N8565Z

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 24,689 hrs · 12,655 cycles

RIGHT SIDE EMERGENCY BATTERY PACK M1676 INOPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-06-960-805.

Part: DOUBLER — CRACKED (ZN 100 FUS LOWER) · airframe 24,689 hrs · 12,655 cycles

EGPR DOOR CUT OUT LOWER DOUBLER IS CRACKED. ACCOMPLISHED REPAIR IAW SRM 53-10-15-2R-4, PARAGRAPH E, FIGURE 204, AND EA 25-153-02159-WIP 2.

Part: HANDLE — LOOSE (ZONE 800) · airframe 24,689 hrs · 12,655 cycles

CR RR R2 DOOR ASSIST HANDLE NEEDS SECURED<[01] SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 52-13-31;[02] SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 52-13-31

Part: PUMP — FAILED (ZONE 400) · airframe 23,757 hrs · 12,164 cycles

ON APPROACH; 'B' ENG DRIVEN PUMP LOW PRESSURE LIGHT FLICKERED AND THEN CAME ON SOLID. ELECT B PUMP LOW PRESSURE LIGHT ALSO ILLUMINATED. VERIFIED QTY WENT TO ZERO. FOLLOWED QRH. FOUND FLUID COMING FROM HYD DRAIN PAD DRAIN. SUSPECT THE PUMP FAILED.<[01] FOUND #2 ENGINE HYD PUMP HAD FAILED. R&R #2 ENGINE HYD PUMP AND ALL CASE DRAIN FILTERS. LEAK AND OPS CHECKS GOOD PER AMM 29-11-11; 29-11-51; 29-11-41

Part: FILTER — FAILED (ZONE 200) · airframe 23,757 hrs · 12,164 cycles

ON APPROACH; 'B' ENG DRIVEN PUMP LOW PRESSURE LIGHT FLICKERED AND THEN CAME ON SOLID. ELECT B PUMP LOW PRESSURE LIGHT ALSO ILLUMINATED. VERIFIED QTY WENT TO ZERO. FOLLOWED QRH. FOUND FLUID COMING FROM HYD DRAIN PAD DRAIN. SUSPECT THE PUMP FAILED.<[01] FOUND #2 ENGINE HYD PUMP HAD FAILED. R&R #2 ENGINE HYD PUMP AND ALL CASE DRAIN FILTERS. LEAK AND OPS CHECKS GOOD PER AMM 29-11-11; 29-11-51; 29-11-41

Part: SLIDE — OUT OF ADJUST (ZONE 800) · airframe 23,569 hrs · 12,066 cycles

AFT GALLEY FIRST OFFICER SIDE EMERGENCY SLIDE COVERING LOOSE<[01] INSPECTED SLIDE ASSY. NO LOOSE PIECES FOUND. PER A.M.M. 25-66-00 G.V.I. WITHOUT REMOVING ASSY. ON AFT GALLEY SERVICE DOOR SIDE

Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 23,054 hrs · 11,782 cycles

FA REPORTS EMERGENCY LIGHTS COME ON AFTER TAKEOFF AND STAY ILLUMINATED FOR APPROX 2 MIN AND THEN GO OFF ON THEIR OWN. THE LIGHT AT R-2 DOOR AND AFT GALLEY AREA.<[01] REMOVED. AND REPLACED EMERGENCY LIGHT CHARGER AS PER AMM 33-51-06 AT LOCATION M01672; OPERATIONAL CHECKS NORMAL.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 22,990 hrs · 11,752 cycles

ROW 7ABC EMERGENCY LIGHTS INOP<[01] R&R'D BATTERY PACK IAW AMM 33-51-06

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 22,990 hrs · 11,752 cycles

L2 DOOR EMERGENCY LIGHT INOP<[01] R&R'D BATTERY PACK IAW AMM 33-51-06

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 22,990 hrs · 11,752 cycles

R2 DOOR EMERGENCY LIGHT INOP<[01] R&R'D BATTERY PACK IAW AMM 33-51-06

Part: RELEASE MECH — INOPERATIVE (ZONE 200) · airframe 21,950 hrs · 11,167 cycles

FLIGHT DECK F/O'S SLIDING WINDOW WILL NOT OPEN WHEN EXTERIOR EMERGENCY RELEASE HANDLE IS PULLED.<[01] READJUSTED FLIGHT DECK F/O'S SLIDING WINDOW RELEASE MECHANISM PER AMM 56-12-11

Part: SIGN — WRONG PART (ZONE 200) · airframe 21,829 hrs · 11,096 cycles

EXIT SIGN BY CAPTAINS SIDE AFT LAV BLANK<[01] REPLACED EXIT SIGN COVER PER AMM 33-51-01.

Part: BATTERY — INOPERATIVE (AFT FLASHLIGHT) · airframe 20,784 hrs · 10,516 cycles

FA REPORTS AFT RIGHT INBD INOP<[01] R&R EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00.

Part: LIGHT — DAMAGED (CABIN) · airframe 19,940 hrs · 10,049 cycles

PHOTO LUMINESCENT STRIP BUBBLED IN MULTIPLE AREAS AT 19ABC<[01] R&R PHOTOLUMINESCENT STRIP AT AREA 19ABC PER AMM 33-51-15.;[02] INSPECTED WORK PERFORMED

Part: SKIN — CRACKED (FUSELAGE) · airframe 19,940 hrs · 10,049 cycles

GROUND POWER PANEL CUTOUT CRACKED AT THE SIX O CLOCK POSITION.<[01] REMOVED DAMAGE PER SRM 53-10-15-2R-4;[02] PERFORMED .040 INSURANCE CUT AFTER NDT PER SRM 53-10-15-2R-4;[03] PREFORMED SURFACE HFEC INSPECTION PART 6 ; 51-00-00 PROCEDURE 23;[04] INSPECTED WORK ABOVE;[05] FABRICATED REPAIR PARTS PER SRM 53-10-15-2R-4;[06] INSPECTED WORK ABOVE;[07] OK TO INSTALL REPAIR PARTS;[08] REPAIRED GROUND POWER PANEL REF SRM 53-10-15-2R-4.;[09] REPAIRED GROUND POWER PANEL REF SRM 53-10-15-2R-4. C/W INSPECTION

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 19,940 hrs · 10,049 cycles

HORIZONTAL STAB. LEFT; UPPER FWD SLIDER SEAL IS CRACKED AT THE FRONT SIDE APROX 3 INCHES LONG.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-401 CONFIG 1-NG (STABILIZER TO BODY FRONT SPAR SLIDING SEAL - REMOVAL/INSTALLATION - PERMANENT)]. ADJUSTMENT AND OPS CHECK GOOD PER AMM 53-31-31.;[02] C/W INSPECTION;[03] C/W INSPECTION

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,940 hrs · 10,049 cycles

FOWARD EMERGENCY LIGHT ABOVE COCKPIT DOOR ENTRY INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY BASE M1675; OPS CHECKS GOOD PER MM 33?51-06;[02] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY BASE M1675; OPS CHECKS GOOD PER MM 33?51-06;[03] 02 - INSPECTED PER [AMM 33-51-06-960-806-NG (POWER SUPPLY - POWER SUPPLY REPLACEMENT - PERMANENT)]

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO AFT CORNER SCUFF PLATE CRACKED<[01] RECEIVED NEW SERVICEABLE SCUFF PLATE. DRILLED AND COUNTERSINK IAW SRM 51-40-05.;[02] RECEIVED NEW SERVICEABLE SCUFF PLATE. DRILLED AND COUNTERSINK IAW SRM 51-40-05. INSPECTED C/A 2. RECEIVED NEW SERVICEABLE SCUFF PLATE. DRILLED AND COUNTERSINK IAW SRM 51-40-05.

Part: PLATE — BROKEN (ZN 600 RIGHT WIN) · airframe 19,940 hrs · 10,049 cycles

WAFFLE PLATE BROKEN R/H WING ABOVE #6 FLAP TRACK<[01] REMOVED AND REPLACED WAFFLE PLATE PHENOLIC NUT PLATE ATTACHMENT IAW SRM 51-40-02-0G-0.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 19,940 hrs · 10,049 cycles

R/H WING: #8 SLAT HAS A DELAMINATED AREA TO THE RIGHT OF THE CHAFFED AREA. DELAMINATED AREA IS MARKED AND PICTURE OF DAMAGED AREA IS ATTACHED TO THIS TASK CARD.<[01] R/H WING: #8 SLAT REMOVED AND REPLACED ON FOUND FAULT # TTG8Q00R9J0Y.;[02] VERIFIED THE REMOVAL AND REPLACEMENT OF THE #8 SLAT IS BEING ACCOMPLISHED ON FOUND FAULT #TTG8Q00R9J0Y. NO WORK WAS PERFORMED ON THIS TASK CARD.

Part: BOOT — CRACKED (RADOME) · airframe 19,940 hrs · 10,049 cycles

NOSE RADOME BOOT HAS MULTIPLE CRACKS AND HOLES EXPOSING COMPOSITE UNDERLAYER<[01] REMOVED AND REPLACED RADOME PER AMM 53-52-00;[02] 02 - INSPECTED PER [AMM 53-52-00-400-801-NG (NOSE RADOME INSTALLATION - PERMANENT)]

Part: CARGO TRACK — CORRODED (BS 767-) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO FLOOR RAIL CORRODED AT STA 767+4'; RBL 3. AFT CARGO FLOOR RAIL CORRODED AT STRAP LOCATION STA 767+4' RBL 3.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.055' REMAINING THICKNESS). RAIL IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] TRIM OUT DAMAGE IAW SRM 53-00-53-2R-2 REPAIR 2. ALT. 4.;[03] C/W INSPECTION OF C/A #2 ONLY.;[04] TRIM OUT DAMAGE IAW SRM 53-00-53-2R-2 REPAIR 2. ALT. 5;[05] C/W INSPECTION OF C/A #4 ONLY. C/A #3 WAS IN ERROR;[06] ACCOMPLISHED HFEC INSPECTION OF DAMAGE CUTOUT PER NDT PART 6 51-00-00 PROC. 23 NO DEFECTS NOTED;[07] LOCATE AND DRILLED REPAIR CHANNEL IAW SRM 53-00-53-2R-2 REPAIR 2 ALT. 5;[08] C/W INSPECTION OF C/A #7 ONLY;[09] ALODINE AND PRIMED REPAIR CHANNEL AND REPAIR AREA IAW SRM 53-00-53-2R-2 REPAIR 2.;[10] VERIFIED CORRECTIVE ACTION #9. OK TO INSTALL REPAIR PARTS;[11] INSTALLED REPAIR CHANNEL IAW SRM 53-00-53-2R-2 REPAIR 2; ALTERNATIVE 5.;[12] VERIFIED CORRECTIVE ACTION #11

Part: SCUFF PLATE — MISSING (FWD DOOR) · airframe 19,940 hrs · 10,049 cycles

FED ENT DOOR FWD SCUFF PLATE IS MISSING<

Part: PANEL — CORRODED (ZONE 100) · airframe 19,940 hrs · 10,049 cycles

PANEL 113BW HAS AREAS OF INNER SURFACE CORROSION AND MISSING PAINT.<[01] PROCURED NEW PANEL. PANEL WILL BE INSTALLED ON NR TTG8Q00QEXAR.;[02] NOSE ACCESS PANEL 113BW;[03] INSTALLED PANEL I.A.W AMM 53-14-01. LEAK CHECK TO BE PERFORMED ON 721-000-00-01; FAULT TTG8R007ELL4.;[04] INSTALLED PANEL I.A.W AMM 53-14-01. LEAK CHECK TO BE PERFORMED ON 721-000-00-01; FAULT TTG8R007ELL4.

Part: PLATE — CORRODED (BS 767-787) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 767-787 AROUND FASTENER HOLES. AFT CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 767-787 AROUND FASTENER HOLES.<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1 (0'044' REMAINING THICKNESS). SHIELD (SIDE PLATE) IS OUT OF LIMITS PER SRM 53-60-15-1A-1.;[02] REMOVED RH SHIELD (SIDE PLATE).;[03] DRILLED AND COUNTERSUNK NEW SIDE PLATE ( SHIELD) IAW SRM 51-40-05 AND SRM 51-40-08.<BR>NEED OK TO INSTALL.;[04] OKAY TO INSTALL NEW SIDE PLATE ASSEMBLY.;[05] INSTALLED FASTENER ON R/H SIDE SIDE PLATE {SHIELD} IAW SRM 51-40-02.;[06] C/W INSPECTION OF THE REPLACED AND INSTALLED PART.

Part: FLOOR SUPPORT — CORRODED (BS 787-807) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 787-807 AROUND FASTENER HOLES. AFT CARGO COMPARTMENT FLOOR STRUCTURE LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 787-807 AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; REMAINING THICKNESS IS 0.034. OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ;[03] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ

Part: MOUNT — CORRODED (BS 647) · airframe 19,940 hrs · 10,049 cycles

AFT GALLEY LAV MOUNT HAS CORROSION AROUND BASE AT STA 947 RBL 24.<[01] CLEANED CORROSION PER SRM 51-10-02. REWORKED AREA REMAINING THICKNESS IS OUT OF LIMIT PER SRM 52-70-51-1A-1 DETAIL C.;[02] REJECT: FAULT CURRENTLY HAS 2 ISSUES:<BR><BR>1. MEASUREMENT #17; CORRODED ELEMENT PART NUMBER () HAS INCOMPLETE PART NUMBER LISTED.<BR><BR>2. MEASUREMENT #22 AND #23 ARE INCONSISTENT WITH OUT OF LIMITS FINDING IN CORRECTIVE ACTION #1.<BR><BR>PLEASE SEE INSPRJCT PAUSE NOTES UNDER 'TASK INFORMATION' TAB FOR GUIDANCE ON THIS REJECTION.<BR><BR>**PLEASE NOTE THAT ALL CORRECTIONS MUST BE DONE ON ORIGINAL FAULT. INSPECTION WILL CLEAR REJECTION FAULT AFTER REJECTED TASK/FAULT HAS BEEN CORRECTED.**;06] REPAIR OF AFT GALLEY MOUNT CORROSION AT STA 947 RBL 24 HAS BEEN REPAIRED PER SRM 53-70-51-2R-5 ON FAULT # ID TTG8Q00RB9L0;[07] VERIFIED CORRECTIVE ACTION #6

Part: PLATE — CORRODED (BS 727J-747) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 727J-747 AROUND FASTENER HOLES. AFT CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 727J-747 AROUND FASTENER HOLES.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 ( 0.035' REMAINING THICKNESS). SIDE PLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] CUT AND REMOVED RH SIDE PLATE SECTION FROM STA. 727H+10 TO STA. 767 IAW SRM 53-00-53-2R-5.;[03] FABRICATE NEW RH SIDE PLATE SECTION FROM STA. 727H+10 TO STA. 767 AND REPAIR SPLICE IAW SRM 53-00-53-2R-5.;[04] RII INSPECTED C/A 2. AND C/A 3.;[05] ALODINE AND PRIME NEW RH SIDE PLATE AND REPAIR SPLICE IAW SRM 53-00-53-2R-5.;[06] INSTALLED BONDED NUTPLATES RH SIDE PLATE STA 727 H+10 TO 767 PER SRM 51-40-10-2R-0 AT 12:30 PM; FEB 13.;[07] INSPECTED WORK PERFORMED ON C/A #6 FOR INITIAL INSTALL OF NUTPLATES.;[08] OK TO INSTALL REPAIR PARTS.;[09] INSTALLED RH SIDE PLATE REPAIR PARTS FROM STA. 727H+10 TO STA. 767 PER SRM 53-00-53-2R-5.;[10] RII: INSPECTED WORK PERFORMED ON C/A #9;[11] REPAIRED RH SIDE PLATE STA 727H+10' TO 767 PER SRM 53-00-53-2R-5.;[12] VERIFIED REPAIRED RH SIDE PLATE STA 727H+10' TO 767 PER SRM 53-00-53-2R-5.

Part: SUPPORT WEB — CORRODED (ZONE 100) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO DOOR SURROUND STRUCTURE: SUPPORT WEB FOR FLOOR SCUFF PLATE HAS CORROSION ON THE UPPER SURFACE. LOCATED AT STA 787 +17; +19; +21; +24; +39; +45; +47 AND +49. RBL 20. AFT CARGO DOOR SURROUND STRUCTURE: SUPPORT WEB FOR FLOOR SCUFF PLATE HAS CORROSION ON THE UPPER SURFACE. LOCATED AT STA 787 +17 +19 +21 +24 +39 +45 +47 AND +49. RBL 20.<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.041' REMAINING THICKNESS). WEB ID OUT OF LIMITS PER SRM 53-60-15-1A-1.;[02] REMOVED AFT CARGO DOOR THRESHOLD WEB PER SRM 51-40-02;[03] DRILLED AND COUNTERSUNK NEW WEB IAW SRM 51-40-05 AND SRM 51-40-08.;[04] C/W INSPECTION OF C/A #3 ONLY.;[05] OK TO INSTALL WEB;[06] INSTALLED REPLACEMENT THRESHOLD WEB I.A.W SRM 51-40-02.

Part: STRIP — CORRODED (BS 887) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT: SCREW STRIP AT STA 887 HAS CORROSION AROUND FASTENER HOLES AT RBL 1; 5; 10; 14 AND 20. AFT CARGO COMPARTMENT: SCREW STRIP AT STA 887 HAS CORROSION AROUND FASTENER HOLES AT RBL 1 5 10 14 AND 20.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.055' REMAINING THICKNESS). STRIP (STRAP) IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] OBTAINED REPLACEMENT PART FROM STOCK; DRILLED FASTENER HOLES AND INSTALLED NUTPLATES PER SRM 51-40-02. OKAY TO INSTALL.;[03] INSPECTED WORK ACCOMPLISHED IN C/A #2. RANDY MOSIER (TECHNICIAN); 24-FEB-2024 01:46 UTC OBTAINED REPLACEMENT PART FROM STOCK; DRILLED FASTENER HOLES AND INSTALLED NUT PLATES PER SRM 51-40-02. OKAY TO INSTALL.;[04] REMOVED AND REPLACED SCREW T-STRIP IAW SRM 51-40-02-0G-0.;[05] C/W INSPECTION

Part: PLATE — CORRODED (BS 847) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 847+6;_10;+15;AND +20 AROUND FASTENER HOLES. AFT CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 847+6_10+15AND +20 AROUND FASTENER HOLES.<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.046' REMAINING THICKNESS). SIDE PLATE (SHIELD) IS OUT OF LIMITS PER SRM 53-60-15-1A-1.;[02] REMOVED RH SHIELD (SIDE PLATE).;[03] DRILLED AND COUNTERSUNK NEW R/H SHIELD I.A.W. SRM 51-40-05 AND SRM 51-40-08. <BR>NEED OK TO INSTALL;[04] OK TO INSTALL;[05] INSTALLED FASTENERS ON NEW RIGHT SIDE SHIELD I.A.W SRM 51-40-02.;[06] VERIFIED CORRECTIVE ACTION #5

Part: PLATE — CORRODED (BS 807-827) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 807-827 AROUND FASTENER HOLES. AFT CARGO COMPARTMENT FLOOR STRUCTURE LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 807-827 AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; REMAINING THICKNESS IS 0.034. OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ;[03] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ

Part: PLATE — CORRODED (BS 767-787) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 767-787 AROUND FASTENER HOLES. AFT CARGO COMPARTMENT FLOOR STRUCTURE LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 767-787 AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; REMAINING THICKNESS IS 0.033. OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] REMOVED R/H SIDE SHIELD ( SIDE PLATE) IAW SRM 51-40-02.<BR>DRILLED AND COUNTERSUNK NEW SIDE PLATE ( SHIELD) IAW SRM 51-40-05 AND SRM 51-40-08.NEED OK TO INSTALL.;[03] SIGNED ON WRONG DOCUMENT DISREGARD STEP2;[04] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ;[05] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ

Part: MOUNT — CORRODED (LAVATORY) · airframe 19,940 hrs · 10,049 cycles

AFT GALLEY LAV MOUNT HAS CORROSION AROUND BASE AT STA 947 LBL 24.<[01] CLEANED CORROSION PER SRM 51-10-02. REWORKED AREA MEASURED OUT OF LIMITS IAW SRM 53-70-51-1A-1 FIG. 104; DETAIL E.;[07] CUT AND REMOVED ENTIRE UPPER SECTION OF STA 947 CHORD I.A.W SRM 53-70-51-2R-5.;[08] VERIFIED CUT AND REMOVED ENTIRE UPPER SECTION OF STA 947 CHORD I.A.W SRM 53-70-51-2R-5.;[09] ACCOMPLISHED HFEC SURFACE AND HOLE PROBE OF REPAIR AREA PER NDT PART 6 51-00-00 PROC. 23 AND 51-00-00 PROC 16 NO DEFECTS NOTED;[10] FLAP PEENED UPPER CHORD CUT EDGE IAW SRM 53-70-51-2R-5 AND RESTORED FINISH PER SRM 51-21-73;[11] VERIFIED FLAP PEENED UPPER CHORD CUT EDGE IAW SRM 53-70-51-2R-5 AND RESTORED FINISH PER SRM 51-21-73.;[12] FABRICATED; LOCATED; AND DRILLED T-CHORD IAW SRM 53-70-51-2R-5;[13] VERIFIED FABRICATED; LOCATED; AND DRILLED T-CHORD IAW SRM 53-70-51-2R-5.;[14] OK TO INSTALL T-CHORD.;[15] INSTALLED T-CHORD AND SPLICE PER SRM 53-70-51-2R-5. OK TO INSTALL REMOVED ATTACHING STRUCTURE.;[16] INSTALLED T-CHORD AND SPLICE PER SRM 53-70-51-2R-5. (RII)<BR> OK TO INSTALL REMOVED ATTACHING STRUCTURE.

Part: FLOOR SUPPORT — CORRODED (BS 727H-727I) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727H-727I AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; REMAINING THICKNESS IS 0.033. OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ;[03] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ

Part: PLATE — CORRODED (BS 747-767) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 747-767 AROUND FASTENER HOLES. AFT CARGO COMPARTMENT FLOOR STRUCTURE LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 747-767 AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; REMAINING THICKNESS IS 0.034. OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ;[03] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ

Part: FLOOR SUPPORT — CORRODED (BS 727E-727F) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727E-727F AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; REMAINING THICKNESS IS 0.033; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ;[03] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ

Part: PLATE — CORRODED (BS 727C-727D) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727C-727D AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; REMAINING THICKNESS IS 0.035; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ;[03] WORK COMPLETED ON CARD TTG8Q00RAMEJ

Part: PLATE — CORRODED (BS 727J-747) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727J-747 AROUND FASTENER HOLES. AFT CARGO COMPARTMENT FLOOR STRUCTURE LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727J-747 AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS. REMAINING THICKNESS IS 0.034. OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ;[03] COMPLETED ON CARD TTG8Q00RAMEJ

Part: PLATE — CORRODED (BS 727G-727C) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727B-727C AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; REMAINING THICKNESS IS 0.034; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] REMOVED L/H SIDE PLATE PER SRM 51-40-02 FROM STA 727-847.;[03] OK TO INSTALL NEW SIDE PLATE.;[04] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ;[05] WORK COMPLETED ON CARD TTG8Q00RAMEJ

Part: MOUNT — CORRODED (BS 947) · airframe 19,940 hrs · 10,049 cycles

AFT GALLEY LAV MOUNT HAS CORROSION AROUND BASE AT STA 947 LBL48.<[01] CLEAN CORROSION PER SRM 51-10-02. REWORKED AREA IS OUT OF LIMIT PER SRM 53-70-51-1A-1 DETAIL C.;[02] REJECT: FAULT CURRENTLY HAS 3 ISSUES:<BR><BR>1. MEASUREMENT #17; CORRODED ELEMENT PART NUMBER () HAS INCOMPLETE PART NUMBER LISTED.<BR><BR>2. MEASUREMENT #22 AND #23 ARE INCONSISTENT WITH OUT OF LIMITS FINDING IN CORRECTIVE ACTION #1.<BR><BR>3. THE CALIBRATED TOOLING LISTED ON THIS FAULT IS INCOMPLETE.<BR><BR>PLEASE SEE INSPRJCT PAUSE NOTES UNDER 'TASK INFORMATION' TAB FOR GUIDANCE ON THIS REJECTION.<BR><BR>**PLEASE NOTE THAT ALL CORRECTIONS MUST BE DONE ON ORIGINAL FAULT. INSPECTION WILL CLEAR REJECTION FAULT AFTER REJECTED TASK/FAULT HAS BEEN CORRECTED.**;[03] ASSIGNED CALIBRATED TOOLING AS REQUIRED. VERIFIED ALL MEASUREMENTS AND CORRECTED #17; 21; 22; AND 23 TO BE CONSISTENT WITH OUT OF LIMITS FINDING IN CORRECTIVE ACTION #1. REWORKED AREA IS OUT OF LIMITS PER SRM 53-70-51-1A-1; DETAIL C.;[04] INSPECTION CONFIRMS THAT REJECTION NOTED ON CORRECTIVE ACTION #2 HAS BEEN CORRECTED AS REQUIRED PER MPM 51.03.01 AND MPM 51.03.04.02. NO FURTHER ACTION REQUIRED. REJECTION FOUND FAULT CLEARED AT THIS TIME.;[05] REPAIR OF AFT GALLEY MOUNT CORROSION AT STA 947 LBL 48 HAS BEEN REPAIRED PER SRM 53-70-51-2R-5 ON FAULT # ID TTG8Q00RB9L0;[06] VERIFIED

Part: STRIP — CORRODED (BS 727) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT: SCREW STRIP AT STA 727I+4 HAS CORROSION AROUND FASTENER HOLES AT RBL 15 AND 20 AND LBL 8; 10 AND 14. AFT CARGO COMPARTMENT: SCREW STRIP AT STA 727I+4 HAS CORROSION AROUND FASTENER HOLES AT RBL 15 AND 20 AND LBL 8 10 AND 14.<[01] REMOVED AND REPLACED SCREW STRIP (FLOOR STRAP) PER AMM 25-52-01.

Part: STRIP — CORRODED (BS 767) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT: SCREW STRIP AT STA 767+4 HAS CORROSION AROUND THE FASTENER HOLES AT LBL 6 AND RBL 6; 10; 12; 14 AND 16. AFT CARGO COMPARTMENT: SCREW STRIP AT STA 767+4 HAS CORROSION AROUND THE FASTENER HOLES AT LBL 6 AND RBL 6 10 12 14 AND 16.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.065' REMAINING THICKNESS). STRAP (STRIP) IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED AND REPLACED SCREW STRIP (FLOOR STRAP) PER AMM 25-52-01 AND SRM 53-00-53-1A-2.

Part: PLATE — CORRODED (BS 747-767) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 747-767 AROUND FASTENER HOLES. AFT CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDE PLATE HAS SURFACE CORROSION FROM STA 747-767 AROUND FASTENER HOLES.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). SIDE PLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] FABRICATE AND INSTALLED NEW RH SIDE PLATE SECTION FROM STA. 727H+10 TO STA. 767. ALL WORK IS ACCOMPLISHED UNDER TASK CARD# TTG8Q00RAMLU; LINE # 2095;[03] VERIFIED CORRECTIVE ACTION #2

Part: PLATE — CORRODED (BS 727F-727G) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727F-727G AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; REMAINING THICKNESS IS 0.034; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ;[03] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ

Part: PLATE — CORRODED (BS 727A-727B) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727A-727B AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS. REMAINING THICKNESS IS .006; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] REMOVED L/H SIDE PLATE FOR REPLACEMENT PER SRM 51-40-02 FROM STA 727-827.;[03] REMOVED LH SIDE PLATE PER SRM 51-40-02 FROM STA 727-847.;[04] OK TO INSTALL NEW SIDE PLATE.;[05] INSTALLED NEW L/H SIDE PLATE FROM STA 727-847 PER SRM 51-40-02;[06] COMPLETED WITH NEW

Part: FLOOR SUPPORT — CORRODED (BS 727G-727H) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727G-727H AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; REMAINING THICKNESS IS 0.035. OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ;[03] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ

Part: PLATE — CORRODED (BS 727D-727E) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727D-727E AROUND FASTENER HOLES.<[01] REMOVED CORROSION; REMAINING THICKNESS IS 0.035; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ;[03] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ

Part: HANDLE — LOOSE (FWD PAX DOOR) · airframe 19,940 hrs · 10,049 cycles

FWD. ENTRY DOOR HANDLE CAM PLATE IS LOOSE(HAS PLAY).<[01] FOUND CASTELLATED CAM PLATE NUT HAD SEVERAL MISSING CASTELLATIONS. REMOVED AND REPLACED NUT IAW CMM. 52-16-12.;[02] FOUND CASTELLATED CAM PLATE NUT HAD SEVERAL MISSING CASTELLATIONS. REMOVED AND REPLACED NUT IAW CMM. 52-16-12. C/W INSPECTION

Part: PLATE — CORRODED (BS 727I-727J) · airframe 19,940 hrs · 10,049 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727I-727J AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; REMAINING THICKNESS IS 0.034. OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ;[03] L/H SIDE PLATE IS REPLACED WITH NEW FROM STA 727 - 847. ALL WORK AND SIGN OFFS ACCOMPLISHED ON TASK CARD TTG8Q00RAMEJ

Part: ANGLE — CORRODED (BS 500C-500D) · airframe 19,940 hrs · 10,049 cycles

FWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500D TO 500C<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] FAULT IS RESOLVED ON FAULT ID # TTG8Q00RA85G;[03] VERIFIED CORRECTIVE ACTION #2

Part: ANGLE — CORRODED (BS 500-500A) · airframe 19,940 hrs · 10,049 cycles

FWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500A TO 500<[01] REMOVED RH TRANSITION SHIELD ASSY ANGLE IAW SRM 51-40-02-0G-0.;[02] DRILLED NEW RH TRANS SHIELD ASSY ANGLE IAW SRM 51-40-05-0G-0.;[03] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[04] OK TO INSTALL;[05] INSTALLED NEW R/H SHIELD TRANSITION ANGLE IAW SRM 51-40-02.;[06] INSPECTED C/A 5.

Part: ANGLE — CORRODED (BS 500B-500C) · airframe 19,940 hrs · 10,049 cycles

FWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500C TO 500B<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] FAULT IS RESOLVED ON FAULT ID # TTG8Q00RA85G;[03] VERIFIED CORRECTIVE ACTION #2

Part: ANGLE — CORRODED (BS 500E-500F) · airframe 19,940 hrs · 10,049 cycles

FWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500F TO 500E<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] FAULT IS RESOLVED ON FAULT ID # TTG8Q00RA85G;[03] VERIFIED CORRECTIVE ACTION #2

Part: ANGLE — CORRODED (BS 500A-500B) · airframe 19,940 hrs · 10,049 cycles

FWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500B TO 500A<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] REMOVED R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-40-02.;[03] DRILLED AND COUNTERSUNK NEW TRANSITION ANGLE PER SRM 51-40-05 AND SRM 51-40-08.<BR>NEED OK TO INSTALL;[04] OK TO CLOSE;[05] INSTALLED NEW FROM STOCK TRANSITION ANGLE PER SRM 51-40-02.;[06] VERIFIED CORRECTIVE ACTION #5

Part: SUPPORT ANGLE — CORRODED (BS 500I) · airframe 19,940 hrs · 10,049 cycles

FWD CARGO BULKHD PANEL SUPPORT ANGLE AT STA. 500I HAS CORROSION.<[01] CLEAN CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-30-08-1A-1 FIG 103 DETAILD.;[02] REMOVED SUPPORT ANGLE PER SRM 51-40-02.;[03] DRILLED NEW ANGLE PER SRM 51-40-05; COUNTERSUNK DRILLED HOLES PER SRM 51-40-08. INSTALLED NEW FROM STOCK ANGLE PER SRM 51-40-02.;[04] DRILLED NEW ANGLE PER SRM 51-40-05; COUNTERSUNK DRILLED HOLES PER SRM 51-40-08. INSTALLED NEW FROM STOCK ANGLE PER SRM 51-40-02

Part: ANGLE — CORRODED (BS 500H-500I) · airframe 19,940 hrs · 10,049 cycles

FWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500I TO 500H<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] DRILLED NEW RH TRANSITION ANGLE IAW SRM 51-40-05-0G-0.;[03] FAULT IS RESOLVED ON FAULT ID # TTG8Q00RA85G;[04] VERIFIED CORRECTIVE ACTION #3

Part: ANGLE — CORRODED (BS 500C-500D) · airframe 19,940 hrs · 10,049 cycles

FWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500D TO 500C<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2;[02] FAULT RESOLVED ON FAULT ID # TTG8Q00RA85G;[03] VERIFIED CORRECTIVE ACTION #2

Part: ANGLE — CORRODED (BS 500F-500G) · airframe 19,940 hrs · 10,049 cycles

FWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500G TO 500F<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] FAULT IS RESOLVED ON FAULT ID # TTG8Q00RA85G;[03] VERIFIED CORRECTIVE ACTION #2

Part: ANGLE — CORRODED (BS 500G-500H) · airframe 19,940 hrs · 10,049 cycles

FWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500H TO 500G<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] FAULT IS RESOLVED ON FAULT ID # TTG8Q00RA85G;[03] VERIFIED CORRECTIVE ACTION#2

Part: ANGLE — CORRODED (BS 500D-500E) · airframe 19,940 hrs · 10,049 cycles

FWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500E TO 500D<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] FAULT IS RESOLVED ON FAULT ID # TTG8Q00RA85G;[03] VERIFIED CORRECTIVE ACTION #2

Part: CABLE — CORRODED (ZN 600 RIGHT WIN) · airframe 19,940 hrs · 10,049 cycles

R/H WING FWD AILERON CABLE HAS SURFACE CORROSION AT TURN AROUND PULLEY/AILERON QUADRANT FWD OF AILERON INPUT ROD.<[01] FABRICATED TERMINAL B FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 AND CUT CABLES TO LENGTH; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 AND SOPM 20-50-16;[02] FABRICATED TERMINAL B FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 AND CUT CABLES TO LENGTH; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 AND SOPM 20-50-16;[03] FABRICATED TERMINAL A FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 ; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 AND SOPM 20-50-16;[04] INSTALLED RIGHT AILERON CONTROL CABLES ABSA-R1 AND ABSB-R2 PER. M.M. 20-10-91;[05] DOUBLE TENSIONED NEW CABLE IAW AMM 27-11-00;[06] RII: INSPECTED WORK PERFORMED ON C/A #3; C/A #4; AND C/A #5;[07] ADJUSTED POGO AND POWER CONTROL UNIT (PCU) PER AMM 27-11-00 DOUBLE TENSIONED CABLES AND CYCLED AILERON 20 TIMES AND ADJUSTED CABLES TO AILERON CABLE RIG LOAD PER AMM 27-09-14 AND AMM 27-11-00 AND MMS AP37.8-0618;[08] RII: VERIFIED CORRECTIVE ACTION #7

Part: CABLE — CORRODED (RT AILERON) · airframe 19,940 hrs · 10,049 cycles

R/H WING O/B AILERON CABLE SWAGED END HAS SURFACE CORROSION AT AILERON QUADRANT FWD OF AILERON INPUT ROD.<[01] FABRICATED TERMINAL B FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 AND CUT CABLE TO LENGTH; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 AND SOPM 20-50-16;[02] FABRICATED TERMINAL B FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 AND CUT CABLE TO LENGTH; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 AND SOPM 20-50-16;[03] FABRICATED TERMINAL A FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 ; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 AND SOPM 20-50-16;[04] INSTALLED RIGHT AILERON CONTROL CABLES ABSA-R1 AND ABSB-R2 PER. M.M. 20-10-91;[05] DOUBLE TENSIONED NEW CABLE IAW AMM 27-11-00;[06] RII: INSPECTED WORK PERFORMED ON C/A #3; C/A #4; AND C/A #5;[07] ADJUSTED AILERON POGO AND POWER CONTROL UNIT (PCU) PER AMM 27-11-00 DOUBLE TENSIONED RH CABLES CYCLED AILERON 20 TIMES AND ADJUSTED CABLES TO AILERON CABLE RIG LOAD PER AMM 27-09-14 AND AMM 27-11-00 AND MMS AP37.8-0618;[08] RII: VERIFIED CORRECTIVE ACTION #7

Part: BALANCE WEIGHT — CORRODED (RT AILERON) · airframe 19,940 hrs · 10,049 cycles

R/H AILERON I/B BALANCE WEIGHTS 4(EA.) FWD OF AILERON INPUT ROD HAVE SURFACE CORROSION (MKD)<[01] REMOVED AND REPLACED WEIGHTS IAW SRM 51-60-03;[02] VERIFIED REMOVED AND REPLACED WEIGHTS IAW SRM 51-60-03.

Part: CABLE — CORRODED (RT AILERONS) · airframe 19,940 hrs · 10,049 cycles

R/H WING AFT AILERON CABLE HAS SURFACE CORROSION AT TURN AROUND PULLEY/AILERON QUADRANT FWD OF AILERON INPUT ROD.<[01] FABRICATED TERMINAL B FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 AND CUT CABLE TO LENGTH; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 AND SOPM 20-50-16;[02] FABRICATED TERMINAL B FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 AND CUT CABLE TO LENGTH; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 AND SOPM 20-50-16;[03] FABRICATED TERMINAL A FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 ; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 AND SOPM 20-50-16;[04] INSTALLED RIGHT AILERON CONTROL CABLES ABSA-R1 AND ABSB-R2 PER. M.M. 20-10-91;[05] -DOUBLE TENSIONED NEW CABLE IAW AMM 27-11-00;[06] RII: INSPECTED WORK PERFORMED ON C/A #3; C/A #4; AND C/A #5;[07] ADJUSTED AILERON POGO AND POWER CONTROL UNIT (PCU) PER AMM 27-11-00 DOUBLE TENSIONED RH CABLES CYCLED AILERON 20 TIMES AND ADJUSTED CABLES TO AILERON CABLE RIG LOAD PER AMM 27-09-14 AND AMM 27-11-00 AND MMS AP37.8-0618;[08] RII: VERIFIED CORRECTIVE ACTION #7

Part: CABLE — CORRODED (RT AILERON) · airframe 19,940 hrs · 10,049 cycles

R/H WING I/B AILERON CABLE SWAGED END HAS SURFACE CORROSION AT AILERON QUADRANT FWD OF AILERON INPUT ROD.<[01] FABRICATED TERMINAL B FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 AND CUT CABLE TO LENGTH; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 AND SOPM 20-50-16;[02] FABRICATED TERMINAL B FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 AND CUT CABLE TO LENGTH; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 AND SOPM 20-50-16;[03] FABRICATED TERMINAL A FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 ; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 AND SOPM 20-50-16;[04] INSTALLED RIGHT AILERON CONTROL CABLES ABSA-R1 AND ABSB-R2 PER. M.M. 20-10-91;[05] DOUBLE TENSIONED NEW CABLE IAW AMM 27-11-00;[06] RII: INSPECTED WORK PERFORMED ON C/A #3; C/A #4; AND C/A #5;[07] ADJUSTED AILERON POGO AND POWER CONTROL UNIT (PCU) PER AMM 27-11-00 DOUBLE TENSIONED RH CABLES CYCLED AILERON 20 TIMES AND ADJUSTED CABLES TO AILERON CABLE RIG LOAD PER AMM 27-09-14 AND AMM 27-11-00 AND MMS AP37.8-0618;[08] RII: VERIFIED CORRECTIVE ACTION #7

Part: FLASHLIGHT — FAILED (ZN 200 FUS TOP) · airframe 19,713 hrs · 9,916 cycles

AFT GALLEY FLASH LIGHT AIRCRAFT RIGHT WILL NOT TEST<[01] PERFORMED PUSH TO TEST FLASHLIGHT CHEKC ON R/H AFT GALLEY FLASHLIGHT PER AMM 25-64-00. TESTS OK.

Part: BATTERY PACK — INOPERATIVE (ZN 100 FUS LOWER) · airframe 19,254 hrs · 9,655 cycles

AFT AISLE AND LH ENTRY DOOR INTERIOR EMERGENCY LIGHTS INOP.<[01] REMOVED AND REPLACED AFT LH EMERGENCY LIGHT BATTERY PACK IN REFERENCE WITH AMM 33-51-06. OPS CHECK GOOD AT THIS TIME.

Part: OVERHEAT SENSOR — INTERMITTENT (ZN 200 FUS TOP) · airframe 18,625 hrs · 9,303 cycles

FIRE WARNING LIGHT AND BELL ALONG WITH WHEEL WELL LIGHT ILLUMINATED; THEN WENT OUT. ON APPROACH; AFTER LANDING GEAR EXTENDED DOWN; HAPPENED AGAIN.<[01] REMOVED AND REPLACED INTERMITTENTLY SHORTINGWHEEL WELL OVERHEAT SENSING ELEMENT IAW AMM CHPT. 26-18-02.

Part: LIGHT — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 18,291 hrs · 9,109 cycles

CEILING EXIT SIGN BETWEEN OVERWINGS IS NOT FULLY ATTACHED<[01] SECURED EMERGENCY EXIT SIGN IAW AMM 33-51-01

Part: LIGHT — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 18,169 hrs · 9,043 cycles

CENTER AISLE EXIT SIGN DISLODGED<[01] REINSTALLED LIGHT ASSY IAW AMM 33-51-01

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 17,458 hrs · 8,632 cycles

FWD SERVICE DOOR SLIDE FELL OUT OF HOUSING<[01] REPOSITION SLIDE TO THE HOUSING PER AMM 25-66-00

Part: SLIDE — OUT OF POSITION (ZN 800 DOOR) · airframe 17,457 hrs · 8,631 cycles

FWD SERVICE DOOR SLIDE FELL OUT OF HOUSING<[01] REPOSITION SLIDE TO HOUSING PER AMM 25-66-00 AND MT 725-61-06

Part: FLASHLIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 17,344 hrs · 8,564 cycles

AFT PANEL HAND HELD FLASH LIGHT TEST RED<[01] R&R AFT HAND HELD FLASH LIGHT BATTERY IAW AMM <BR>25-64-00; OPS CHK OK

Part: FLASHLIGHT — INOPERATIVE · airframe 15,525 hrs · 7,533 cycles

AFT GALLEY CAPTS SIDE FLASHLIGHT INOP / [01] PROPERLY SEATED AND PERFORMED FLASH LT CHECK AT AFT LEFT IAW AMM 25-64-00

Part: FLASHLIGHT — FAILED · airframe 15,111 hrs · 7,274 cycles

BOTH FWD FLASHLIGHT WOULD NOT TEST / [01] REPLACED BATTERIES IN BOTH FLASHLIGHTS PER AMM 25-64-00

Part: COVER — MISSING (OVERWING EXIT) · airframe 14,237 hrs · 6,796 cycles

EXIT SIGN COVER MISSING AT AFT RIGHT OVERWING EXIT / [01] INSTALLED A NEW EMERGENCY EXIT LIGHT AS REQUIRED. LIGHT OPS CKS GOOD IAW AMM 33-51-01.

Part: BATTERY — FAULTY (CABIN) · airframe 12,977 hrs · 6,094 cycles

AFT GALLEY FLIGHT ATTENDANT FLASH LIGHT RED ; / [01] OK TO CONTINUE PER MEL 25-12-01<BR>AUTH #43569; [02] REACHED BATTERY ON F.O. OUTBD. FLASHLIGHT AFT GALLEY PER SIP.

Part: INDICATOR — INCORRECT (TE FLAPS) · airframe 12,947 hrs · 6,078 cycles

FLAPS WOULD NOT EXTEND PAST 10 DEGREES. ; / [01] PERFORMED FLAP SKEW DETECTION FUNCTIONAL TEST. NO DEFECTS NOTED. REF AMM 27-59-00. PERFORMED FIM 27-51 TASK 849. FOUND #1 TRAILING EDGE FLAPS TRANSMISSION TORQUE TRIP INDICATOR EXTENDED. REPLACED #1 FLAP TRANSMISSION OIL. REF AMM 12-22-51. OPS CHECK GOOD.

Part: FLOOR PANEL — UNSECURE (CABIN)

AISLE FLOOR BETWEEN ROWS 16 & 17 'POPS' EXCESSIVELY WHEN WALKED ON.C/W REPAIR-53EA-04959 REV 1 / 1-A53-31403 REV 1REPETITIVE INSPECTION ACTION; ACTION REQUIRED: PERFORM GENERAL VISUAL EXAMINATION OF THE PANEL TO ENSURE PANEL IS FREE OF DEFECTS (CRACKS; DENTS; PUNCTURES; ETC.) IF DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. INSPECTION THRESHOLD: 100 FLIGHT CYCLES; REPEAT INSPECTION INTERVAL: 100 FLIGHT CYCLES. PERMANENT REPAIR LIMIT; ACTION REQUIRED PERFORM PERMANENT REPAIR BY REPLACING PANEL OR RECTIFY PER AMM 53-21-00/401 PERMANENT REPAIR TIME LIMIT: 250 FLIGHT CYCLES *** REPETITIVE ACTION REQUIRED *** /

Part: FLOOR PANEL — UNSECURE (CABIN)

AISLE FLOOR BETWEEN ROWS 16 & 17 'POPS' EXCESSIVELY WHEN WALKED ON.C/W REPAIR-53EA-04959 REV 1 / 1-A53-31403 REV 1REPETITIVE INSPECTION ACTION; ACTION REQUIRED: PERFORM GENERAL VISUAL EXAMINATION OF THE PANEL TO ENSURE PANEL IS FREE OF DEFECTS (CRACKS; DENTS; PUNCTURES; ETC.) IF DEFECTS ARE NOTED; CONTACT SERVISE ENGINEERING. INSPECTION THRESHOLD: 100 FLIGHT CYCLES; REPEAT INSPECTION INTERVAL: 100 FLIGHT CYCLES. PERMANENT REPAIR LIMIT; ACTION REQUIRED PERFORMED PERMANENT REPAIR BY REPLACING PANEL OR RECTIFY PER AMM 53-21-00/401 PERMANENT REPAIR TIME LIMIT: 250 FLIGHT CYCLES *** PERMANENT ACTION REQUIRED *** /

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 5,214 hrs · 11,310 cycles

CREW REPORTS AFT LEFT OUTBOARD EMERGENCY FLASHLIGHT WONT TEST ( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ) / REMOVED AND REPLACED AFT ELFT EMERGENCY FLASHLIGHT BATTERY PACK REF AMM 25-64-00. OPS CHECK GOOD. THIS CLEARS MEL 25-12-01. AUTH # 113405. CL # 91095

Part: FLASHLIGHT — NO TEST (FWD CABIN) · airframe 10,687 hrs · 4,876 cycles

CREW REPORTS FWD FA OD FLASHLIGHT FAILS TEST. REINSTALLED FWD FA OB FLASHLIGHT PER MM 256400.

Part: BATTERY — NO TEST (AFT FLASHLIGHT) · airframe 10,504 hrs · 4,778 cycles

AFT LFT FLASHLIGHT WILL NOT TEST. REMOVED AND REPLACED BATTERY PER MM 256400.

Part: PANEL — CRACKED (AFT CARGO) · airframe 7,116 hrs · 3,104 cycles

AFT CARGO FWD BULKHEAD PANEL 142NW DAMAGED/CRACKED IN 3 LOCATIONS. / R+R 142W PANEL IAW AMM 25-52-78 AMT 69696

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 5,138 hrs · 2,240 cycles

FORWARD LT UPPER ENTRY EMERGENCY LIGHTS INOP. R&R BATTERY PACK PER AMM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 2,672 hrs · 1,162 cycles

AFT RT GALLEY UNDER RH FLIGHT ATTENDANCE SEAT EMERGENCY FLASHLIGHT INOP. REPAIRED FLASHLIGHT ASSEMBLY PER MMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 1,807 hrs · 771 cycles

AFT RT SIDE INBOARD EMERGENCY FLASHLIGHT INOP. R&R BATTERY IAW AMM.

Part: ADIRU — FAILED (E&E BAY) · airframe 872 hrs · 385 cycles

DIVERSION, NR 2 AIR DATA INERTIAL REFERENCE UNIT FAILED INFLIGHT. R&R NR 2 DATA INERTIAL REFERENCE UNIT PER AMM.