK PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 26,284 hrs · 12,972 cycles

FWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 500C L/H IS INOP. REMOVED AND REPLACED FWD CABIN EMERGENCY LIGHT POWER PACK AT STA 500C L/H PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 26,284 hrs · 12,972 cycles

AFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C L/H IS INOP. REMOVED AND REPLACED AFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C L/H PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 26,284 hrs · 12,972 cycles

FWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 500C R/H IS INOP. REMOVED AND. REPLACED FWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 500 R/H PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 26,284 hrs · 12,972 cycles

AFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C RT IS INOP. REMOVED AND REPLACED AFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C R/H PER AMM 3-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

PASSENGER CABIN FLOOR PANEL SUPPORT CRACKED ATTACH FASTENER STA. 540; LBL 2.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

PASSENGER CABIN FLOOR PANEL SUPPORT CRACKED ATTACH FASTENER STA. 540; RBL 2.<[01] REMOVED AND REPLACED PER SRM 51-40-02.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 26,279 hrs · 12,968 cycles

FLOOR STRUCTURE INTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 25 HAS CORROSION ON FWD/RH EDGE<[01] REMOVED CORROSION ON FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; RBL 25. ORIGINAL THICKNESS OF 0.084; MATERIAL REMOVED .024; REMAINING THICKNESS IS 0.060. INTERCOSTAL FOUND TO BE OUT OF LIMITED PER SRM 53-70-51-1A-1.;REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL (P/N 147A5660U3) IAW SRM 51-40-02.

Part: ANGLE — CORRODED (ZONE 200) · airframe 26,284 hrs · 12,972 cycles

FWD ENTRY DOOR: THRESHOLD SUPPORT ANGLE LBL 61 FROM STA 312-348; HAS CORROSION AT SEVERAL NUTPLATES. (M) (M)<[01] REMOVED CORROSION PER SRM 51-10-02.;[02] INSPECTED DAMAGE REMOVAL;[03] TREATED AND PRIMED PER SRM 51-20-02.;[04] TREATED AND PRIMED PER SRM 51-20-01.

Part: ANGLE — CORRODED (ZONE 200) · airframe 26,284 hrs · 12,972 cycles

FWD ENTRY DOOR: THRESHOLD SUPPORT ANGLE LBL 58 FROM STA 312-348; HAS CORROSION AT SEVERAL NUTPLATES AND RADIUS AREA. (M)<[01] REMOVED CORROSION PER SRM 51-10-02.;[02] INSPECTED DAMAGE REMOVAL;[03] TREATED AND PRIMED PER SRM 51-20-02.;[04] TREATED AND PRIMED PER SRM 51-20-02.;[05] TREATED AND PRIMED PER SRM 51-20-01.

Part: PLATE — CORRODED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

CORROSION ON AFT CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA 727I-727J (MARKED)<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727I-727J ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.005; MAX ALLOWED IS 0.004 ?; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] TOOL T010008 S/N 503011WAS NOT USED;[03] CUT OUT DAMAGED SECTION OF THE LH SIDE PLATE FROM STA 727F+10 TO STA 787+10 FOR REPAIR PER SRM 53-00-53-1A-2;[04] LOCATED AND DRILLED NEW LH SIDE PLATE PER SRM 51-40-02;[05] COUNTERSUNK LH SIDE PLATE PER SRM 51-40-08.;[06] LOCATED AND DRILLED NEW LH SIDE PLATE FROM STA.727 - STA.847 PER SRM 51-40-02.;[07] RII. VERIFIED. LOCATED AND DRILLED NEW LH SIDE PLATE FROM STA.727 - STA.847 PER SRM 51-40-02. SIGN OFF FOR CORRECTIVE ACTION #6 ONLY.;[08] RII. VERIFIED COUNTERSUNK LH SIDE PLATE PER SRM 51-40-08. NEW LH SIDE PLATE FROM STA.727 - STA.847. SIGN OFF FOR CORRECTIVE ACTION #5 ONLY.;[09] RII. OK TO INSTALL NEW LH SIDE PLATE FROM STA 727 - STA 847.;[10] INSTALLED NEW LH SIDE PLATE FROM STA 727-847 PER SRM 51-40-02;[11] CW

Part: SKIN — DELAMINATED (ZONE 500) · airframe 26,284 hrs · 12,972 cycles

LH OUTBD AFT FLAP LOWER INBD CORNER HAS DELAMINATION ON UPPER AND LOWER SURFACES.<[01] OK TO INSTALL L/H OUTBD AFT FLAP.;[02] OK TO INSTALL AFT OUTBD FLAP;[03] INSTALLED NEW SERVICEABLE L/H O/B AFT FLAP PER AMM 27-51-22.;[04] INSTALLED NEW SERVICEABLE L/H O/B AFT FLAP PER AMM 27-51-22. RII INSPECTION C/W.

Part: PLATE — CORRODED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

CORROSION ON AFT CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA 727J-747 (MARKED)<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727J-747 ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.005; MAX ALLOWED IS 0.004 ?; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] TOOL T010008 S/N 503011WAS NOT USED;[03] SEE WORK CAPTURE # TTG8Q00UALJZ FOR REPLACEMENT OF LH SIDE PLATE;[04] CW

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 51 HAS CORROSION ON TOP/FWD SURFACE.<[01] REMOVED FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; RBL 51 PER SRM 51-40-02;[02] REMOVED CORROSION ON FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; RBL 51. ORIGINAL THICKNESS OF 0.210; MATERIAL REMOVED .009; REMAINING THICKNESS IS 0.201. INTERCOSTAL FOUND TO BE WITHIN LIMITED PER SRM 53-70-51-1A-1.;[03] REMOVED CORROSION ON FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; RBL 51. ORIGINAL THICKNESS OF 0.201; MATERIAL REMOVED .063; REMAINING THICKNESS IS 0.138. INTERCOSTAL FOUND TO BE OUT OF LIMITED PER SRM 53-70-51-1A-1.;[04] DISREGARD STEP 2;[05] LOCATED AND DRILLED FASTENER HOLES ON NEW INTERCOSTAL PER SRM<BR>51-40-05. EXCEPT FASTENER HOLES ATTACHING TO FLOOR STRUCTURAL 947 AND LAV MOUNT.;[06] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02;[07] INSPECTED AS REQUIRED. CORRECTIVE ACTION #5 AND #6

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

FLOOR SUPPORT MACHINED INTERCOSTAL LOCATED BETWEEN STAS 927-947; LBL 51 HAS CORROSION AT STA 946.<[01] REMOVED FLOOR SUPPORT MACHINED INTERCOSTAL LOCATED BETWEEN STA?S 927-947; LBL 51 PER SRM 51-40-02;[02] REMOVED LIGHT SURFACE CORROSION ON FLOOR SUPPORT MACHINED INTERCOSTAL LOCATED BETWEEN STA?S 927-947; LBL 51. ORIGINAL THICKNESS OF 0.074; MATERIAL REMOVED .001; REMAINING THICKNESS IS 0.073. INTERCOSTAL FOUND TO BE WITHIN LIMITED PER SRM 53-70-51-1A-1.;[03] DISREGARD STEP 2.<BR><BR>REMOVED LIGHT SURFACE CORROSION ON FLOOR SUPPORT MACHINED INTERCOSTAL LOCATED BETWEEN STA?S 927-947; LBL 51. ORIGINAL THICKNESS OF 0.70; MATERIAL REMOVED .023; REMAINING THICKNESS IS 0.047. INTERCOSTAL FOUND TO BE OUT LIMITED PER SRM 53-70-51-1A-1.;[04] LOCATED AND DRILLED FASTENER HOLES ON NEW INTERCOSTAL PER SRM<BR>51-40-05. EXCEPT FASTENER HOLES ATTACHING TO FLOOR STRUCTURAL 947 .;[05] INSTALLED INTERCOSTAL PER SRM 51-40-02.;[06] VERIFIED. LOCATED AND DRILLED FASTENER HOLES ON NEW INTERCOSTAL PER SRM<BR>51-40-05. EXCEPT FASTENER HOLES ATTACHING TO FLOOR STRUCTURAL 947.;[07] RII. VERIFIED INSTALLATION OF INTERCOSTAL LOCATED BETWEEN STA?S 927-947; LBL 51 PER SRM 51-40-02.

Part: PLATE — CORRODED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

CORROSION ON AFT CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA 747-767 (MARKED)<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 747-767 ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.005; MAX ALLOWED IS 0.004 ?; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] TOOL T010008 S/N 503011WAS NOT USED;[03] SEE WORK CAPTURE # TTG8Q00UALJZ FOR REPLACEMENT OF LH SIDE PLATE;[04] INSPECTED WORK ABOVE

Part: ATTACH ANGLE — CORRODED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

UPPER WEB ATTACH ANGLE LOCATED BETWEEN STAS 927-947; RBL 25 HAS CORROSION AT STA 946.<[01] REMOVED CORROSION UPPER WEB ATTACH ANGLE LOCATED BETWEEN STA?S 927-947; RBL 25 . ORIGINAL THICKNESS OF 0.070; MATERIAL REMOVED .019; REMAINING THICKNESS IS 0.051. ANGLE FOUND TO BE OUT OF LIMITED PER SRM 53-70-51-1A-1.;[02] LOCATED AND DRILLED NEW UPPER WEB ATTACH ANGLE (CHORD) BETWEEN STA 927 - 947 RBL 25 PER SRM 51-40-05; TREATED. AND PRIMED BARE METAL PER SRM 51-20-01;[03] INSPECTED C/A #2 LOCATING & DRILLING OF NEW UPPER WEB ATTACH ANGLE (CHORD) BETWEEN STA 927 - 947 RBL 25 PER SRM 51-40-05 & PRIMING OF BARE METAL PER SRM 51-20-01 (RII);[04] INSPECTED C/A #2 LOCATING & DRILLING OF NEW UPPER WEB ATTACH ANGLE (CHORD) BETWEEN STA 927 - 947 RBL 25 PER SRM 51-40-05 & PRIMING OF BARE METAL PER SRM 51-20-01;[05] REMOVED AND REPLACED ANGLE (CHORD) PER SRM 51-40-02;[06] INSPECTED AS REQUIRED. CORRECTIVE ACTION #5

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 26,284 hrs · 12,972 cycles

FLOOR STRUCTURE INTERCOSTAL LOCATED BETWEEN STAS 947-967; LBL 25 HAS CORROSION ON FWD/LH EDGE<[01] REMOVED FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; LBL 51 PER SRM 51-40-02;[02] REMOVED CORROSION ON FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; LBL 25. ORIGINAL THICKNESS OF 0.210; MATERIAL REMOVED .048; REMAINING THICKNESS IS 0.162. INTERCOSTAL FOUND TO BE OUT OF LIMITED PER SRM 53-70-51-1A-1.;[03] LOCATED AND DRILLED FASTENER HOLES ON NEW INTERCOSTAL PER SRM<BR>51-40-05. EXCEPT FASTENER HOLE ATTACHING TO FLOOR STRUCTURAL 947 AND LAV MOUNT.;[04] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02. REFERENCE TASK (TTG8Q00U9UHV);[05] INSPECTED AS REQUIRED. CORRECTIVE ACTION #3; #4

Part: PLATE — CORRODED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

CORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500A-500B.(MARKED)<[01] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] LOCATED AND DRILLED NEW TRANSITION ANGLE P/N #143A7501U188 PER SRM 51-40-05 ;OK TO INSTALL;[03] VERIFIED C/A # 1 : ROBERT DENSFORD (TECHNICIAN); 03-JUL-2024 12:01 UTC<BR>BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[04] VERIFIED C/A 2 : TONY NGUYEN (TECHNICIAN); 03-JUL-2024 14:10 UTC<BR>LOCATED AND DRILLED NEW TRANSITION ANGLE P/N #143A7501U188 PER SRM 51-40-05 ;OK TO INSTALL;[05] GRANTED OK TO INSTALL REPLACE SECTION FROM STA 500A TO STA 500 I;[06] REMOVED AND REPLACED RH SIDE PLATE FROM STA 500A TO STA 500I PER SRM 53-00-53-1A-2;AND SRM 51-40-02.;[07] 02 - INSPECTED PER [SRM 53-00-53-1A-2-B00297 (PERMANENT (NON-DENT DAMAGE TYPES))]

Part: PLATE — CORRODED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

CORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500C-500D.(MARKED)<[01] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.;[03] VERIFIED : ROBERT DENSFORD (TECHNICIAN); 03-JUL-2024 12:31 UTC<BR>BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[04] VERIFIED : ROBERT DENSFORD (TECHNICIAN); 03-JUL-2024 13:46 UTC<BR>BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.

Part: PLATE — CORRODED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

CORROSION ON FWD CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA. 500D-500E.(MARKED)<[01] BLENDED AREAS REMOVED .009' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] VERIFIED OUT OF LIMITS;[03] FABRICATED REPAIR PARTS PER SRM 53-00-53-2R-5 AND EA M-22-153-01550.;[04] 02 - INSPECTED PER [SRM 53-00-53-2R-5-B00308 (REPAIR 5 - CARGO COMPARTMENT SIDEPLATE REPAIR BETWEEN FLOOR PANEL SPLICES - PERMANENT)];[05] OK TO INSTALL ALL REPAIR PARTS PER SRM 53-00-53;[06] REPLACED SECTION OF SIDE PLATE FROM STA. 500B+10 TO 500E+10 PER SRM 53-00-53-2R-5 AND EA M-22-153-01550.;[07] 02 - INSPECTED PER [SRM 53-00-53-2R-5-B00308 (REPAIR 5 - CARGO COMPARTMENT SIDEPLATE REPAIR BETWEEN FLOOR PANEL SPLICES - PERMANENT)]

Part: PLATE — CORRODED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

CORROSION ON FWD CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA. 500E-500F.(MARKED)<[01] BLENDED AREAS; REMOVED .010 ' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION REPLACED ON NR# TTG8Q00UA2SG.;[02] BLENDED AREAS; REMOVED .010 ' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION REPLACED ON NR# TTG8Q00UA2SG.;[03] 02 - INSPECTED PER [SRM 53-00-53-1A-2-B00297 (PERMANENT (NON-DENT DAMAGE TYPES))];[04] 02 - INSPECTED PER [SRM 53-00-53-1A-2-B00297 (PERMANENT (NON-DENT DAMAGE TYPES))]

Part: PLATE — CORRODED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

CORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500H-500I.(MARKED)<[01] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.;[02] VERIFIED : ROBERT DENSFORD (TECHNICIAN); 03-JUL-2024 14:32 UTC<BR>BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.

Part: PLATE — CORRODED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

CORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500F-500G.(MARKED)<[01] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.;[02] VERIFIED : ROBERT DENSFORD (TECHNICIAN); 03-JUL-2024 14:17 UTC<BR>BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 26,284 hrs · 12,972 cycles

PASSENGER CABIN FLOOR BEAM BS947 RBL28 HAS SURFACE CORROSION ON TOP SIDE .<[01] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.052IN MATERIAL; REMAINING 0.128IN; FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1..;[02] ENTIRE LENGTH OF FLOOR BEAM UPPER FLANGE FROM LBL 60 - RBL 60 TO BE REMOVED AND REPAIRED PER SRM 53-70-51-2R-5; ALTERNATIVE 1 ON FAULT #TTG8Q00U9S43.;[03] LOCATED; MATCH DRILLED AND DEBURRED NEW FLOOR BEAM PER SRM 51-10-02.;[04] 01 - REMOVED AND REPLACED PER [REFERENCE] 51-10-02 OK TO INSTALL NEW FLOOR BEAM.;[05] INSTALLED FLOOR BEAM STA.947; LBL 60-RBL 60. PER SRM 51-10-02;[06] REMOVED AND REPLACED FLOOR BEAM STA. 947 LBL 60- RBL 60 PER SRM 51-10-02. ALSO; REFERENCE TASK (TTG8Q00U9S43);[07] RII INSPECTED AS REQUIRED. CORRECTIVE ACTION #5. REMOVE AND REPLACE OF STA. 947 FLOOR BEAM. REF.#TTG8Q00U9S43 FOR ALL WORK ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 26,284 hrs · 12,972 cycles

PASSENGER CABIN FLOOR BEAM BS947 LBL51 UNDER LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 LBL 51 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.100IN MATERIAL; REMAINING THICKNESS IS 0.080IN. OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] REMOVED AND REPLACED FLOOR BEAM STA. 947 LBL 60- RBL 60 PER SRM 51-10-02. ALSO; REFERENCE TASK (TTG8Q00U9S5C);[04] RII INSPECTED AS REQUIRED. CORRECTIVE ACTION #3. REMOVE AND REPLACE OF STA. 947 FLOOR BEAM.

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 26,284 hrs · 12,972 cycles

PASSENGER CABIN BS952 LBL25 SCREW HOLE HAS POSSIBLE CORROSION.<[01] REMOVED LIGHT SURFACE CORROSION ON PASSENGER CABIN BS952 LBL25 SCREW HOLE. ORIGINAL THICKNESS OF 0.083; MATERIAL REMOVED .003; REMAINING THICKNESS IS 0.080. INTERCOSTAL FOUND TO BE WITHIN LIMITED PER SRM 53-70-51-1A-1.;[02] SEE WORK CAPTURE # TTG8Q00UA9P8 FOR INTERCOSTAL REPLACEMENT.;[03] INTERCOSTAL REPLACED ON TASK CARD (TTG8Q00UA9P8);[04] INTERCOSTAL REPLACED PER SRM 51-40-02 ON TASK CARD (TTG8Q00UA9P8);[05] INSPECTED AS REQUIRED. CORRECTIVE ACTION #4

Part: ANGLE — CORRODED (ZONE 200) · airframe 26,284 hrs · 12,972 cycles

PASSENGER CABIN FLOOR BEAM AT APPROX. BS987 LBL 43 HAS CORROSION AROUND HOLE. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. CUT AND REMOVED DAMAGED PART OF FLOORBEAM IAW SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4. NDT PART 6;51-00-00 PROCEDURE 16. FABRICATED/DRILLED ANGLE AND STRAP PER SRM 53-70-51-2R-6. FLAP PEENED AREA PER SRM 53-70-51-2R-6 AND SOPM 20-10-03. FABRICATED FILLER IAW SRM 53-70-51-2R-6. TREATED & PRIMED PER SRM 51-20-01. INSTALLED REPAIR PARTS ON FLOORBEAM IAW SRM 53-70-51-2R-6.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 26,284 hrs · 12,972 cycles

PASSENGER CABIN FLOOR BEAM BS947 RBL50 UNDER AND AROUND LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 RBL 50 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.075IN MATERIAL; REMAINING THICKNESS IS 0.105IN. OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] ENTIRE LENGTH OF FLOOR BEAM UPPER FLANGE FROM LBL 60 - RBL 60 TO BE REMOVED AND REPAIRED PER SRM 53-70-51-2R-5; ALTERNATIVE 1 ON FAULT #TTG8Q00U9S43.;[04] 01 - REMOVED AND REPLACED 947 FLOOR BEAM SEE TASK CARD TTG8Q00U9S5C.;[05] VERIFIED

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 26,284 hrs · 12,972 cycles

PASSENGER CABIN FLOOR BEAM BS947 RBL25 UNDER AND AROUND LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 RBL 25 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.052IN MATERIAL; REMAINING THICKNESS IS 0.128IN. OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] CORRECTIVE ACTION #2 WRITTEN IN ERROR. WRONG N/R CARD.;[04] INSTALLATION OF LAV TIE DOWN FITTING AT STA 947; RBL 25 TO BE ACCOMPLISHED ON FAULT #TTG8Q00U9S43.;[05] FURTHER INSPECTION REVEALED NO CORROSION ON FLOOR BEAM AT STA 947; RBL 25 UNDER OR AROUND LAV TIE DOWN FITTING PER SRM 51-10-02.;[06] ENTIRE LENGTH OF FLOOR BEAM UPPER FLANGE FROM LBL 60-RBL 60 TO BE REMOVED AND REPAIRED PER SRM 53-70-51-2R-5; ALTERNATIVE 1 ON FAULT. #TTG8Q00U9S43.;[07] 02 - INSPECTED PER [SRM 51-10-02-0G-0-B00070 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)]

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 26,284 hrs · 12,972 cycles

PASSENGER CABIN FLOOR BEAM AT APPROX. BS987 LBL 43 HAS CORROSION AROUND HOLE.<[01] REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] CUT AND REMOVED DAMAGED PART OF FLOOR BEAM IAW SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4.;[03] C/W INSPECTION<BR>CUT AND REMOVED DAMAGED PART OF FLOOR BEAM IAW SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4.<BR>C/W NDT INSPECTION PER 737 NDT PART 6;51-00-00 PROCEDURE 23<BR> 737 NDT PART 6;51-00-00 PROCEDURE 16;[04] FABRICATED/DRILLED ANGLE AND STRAP PER SRM 53-70-51-2R-6.;[05] FLAP PEENED AREA PER SRM 53-70-51-2R-6 AND SOPM 20-10-03.;[06] FABRICATED FILLER PER SRM 53-70-51-2R-6.;[07] RII INSPECTED AS REQUIRED. CORRECTIVE ACTION #4; #5 AND #6.;[08] TREATED AND PRIMED PER SRM 51-20-01. OK TO INSTALL.;[09] VERIFIED TREATED AND PRIMED PER SRM 51-20-01. SIGN OFF FOR CORRECTIVE ACTION #8.;[10] RII. OK TO INSTALL REPAIR PARTS. SIGN OFF FOR CORRECTIVE ACTION #8.;[11] INSTALLED REPAIR PARTS AT PASSENGER CABIN FLOOR BEAM AT APPROX. BS987 LBL 43 PER SRM 53-70-51-2R-6.;[12] RII INSPECTED WORK ABOVE;[13] REPAIR COMPLEAT

Part: BRACKET — CORRODED (ZONE 600) · airframe 26,284 hrs · 12,972 cycles

RH WING LEADING EDGE FUEL GAUGE BRACKET HAS CORROSION MARKED<[01] REMOVED AND REPLACED WING REFUEL PANEL PER SOPM 20-50-01 AND MM 28-41-61.REFUELING PANELS OPS CHECKED GOOD PER MM 28-41-61;MM 28-21-81 AND MM 28-21-00;[02] C/W INSPECTION

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 24,880 hrs · 12,219 cycles

CENTER FWD EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 24,880 hrs · 12,219 cycles

RIGHT WING O/B AFT FLAP I/B TE DELAMINATED 14 BY 9 INCH. REMEASURE RIGHT WING O/B AFT FLAP FOUND FLAP DELAMINATED 20.6BY 9.5 INCH.<[01] R AND R RIGHT WING O/B AFT FLAP PER AMM 27-51-22.

Part: FLASHLIGHT — FAILED (ZN 200 FUS TOP) · airframe 24,115 hrs · 11,786 cycles

AFT GALLEY EMERGENCY FLASHLIGHT WILL NOT TEST. R/H #1 POS. / [01] REMOVED AND REPLACED AFT GALLEY EMERGENCY FLASHLIGHT. PER AMM 25-64-00. OPS CK GOOD.;[02] (CORRECTION TO MATCH LOGPAGE)REMOVED AND REPLACED AFT GALLEY EMERGENCY FLASHLIGHT. RH #1 POS PER AMM 25-64-00. OPS CK GOOD.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 23,726 hrs · 11,554 cycles

R/H AFT EMERGENCY LIGHTING BATTERY PACK WILL NOT CHARGE.<[01] REMOVED AND REPLACED BATTERY PER M/M 33-51-06.

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 22,948 hrs · 11,128 cycles

FWD GIRT BAR CAP. SIDE LOOSE<[01] ADJUSTED L-1 DOOR GIRT BAR IAW SIP. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: SEAT TRACK — DEFORMED (ZN 100 FUS LOWER) · airframe 19,861 hrs · 9,651 cycles

F.O. SEAT WILL NOT MOVE FOUND DEFORMATION ON AFT OUTBOARD F/O SEAT TRACK WHICH MAKES MOVEMENT DIFFICULT<[01] R&R FO'S AFT O/B SEAT TRACK IAW AMM 25-11-11

Part: FLASHLIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 21,562 hrs · 10,334 cycles

2 AFT CABIN FLASHLIGHTS INOP<[01] R&R SECURITY SEAL PER S.I.P;[02] PERFORMED OPS CHECK OF FLASH LIGHT; OPS CHECK GOOD PER AMM 25-64-00

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 20,737 hrs · 9,873 cycles

EXIT SIGN IN MID CABIN BY EMERGENCY EXIT ROW IS MISSING; CEILING / [01] REMOVED AND REPLACED MID-CABIN OVERHEAD EMERGENCY EXIT SIGN HOUSING AND LENS. OPS CHECK GOOD. REF AMM 33-51-01.

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 19,916 hrs · 9,391 cycles

ALL EMERGENCY EXIT LIGHTS CONNECTED TO BATTERY PACK M1673 ARE INOP. / [01] REMOVED AND REPLACED BATTERY PACK M1673 AND TEST GOOD IAW AMM 33-51-06-960-805.;[02] CERTIFIED REMOVED AND REPLACED BATTERY PACK M1673 AND PERFORMED GOOD INSTALL TEST AS PER AMM 33-51-06-960-805;[03] VERIFIED CORRECTIVE ACTIONS STEP 1.

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 19,916 hrs · 9,391 cycles

ALL EMERGENCY EXIT LIGHTS CONNECTED TO BATTERY PACK M1675 ARE INOP. / [01] REMOVED AND REPLACED BATTERY PACK AND TEST GOOD IAW AMM 33-51-06-960-805.;[02] REMOVED AND REPLACED BATTERY PACK M1675 AND TEST GOOD IAW AMM 33-51-06-960-805.;[03] CERTIFIED ALL WORK AND GOOD INSTALL TEST AS PER AMM 33-51-06-960-805;[04] VERIFIED CORRECTIVE ACTIONS STEP 2.

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 19,916 hrs · 9,391 cycles

ALL EMERGENCY EXIT LIGHTS CONNECTED TO BATTERY PACK M1672 ARE INOP. / [01] REMOVED AND REPLACED BATTERY PACK M1672 AND TEST GOOD IAW AMM 33-51-06-960-805.;[02] REMOVED AND REPLACED BATTERY PACK M1672 AS PER AMM 33-51-06-960-805;[03] VERIFIED CORRECTIVE ACTIONS STEP 1.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 19,916 hrs · 9,391 cycles

BREAK PANEL IS CRACKED AT STA 540; BL 0-LBL 25; WL 208. / [01] UPDATED TABLE;[02] REMOVED FLOOR PANEL 231UF PER AMM 53-21-00-000-801;[03] REMOVED BRAKE PANEL AT STA 540 BL0 - LBL 25 WL 208 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW BREAK PANEL AT STA 540 BL0 LBL 25 WL 208 PER SRM 51-40-05-0G-0. OK TO INSTALL;[05] CERTIFIED REMOVAL OF FLOOR PANEL #231UF AND REMOVAL OF BRAKE PANEL AND LOCATED AND DRILLED NEW BREAK PANEL;[06] VERIFIED CORRECTIVE ACTION #4;[07] INSTALLED BREAK PANEL AT STA 540; BL0 LBL 25;WL 208 I.A.W SRM 51-40-02-0G-0. OK TO INSTALL FLOOR PANEL 231UF.;[08] CERTIFIED INSTALLATION OF BREAK PANEL AT STA540 BLO-LBL25 WL 208;[09] VERIFIED CORRECTIVE ACTION #7;[10] INSTALLED FLOOR PANEL 231UF I.A.W AMM 53-21-00-400-801.<BR>TOOL ID: ATS2266 S/N 1703449 DATE: 02/2022 DUE: 02/2023;[11] CERTIFIED INSTALLATION OF FLOOR PANEL #231UF;[12] VERIFIED CORRECTIVE ACTION #10<BR>VERIFIED MEASUREMENTS

Part: ANGLE — CORRODED (AFT CARGO) · airframe 19,916 hrs · 9,391 cycles

AFT CARGO BAY ATTACH ANGLE COMMON TO SHIELD HAS AREAS OF CORROSION BS767 TO 787 RBL21 WL156 / [01] EVALUATED CORROSION ON ATTACH ANGLE BS 767 TO 787 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED ACTION #1;[03] REMOVED ACB ATTACH ANGLE COMMON TO SHIELD BS 767 TO BS 787; RBL 21; WL 156 PER SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW ACB ATTACH ANGLE COMMON TO SHIELD BS 767 TO BS 787; RBL 21; WL 156 PER DWG 146A8123 AND SRM 51-40-05-0G-0.;[05] VERIFIED CORRECTIVE ACTION #4;[06] OK TO INSTALL NEW ANGLE;[07] OK TO INSTALL GIVEN;[08] INSTALLED NEW ACB ATTACH ANGLE COMMON TO SHIELD BS 767 TO BS 787; RBL 21; WL 156 PER DWG 146A8123 AND SRM 51-40-02-0G-0.;[09] VERIFIED CORRECTIVE ACTION 8;[10] VERIFIED JOB COMPLETE AND MEASUREMENT TABLE

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 19,916 hrs · 9,391 cycles

FWD CARGO BAY AFT BULKHEAD LOWER SUPPORT HAS AREAS OF CORROSION BS500I LBL15 TO RBL15 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS OF BULKHEAD SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 500I RBL 14 WL 156; FOUND 0.020 REMOVED FROM ORIG 0.071 IN NUMEROUS 1'X1' AREAS; FOUND TO BE OUT OF LIMITS PER SRM 53-30-08-1A-1 USING DIAL DEPTH GAUGE ATS 2678 DUE 04/2023;[02] VERIFIED ACTION #1;[03] REMOVED FCB AFT BULKHEAD LOWER SUPPORT BS500I; LBL15 TO RBL15; WL156 PER SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW FCB AFT BULKHEAD LOWER SUPPORT BS500I; LBL15 TO RBL15; WL156 PER DWG 143A7902 AND SRM 51-40-05-0G-0. OK TO INSTALL.;[05] VERIFIED ACTION #3-4; OK TO INSTALL GIVEN;[06] INSTALLED NEW FCB AFT BULKHEAD LOWER SUPPORT BS500I; LBL15 TO RBL15; WL156 PER DWG 143A7902 AND SRM 51-40-02-0G-0.;[07] VERIFIED CORRECTIVE ACTION #6 AND MEASUREMENT FIELD;[08] VERIFIED CORRECTIVE ACTION #6 AND MEASUREMENT FIELD

Part: SHIELD — CORRODED (AFT CARGO) · airframe 19,916 hrs · 9,391 cycles

AFT CARGO BAY SHIELD FWD OF THE CARGO DOOR HAS AREAS OF CORROSION 767 TO 787 RBL21 WL156 / [01] EVALUATED CORROSION ON SHIELD BS 767 TO 787 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED ACTION #1;[03] REMOVED ACB FWD SHIELD BS 767 TO BS 792; RBL 21; WL 156 PER SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW ACB FWD SHIELD BS 767 TO BS 792; RBL 21; WL 156 PER DWG 146A0081 AND SRM 51-40-05-0G-0;[05] VERIFIED CORRECTIVE ACTION #4;[06] OK TO INSTALL;[07] OK TO CLOSE GIVEN;[08] INSTALLED NEW ACB FWD SHIELD BS 767 TO BS 792; RBL 21; WL 156 PER DWG 146A0081 AND SRM 51-40-02-0G-0;[09] VERIFIED CORRECTIVE ACTION ITEM 8.;[10] VERIFIED MEASUREMENTS.<BR>VERIFIED FAULT COMPLETE.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 19,916 hrs · 9,391 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION BS727F TO BS767 RBL21 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 727I +10 RBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN NUMEROUS 1'X1' AREAS; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2678 DUE 04/2023;[02] VERIFIED ACTION #1;[03] VALIDATED APPLICABILITY OF SRM 53-00-53-2R-5;[04] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E + 10 - BS767; RBL21; WL156 PER SRM 53-00-53-2R-5 STEP 4.B. SRM 51-40-02-0G-0;[05] FABRICATED; LOCATED AND APPLIED CHEMICAL CONVERSION COATING TO ACB FLOOR TO SIDEWALL SUPPORT AT BS727E+10' - BS767; RBL21; WL156 AND SPLICE REPAIR AT BS727E+8' - BS727E+18' USING BAC1496-77#7075T62 LOT # 1477731-1 PER SRM 51-40-05-0G AND DWG 146A7500; SRM 53-00-53-2R-5 STEP 4. I. AMM 51-21-41-370-802;[06] CORRECTION TO STEP 5; MATERIAL USED IS BAC1496-377#7075T62;[07] VERIFIED CORRECTIVE ACTION #4-6; OK TO PRIME;[08] APPLIED PRIMER TO ACB FLOOR TO SIDEWALL SUPPORT PER SRM 53-00-53-2R-5 STEP 4. J.;[09] OK TO INSTALL REPAIR PARTS.;[10] VERIFIED CORRECTIVE ACTION #9 OK TO INSTALL;[11] INSTALLED NEW ACB FLOOR TO SIDEWALL SUPPORT AT BS727E+10' - BS767; RBL21; WL156 AND SPLICE REPAIR AT BS727E+8' - BS727E+18' PER SRM 53-00-53-2R-5 AND DWG 146A7500;;[12] VERIFIED CORRECTIVE ACTION #11 AND MEASUREMENT FIELD;[13] VERIFIED CORRECTIVE ACTION #11 AND MEASUREMENT FIELD

Part: BRACKET — BROKEN (AFT CARGO) · airframe 19,916 hrs · 9,391 cycles

AFT CARGO BAY LAV TANK BULKHEAD LOWER BRACKET IS BROKEN BS867 LBL10 WL166 / [01] REMOVED DAMAGED LAV TANK LOWER BRACKET; BS867 LBL10; WL 166; LOCATED AND DRILLED AND INSTALLED NEW BRACKET; IAW SRM 51-40-02-0G-0; 51-40-05-0G-0; DWG 149A8104; DWG; 149A8102. IPC 53-42-51-06.;[02] VERIFIED CORRECTIVE ACTION #1

Part: ANGLE — CRACKED (CENTER WING) · airframe 19,916 hrs · 9,391 cycles

L/H BS663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED RBL 8 WL 167.68 / [01] VALIDATED APPLICABILITY OF SRM 57-10-10-2R-5;[11] LOCATED; DRILLED; TRIMMED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING AND PRIMERED REPAIR PARTS @ LH BS663 VAPOR BARRIER UPPER ATTACH ANGLE LBL8-LBL20 WL167.68 IAW SRM 57-10-10-2R-5. OK TO INSTALL.;[12] VERIFIED CORRECTIVE ACTION STEP 11. VERIFIED OK TO INSTALL.;[13] INSTALLED LH BS663 VAPOR BARRIER UPPER ATTACH ANGLE REPAIR PARTS LBL8-LBL20 WL167.68 IAW SRM 57-10-10-2R-5. BOND CHECK GOOD. BONDING METER ID:ATS758 S/N:1971 DUE:08/2022.;

Part: ANGLE — CRACKED (CENTER WING) · airframe 19,916 hrs · 9,391 cycles

R/H BS663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED RBL 8 WL 167.68 / [01] VALIDATED APPLICABILITY OF SRM 57-10-10-2R-5;[[08] RECEIVED REPAIR PARTS FOR RH BS663 VAPOR BARRIER UPPER ATTACH ANGLE. RECEIVED SPLICE ANGLE RO#877067-SWA AND REPLACEMENT ANGLE RO#87066-SWA.;[09] CORRECTION: REPLACEMENT ANGLE RO#877066-SWA.;[10] VERIFIED ACTION #8-9;[11] LOCATED; DRILLED; TRIMMED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING AND PRIMERED REPAIR PARTS @ RH BS663 VAPOR BARRIER UPPER ATTACH ANGLE RBL8-RBL20 WL167.68 IAW SRM 57-10-10-2R-5. OK TO INSTALL.;[12] VERIFIED CORRECTIVE ACTION STEP 11. VERIFIED OK TO INSTALL.;[13] INSTALLED RH BS663 VAPOR BARRIER UPPER ATTACH ANGLE REPAIR PARTS RBL8-RBL20 WL167.68 IAW SRM 57-10-10-2R-5. BOND CHECK GOOD. BONDING METER ID:ATS758 S/N:1971 DUE:08/2022.;

Part: LENS — DETACHED (CABIN) · airframe 19,526 hrs · 9,179 cycles

CEILING EXIT SALIDA SIGN OVER CENTER AISLE LENS DETACHED / [01] SECURED CENTER AISLE EXIT SIGN LENS PER SIP

Part: LIGHT — FAILED (OVERWING EXIT) · airframe 19,145 hrs · 8,960 cycles

OVERWING CEILING EXIT SIGNS CAME OFF / [01] SECURED LENS PER SIP

Part: FAN — FAULTY (CABIN RECIRC) · airframe 18,834 hrs · 8,794 cycles

SMELL/FUMES IN CABIN ON CLIMB OUT. AFTER APPROX. 10 MIN; THE SMELL DISSIPATED / [01] FOUND RIGHT RECIRC FAN C/B POPPED REPLACED RIGHT RECIRC FAN PER AMM 21-25-02 OPS CHECKS OK<BR>REPLACED RIGHT CABIN RECIRCULATION FILTER PER MM 21-25-01

Part: LENS — MISSING (OVERWING EXIT) · airframe 18,384 hrs · 8,542 cycles

OVERWING CEILING EMERGENCY LENS M.I.A. ; / [01] FOUND LEN?S RESECURRED PER S.I.P.

Part: LIGHT — DAMAGED · airframe 18,135 hrs · 8,409 cycles

EMERGENCY EXIT CEILING SIGN DAMAGED. / [01] RESECURED LIGHT COVER PANEL PER SIP;NO DAMAGE NOTICE

Part: FLASHLIGHT ASSY — INOPERATIVE (AFT CABIN) · airframe 14,118 hrs · 6,286 cycles

AFT GALLEY FLIGHT ATTENDANT EMERGENCY FLASHLIGHT LOCATED INBOARD. CAPTAIN'S SIDE WILL NOT TEST PROPERLY. OK TO CONTINUE, PER MEL 25-12-01; SP-1B; TRACKING NUMBER 99807. R & R BATTERY AND FLASHLIGHT ASSEMBLY, PER AMM 25-64-00 CL NR 80816.

Part: BATTERY — FAULTED (FLASHLIGHT) · airframe 14,118 hrs · 6,286 cycles

AFT GALLEY FLIGHT ATTENDANT EMERGENCY FLASHLIGHT LOCATED INBOARD. CAPTAIN'S SIDE WILL NOT TEST PROPERLY. OK TO CONTINUE, PER MEL 25-12-01; SP-1B; TRACKING NUMBER 99807. R & R BATTERY AND FLASHLIGHT ASSEMBLY, PER AMM 25-64-00 CL NR 80816.

Part: FAIRING — DELAMINATED (FUSELAGE) · airframe 12,212 hrs · 5,361 cycles

REMOVED WTB FAIRING 192BL DUE TO DELAMINATION ON LE OF PNL / ACCOMPLISHED PERMANENT REPAIR IAW SRM 51-70-05 INSTALLED FAIRING 192BL IAW AMM 47-31-02. (SEE SA-M 326 ATTACHED: A755268)

Part: BATTERY — INOPERATIVE (AFT FLASHLIGHT) · airframe 11,424 hrs · 5,030 cycles

"1" AFT GALLEY EMERGENCY FLASHLIGHT WOULD NOT TEST. / R&R BATTERY IAW AMM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 8,715 hrs · 3,822 cycles

LT REAR EMERGENCY EXIT SIGN LENS FELL OFF AT ROW 16. REINSTALLED LENS PER MM.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 433 hrs · 213 cycles

RT AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPOSITIONED FLASHLIGHT AT MOUNT BASE IAW MM.