N8523W

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 29,552 hrs · 14,814 cycles

AFT MEGAPHONE INOPERATIVE. R & R AFT MEGAPHONE IAW AMM 25-64-00

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 29,314 hrs · 14,696 cycles

R/H OVERWING EMERGENCY LIGHTS ARE INOPERABLE. REMOVED AND REPLACED THE RT OVERWIND EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06.

Part: PANEL — PULLED (ZONE 500) · airframe 29,314 hrs · 14,696 cycles

PANEL 561CB HAS SEVERAL PULLED THROUGH HOLES. DAMAGE OUTSIDE OF ALLOWABLE LIMITS, SANDED AND CLEANED AREAS OF PANEL IN PREPARATION FOR REPAIR IAW SRM 57-51-01-1A-1, SRM 57-51-01-2R-1, AND SRM 51-70-05-2R-8. REPAIRED AREAS WHERE DAMAGED IAW SRM 57-51-01-2R-1, AND SRM 51-70-05-2R-8. REPAIRED AND RESTORED ALL FINISHES TO PANEL 561CB IAW SRM 57-51-01-2R-1, AND SRM 51-70-05-2R-8.

Part: PANEL — PULLED (ZONE 500) · airframe 29,314 hrs · 14,696 cycles

PANEL 561CB HAS SEVERAL PULLED THROUGH HOLES. DAMAGE OUTSIDE OF ALLOWABLE LIMITS, SANDED & CLEANED AREAS OF PANEL IN PREPARATION FOR REPAIR IAW SRM 57-51-01-1A-1, SRM 57-51-01-2R-1, AND SRM 51-70-05-2R-8. REPAIRED AREAS WHERE DAMAGED IAW SRM 57-51-01-2R-1, AND SRM 51-70-05-2R-8. REPAIRED AND RESTORED ALL FINISHES TO PANEL 561CB IAW SRM 57-51-01-2R-1, AND SRM 51-70-05-2R-8.

Part: ATTACH BRACKET — CRACKED (ZONE 200) · airframe 29,314 hrs · 14,696 cycles

SEAT TRACK NR 1 ATTACH BRACKET HAS POSSIBLE CRACK AT RADUIS BS 727B. HFEC VERIFIED THE ATTACHED BRACKET IS CRACKED AT BS 727B IAW NDT PART 6; 51-00-00 PROCEDURE 23. REMOVED AND REPLACED THE ATTACH BRACKET FOR NR 1 SEAT TRACK IAW SRM 51-40-05, AND SRM 51-40-02.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 29,314 hrs · 14,696 cycles

CABIN CENTER SECTION FLOORBEAM CRACKED AT BS 540, LBL 1. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-02.

Part: FASTENER — CRACKED (ZONE 400) · airframe 29,314 hrs · 14,696 cycles

RIGHT INLET COWL OUTER LIP SKIN FASTENER AT 6 O'CLOCK, HEAD CRACKED. REMOVED AND OVERSIZED TO 1ST OVER RT INLET COWL OUTER LIP SKIN FASTENER AT 6 O'CLOCK POSITION IAW SRM 54-10-01-1A-2. PERFORMED NDT OF FASTENER HOLE PER NDT MANUAL PART6 51-00-00 PROCEDURE 11. NO DEFECTS FOUND. OKAY TO INSTALL NEW FASTENER. INSTALLED NEW FASTENER PER SRM 54-10-01-1A-2. INSPECTED AND VERIFIED. CA 3 COMPLIED WITH AND OKAY TO INSTALL PANEL 412/422AB. REINSTALLED PANEL 412/422AB IAW SRM 51-40-02; SEALED PER AMM 51-31-00, AND APPLIED DECORATIVE EXTERIOR FINISH IAW AMM 51-21-99.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 28,782 hrs · 14,412 cycles

ROW 14ABC AND 15BC EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 28,662 hrs · 14,350 cycles

EMERGENCY FLASHLIGHT IN AFT GALLEY CAPTS SIDE INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT AFT GALLEY CA SIDE #2 BATTERY IAW AMM 25-64-00. OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 27,568 hrs · 13,760 cycles

AFT LEFT MOST OUTBOARD FLASHLIGHT INOP UNDER F/A SEAT<[01] OK TO CONTINUE PER MEL 25-12-01 SP1B;[02] R AND R AFT LEFT O/B FLASH LIGHT ASSEMBLY IAW AMM 25-64-00 OPS CK GOOD

Part: FLASHLIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 26,233 hrs · 13,038 cycles

FWD GALLEY FLASHLIGHT PANEL STATUS LIGHT INOP.<[01] REPLACED FWD GALLEY FLASHLIGHT CRADLE IAW SIP. OPS CK GOOD.

Part: STRIP — CORRODED (ZONE 200) · airframe 26,231 hrs · 13,036 cycles

ALL FWD CARGO CAP STRIPS HAVE CORROSION ON THE LOWER SURFACE.<[01] R/R LH CAP STRIP AT STA 500D TO STA 500I REF. AMM 25-52-06;[02] C/W INSPECTION OF CA #1;[03] REMOVED LIGHT CORROSION. ORIGINAL THICKNESS OF 0.050IN; REMOVED 0.003IN; REMAINING THICKNESS OF 0.047IN. FOUND TO BE WITHIN LIMITS; TREATED AND APPLIED DECORATIVE FINISH PER SRM 53-00-53-1A-2.;[04] C/W INSPECTION

Part: STRIP — CORRODED (ZONE 100) · airframe 26,231 hrs · 13,036 cycles

VARIOUS AFT CARGO CAP STRIPS HAVE CORROSION ON THE LOWER SURFACE.<[01] INSTALLATION OF CAPSTRIPS TO BE ACCOMPLISHED ON FAULTS TTG8Q00XGA0F AND TTG8Q00XGA0G.;[02] REMOVED LIGHT CORROSION. ORIGINAL THICKNESS OF 0.050IN; REMOVED 0.003IN; REMAINING THICKNESS OF 0.047IN. FOUND TO BE WITHIN LIMITS; TREATED AND APPLIED DECORATIVE FINISH PER SRM 53-00-53-1A-2.;[03] C/W INSPECTION

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 26,231 hrs · 13,036 cycles

CABIN EMERGENCY LIGHT BATTERY PACK INOP AT STA 527C R/H<[01] REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-06. INSTALLATION TEST IS GOOD.;[02] VERIFIED

Part: SLIDE — OUT OF ADJUST (ZONE 200) · airframe 26,231 hrs · 13,036 cycles

FWD PASSENGER CABIN ENTRY DOOR ESCAPE SLIDE LOOSE AT ATTACH POINTS.<[01] SECURED SLIDE PER SOPM 20-50-01.;[02] 02 - INSPECTED PER [SOPM SOPM REPREF NOT FOUND (SOPM REPAIR REFERENCE NOT FOUND (NO FOLLOW-ON ACTIONS REQUIRED))] 20-50-01

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 26,231 hrs · 13,036 cycles

FWD CARGO DOOR FWD CORNER SCUFFPLATE (PN 143A8331-3) IS CRACKED<[01] INSTALLED NEW FWD CARGO DOOR CORNER SCUFFPLATE PER AMM 53-11-02;[02] VERIFIED

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 26,231 hrs · 13,036 cycles

AFT CARGO DOOR FWD CORNER SCUFFPLATE (PN 146A8341-7) IS CRACKED<[01] REMOVED DAMAGED CORNER SCUFF PLATE AND INSTALLED NEW SERVICEABLE CORNER SCUFF PLATE PER AMM 53-11-02.;[02] VERIFIED. REMOVED DAMAGED CORNER SCUFF PLATE AND INSTALLED NEW SERVICEABLE CORNER SCUFF PLATE PER AMM 53-11-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 26,231 hrs · 13,036 cycles

INTERCOSTAL AT STA 947 TO STA 967; LBL 51 HAS CORROSION AT LAV MOUNT.<[01] BLENDED CORROSION ON INTERCOSTAL STA. 947+1; LBL 51' PER SRM 51-10-02. REMOVED .010' OF MATERIAL AT THE DEEPEST POINT, REMAINING THICKNESS IS .070'. DAMAGE REMOVAL WAS FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. REMOVED DAMAGED INTERCOSTAL AT STA. 947 TO 967 LBL 51 PER SRM 51-40-02. LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-05. INSTALLED FOUR BONDED NUTPLATES TO INTERCOSTAL. IAW SRM 51-40-10-2R-0.

Part: CHANNEL — CRACKED (ZONE 400) · airframe 26,231 hrs · 13,036 cycles

#1 ENGINE I/B COWL; INTERCOSTAL CHANNEL CRACKED AFT OF ENGINE OIL ACCESS DOOR.<[01] #1 I/B FAN COWL REPLACED ON 7111-E-17063-NG (REP - RIGHT-HALF FAN COWL ASSEMBLY) [TTG8Q00S5HJF] LINE# 19;[02] C/W INSPECTION

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 26,231 hrs · 13,036 cycles

THE INTERCOSTAL AT LBL 24 BETWEEN BS 927 AND 947 HAS EVIDENCE OF CORROSION ON THE AFT END. UNABLE TO ASCERTAIN IF THE LOWER SURFACE OF THE 947 FRAME UPPER FLANGE IS AFFECTED. REMOVED ANGLE FROM WEB BETWEEN BS 927 TO STA. 947 AT LBL 24 IAW SRM 51-40-02. BLENDED CORROSION PER SRM 51-10-02. REMOVED .014 OF MATERIAL. REMAINING THICKNESS IS .049. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1.

Part: MOUNT — CORRODED (ZONE 200) · airframe 26,231 hrs · 13,036 cycles

AT STATION 947 RBL 51 THERE IS EVIDENCE OF CORROSION ON THE FWD SIDE OF THE FRAME AT THE LAVATORY MOUNT. BLENDED CORROSION ON THE FWD FLANGE OF THE UPPER CHORD ON FLOORBEAM STA. 947 PER SRM 51-10-02. REMOVED .039' OF MATERIAL. REMAINING THICKNESS IS .141'. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1. REMOVED DAMAGED ON TOP SIDE OF UPPER FLANGE OF FLOORBEAM 947.5 FROM RBL 49.5 TO RBL 51; IAW SRM 53-70-51-2R-8 ALTERNATIVE 3. REMOVED DAMAGED ON TOP SIDE OF UPPER FLANGE OF FLOORBEAM 947.5 FROM RBL 49.5 TO RBL 51; IAW SRM 53-70-51-2R-8 ALTERNATIVE 3. REMOVED AN ADDITIONAL 0.002 INCH OF MATERIAL IN BLENDED AREA AND FLAP PEENED THE BLENDED AREA ALL IAW SRM 53-70-51-2R-8 ALTERNATIVES 3.;[07] 6. REMOVED AN ADDITIONAL 0.002 INCH OF MATERIAL IN BLENDED AREA AND FLAP PEENED THE BLENDED AREA ALL IAW SRM 53-70-51-2R-8 ALTERNATIVES 3. INSPECTED.;[08] RII: FABRICATED SHIM PER SRM 53-70-51-2R-8 ALTERNATIVE 3.;[09] VERIFIED WORK IN C/A #8; FABRICATED SHIM PER SRM 53-70-51-2R-8 ALTERNATIVE 3. (RII);[10] ALODINED AND PRIMED REPAIR PART AND REWORK AREA PER SRM 51-20-01; AND SOPM 20-41-0INSTALLED REPAIR PARTS PER SRM 53-70-51-2R-8; ALTERNATIVE 3.

Part: ANGLE — CORRODED (ZONE 100) · airframe 26,231 hrs · 13,036 cycles

FORWARD CARGO COMPARTMENT LH TRANSITION ANGLE HAS CORROSION AT STA 500A-500B LBL 24<[01] BLENDED AREAS; REMOVED .030' MATERIAL AT 2 FASTENER HOLES; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] CUT OUT DAMAGE SECTION OF TRANSITION ANGLE FROM STA 480+10 TO 500A+10 PER SRM 53-30-53-2R-5;[03] INSPECTED WORK ABOVE;[04] INSTALLED REPAIR SECTION PER SRM 53-00-53-2R-5 AND EA M-22-153-01550.;[05] VERIFIED WORK COMPLETED.

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 26,231 hrs · 13,036 cycles

FORWARD CARGO COMPARTMENT STRINGER CLIP IS CRACKED AT STA 500I STR 26R<[01] REMOVED CRACKED STRINGER CLIP ; LOCATED AND DRILLED NEW CLIP PER SRM 51-40-02.;[02] INSTALLED THE NEW STRINGER CLIP PER SRM 51-40-02-0G-0-B00069.;[03] VERIFIED WORK SIGNED IN CA# 2.........INSTALLED THE NEW STRINGER CLIP PER SRM 51-40-02-0G-0-B00069. RII

Part: ANGLE — CORRODED (ZONE 100) · airframe 26,231 hrs · 13,036 cycles

FORWARD CARGO COMPARTMENT RH TRANSITION ANGLE HAS CORROSION AT STA 500E-500F RBL 25<[01] REMOVED SURFACE CORROSION ON FORWARD CARGO RH TRANSITION ANGLE. MATERIALS REMAINING THICKNESS .035 IS FOUND TO BE OUT OF LIMED PER SRM 53-00-53-1A-2<BR>SEE WORKS CAPTURE # TTG8Q00X4GPG FOR REPLACEMENT OF RH TRANSITION ANGLE FORM STA 500A TO 500I;[02] INSPECTED WORK ABOVE

Part: SEAL — CRACKED (ZONE 300) · airframe 26,231 hrs · 13,036 cycles

RIGHT HORIZONTAL STAB UPPER FWD SLIDER SEAL IS CRACKED.<[01] R&R?D R/H HORIZONTAL STAB UPPER FWD SLIDER SEAL IAW AMM 53-31-31.;[02] 02 - INSPECTED PER [AMM 53-31-31-401 CONFIG 1-NG (STABILIZER TO BODY FRONT SPAR SLIDING SEAL - REMOVAL/INSTALLATION - PERMANENT)]

Part: HANDLE — SEIZED (ZONE 800) · airframe 26,231 hrs · 13,036 cycles

LEFT HAND AFT EMERGENCY EXIT DOOR HANDLE BEARING SEIZED LEFT HAND AFT EMERGENCY EXIT DOOR HANDLE BEARING SEIZED.<[01] R&R'D HANDLE ASSEMBLY PER AMM 52-22-51.;[02] INSPECTED C/A 1.

Part: HANDLE — SEIZED (ZONE 800) · airframe 26,231 hrs · 13,036 cycles

LEFT HAND FWD EMERGENCY EXIT DOOR HANDLE BEARING SEIZED. R&R HANDLE ASSEMBLY PER AMM 52-22-51.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 26,231 hrs · 13,036 cycles

L/H A/C BAY STA 663 ANGLE TO VAPOR BARRIER CRACKED AT FASTENER HOLE<[01] REMOVED DAMAGED L/H VAPOR BARRIER ANGLE FOR REPLACEMENT PER SRM 51-40-02.;[02] ACCOMPLISHED HFEC HOLE PROBE INSPECTION OF REPAIR AREA PER NDT PART 6 51-00-00 PROC. 16 NO DEFECTS NOTED;[03] LOCATED AND DRILLED NEW L/H VAPOR BARRIER ANGLE AT STA.663 PER SRM 51-40-05. OK TO INSTALL REPLACEMENT PART PER SRM 51-40-02.;[04] INSPECTED WORK ABOVE;[05] OK TO INSTALL;[06] INSTALLED FASTENERS IN NEW L/H VAPOR BARRIER ANGLE INSIDE FUEL CELL ONLY PER SRM 51-40-02.;[07] INSPECTED WORK ABOVE;[08] CAP SEALED L/H VAPOR BARRIER FUEL TANK FASTNERS INSIDE FUEL CELL PER SRM 51-40-02;[09] VERIFIED ALL L/H VAPOR BARRIER FUEL TANK FASTNERS INSIDE FUEL CELL ARE CAP SEALED. SIGN OFF FOR CORRECTIVE ACTION #8.;[10] REMOVED AND REPLACED ANGLE PER SRM 51-40-02. REF CORRECTIVE ACTIONS 1 THRU 9.;[11] C/W INSPECTION OF C/A #8;[12] C/A #11 IS WRITTEN IN ERROR. SEE STEP #13 FOR PROPER SIGN OFF.;[13] C/W INSPECTION OF C/A #10;[14] FUEL LEAK CHECKS WERE ACCOMPLISHED ON L/H AND R/H A/C BAY STA 663 ANGLE TO VAPOR BARRIER FASTENERS TO FUEL TANK REQUIRE FUEL LEAK CHECK. REF TTG8Q00X2BKZ AND TTG8Q00X2B2K. [TTG8Q00XD6UZ;[15] INSP VERIFIED FUEL LEAK CHECK C/W ON TTG8Q00XD6UZ.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 26,231 hrs · 13,036 cycles

RIGHT A/C BAY STA 663 ANGLE TO VAPOR BARRIER 2 CRACKS AT FASTENER HOLES. REMOVED DAMAGED R/H VAPOR BARRIER ANGLE FOR REPLACEMENT PER SRM 51-40-02. ACCOMPLISHED HFEC HOLE PROBE INSPECTION OF REPAIR AREA PER NDT PART 6 51-00-00 PROC. 16 NO DEFECTS NOTED. DRILLED NEW ANGLE PER SRM 51-40-05. MATCH REPLACEMENT ANGLE OFF OF TEMPLETE AND TREATED AND PRIMED SRM 51-40-02 AND SRM 51-20-01 AND SRM 51-40-05. INSTALLED RH VAPOR BARRIER ANGLE FASTNERS INSIDE FUEL CELL AND CAP SEALED RH FUEL TANK FASTENERS INSIDE FUEL CELL. PER SRM 51-40-02. VERIFIED R/H VAPOR BARRIER ANGLE FASTNERS INSTALLATION THROUGH FUEL CELL AND CAP SEALED ALL FASTENERS IN FUEL CELL. INSTALLED FASTENER ON RH VAPOR BARRIER ANGLE ON VERTICAL SIDE OF ANGLE ONLY PER SRM 51-40-02. INSTALLED FASTENER ON RH VAPOR BARRIER ANGLE ON HORIZONTAL SIDE FROM STA RBL 7 -RBL 48 PER SRM 51-40-02 REMOVED AND REPLACED ANGLE PER SRM 51-40-02.

Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 26,062 hrs · 12,944 cycles

EMERGENCY LIGHTS ROW 17DEF AND 21DEF INOP.<[01] R/R EMERGENCY LIGHT BATTERY PACK AND BATTERY CHARGER FOR ROWS 17DEF AND 21DEF PER 33-51-06-960-805 AND 33-51-06-960-804.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 26,062 hrs · 12,944 cycles

EMERGENCY LIGHTS ROW 17DEF AND 21DEF INOP.<[01] R/R EMERGENCY LIGHT BATTERY PACK AND BATTERY CHARGER FOR ROWS 17DEF AND 21DEF PER 33-51-06-960-805 AND 33-51-06-960-804.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 25,988 hrs · 12,904 cycles

AFT R/H SECTION OF EMERGENCY LIGHTS INOP.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-200-801-NG (POWER SUPPLY - BATTERY PACK CAPACITY CHECK - PERMANENT)]

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 25,988 hrs · 12,904 cycles

ADDING PARTS INFORMATION FOR 'RH AFT EMERGENCY LIGHTS INOP'<[01] ADDED PARTS INFORMATION AS REQUIRED.

Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 25,839 hrs · 12,821 cycles

2 EMERGENCY LIGHTS ON R/H SIDE OF A/C AFT OF WING INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER (M1671) AS PER AMM 33-51-06. OPS CHECK IS GOOD.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 25,719 hrs · 12,759 cycles

EMERGENCY LIGHTS SUPPLIED BY M1670 DO NOT ILLUMINATE AFTER CHARGE<[01] REMOVED AND REPLACED M1670 CHARGER ASSY AND BATTERY PACK REF AMM 33-51-06.

Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 25,719 hrs · 12,759 cycles

EMERGENCY LIGHTS SUPPLIED BY M1670 DO NOT ILLUMINATE AFTER CHARGE<[01] REMOVED AND REPLACED M1670 CHARGER ASSY AND BATTERY PACK REF AMM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 25,688 hrs · 12,741 cycles

EMER. LIGHT AT L2 DOOR INOP. REMOVED AND REPLACED PER [AMM 33-51-06-960-806-NG (POWER SUPPLY - POWER SUPPLY REPLACEMENT - PERMANENT)]ALSO REPLACED BATTERY PACK OPSCHECKED GOOD

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 25,185 hrs · 12,471 cycles

FWD L/H EMERGENCY LIGHT BATTERY DISCHARGED.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY REF BOEING 737 AMM 33-51-06. OPS CHECKED GOOD.

Part: FLASHLIGHT — UNKNOWN (FWD CABIN) · airframe 24,865 hrs · 12,292 cycles

FWD FA EMERGENCY FLASHLIGHT INOP<[01] OPS CHECK NORMAL REF M/M 25-64-00

Part: SHUTOFF VALVE — MALFUNCTIONED (ENGINE) · airframe 24,475 hrs · 12,067 cycles

ACFT DEPARTED BLEEDS OFF. GOT CABIN ALTITUDE WARNING AT 12;500. PERFORMED QRH STEPS IMMEDIATE ACTION. BLEEDS TURNED ON. CABIN PRESSURIZATION IN MANUAL. OUTFLOW VALVE AND VSI RESPONDED CORRECTLY. CABIN ALTITUDE SHOWED 25000 FT AT 11000FT. CABIN DIFFERENTIAL AT 8.8 CAPT AND FO USED O2<[01] PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-81; FOUND NO DISCREPANCIES. PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-91 AND PACK CONFIDENCE PER MT 734-00-03. FOUND ENG 2 BLEED PRESSURE TO BE LOW AT IDLE (10 PSI). FOUND ENG 2 PRSOV; HSR; AND RH PRECOOLER SENSE LINE LEAKING. R+R #2 PRSOV PER AMM 36-11-04. R+R #2 HSR PER AMM 36-11-07. R+R RIGHT PRECOOLER SENSE LINE PER SIP. OPS AND LEAK CHECKS GOOD. PACK CONFIDENCE CHECK PASS. PERFORMED BITE TEST OF CPC?S FOUND FAULTS 30 AND 58 IN HISTORY. FAULT?S WERE SET DURING MANUAL OVERRIDE OF OUTFLOW VALVE. SUSPECT OPERATOR ERROR. CPC?S BITE SYSTEM TEST PASS. NO OTHER FAULTS FOUND. OK FOR SERVICE.

Part: SHUTOFF VALVE — MALFUNCTIONED (ENGINE) · airframe 24,475 hrs · 12,067 cycles

ACFT DEPARTED BLEEDS OFF. GOT CABIN ALTITUDE WARNING AT 12;500. PERFORMED QRH STEPS IMMEDIATE ACTION. BLEEDS TURNED ON. CABIN PRESSURIZATION IN MANUAL. OUTFLOW VALVE AND VSI RESPONDED CORRECTLY. CABIN ALTITUDE SHOWED 25000 FT AT 11000FT. CABIN DIFFERENTIAL AT 8.8 CAPT AND FO USED O2<[01] PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-81; FOUND NO DISCREPANCIES. PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-91 AND PACK CONFIDENCE PER MT 734-00-03. FOUND ENG 2 BLEED PRESSURE TO BE LOW AT IDLE (10 PSI). FOUND ENG 2 PRSOV; HSR; AND RH PRECOOLER SENSE LINE LEAKING. R+R #2 PRSOV PER AMM 36-11-04. R+R #2 HSR PER AMM 36-11-07. R+R RIGHT PRECOOLER SENSE LINE PER SIP. OPS AND LEAK CHECKS GOOD. PACK CONFIDENCE CHECK PASS. PERFORMED BITE TEST OF CPC?S FOUND FAULTS 30 AND 58 IN HISTORY. FAULT?S WERE SET DURING MANUAL OVERRIDE OF OUTFLOW VALVE. SUSPECT OPERATOR ERROR. CPC?S BITE SYSTEM TEST PASS. NO OTHER FAULTS FOUND. OK FOR SERVICE.

Part: SENSE LINE — LEAKING (PRECOOLER) · airframe 24,475 hrs · 12,067 cycles

ACFT DEPARTED BLEEDS OFF. GOT CABIN ALTITUDE WARNING AT 12;500. PERFORMED QRH STEPS IMMEDIATE ACTION. BLEEDS TURNED ON. CABIN PRESSURIZATION IN MANUAL. OUTFLOW VALVE AND VSI RESPONDED CORRECTLY. CABIN ALTITUDE SHOWED 25000 FT AT 11000FT. CABIN DIFFERENTIAL AT 8.8 CAPT AND FO USED O2<[01] PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-81; FOUND NO DISCREPANCIES. PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-91 AND PACK CONFIDENCE PER MT 734-00-03. FOUND ENG 2 BLEED PRESSURE TO BE LOW AT IDLE (10 PSI). FOUND ENG 2 PRSOV; HSR; AND RH PRECOOLER SENSE LINE LEAKING. R+R #2 PRSOV PER AMM 36-11-04. R+R #2 HSR PER AMM 36-11-07. R+R RIGHT PRECOOLER SENSE LINE PER SIP. OPS AND LEAK CHECKS GOOD. PACK CONFIDENCE CHECK PASS. PERFORMED BITE TEST OF CPC?S FOUND FAULTS 30 AND 58 IN HISTORY. FAULT?S WERE SET DURING MANUAL OVERRIDE OF OUTFLOW VALVE. SUSPECT OPERATOR ERROR. CPC?S BITE SYSTEM TEST PASS. NO OTHER FAULTS FOUND. OK FOR SERVICE.

Part: RADOME — OUT OF LIMITS (NOSE) · airframe 23,764 hrs · 11,697 cycles

NOSE RADOME OUT OF LIMITS<[01] RR NOSE RADOME ASSY PER AMM 53-52-00.

Part: DOUBLER — CRACKED (ZN 100 FUS LOWER) · airframe 23,473 hrs · 11,537 cycles

23-153-03732-TLD (N8523W - SWA - REPAIR - EXTERNAL GROUND POWER RECEPTACLE DOOR SURROUND DOUBLER BENT AND CRACKED AT LOWER TAB - PERMANENT)<[01] REMOVED DAMAGE PER SRM 52-10-15-2R-4;[02] ACCOMPLISHED HFEC INSPECTION OF CUTOUT PER 737 NDT MANUAL PART 6 51-00-00 FIG 23. NO DEFECTS NOTED;[03] PERFORMED REPAIR OF THE EGPR CUT OUT. IAW SRM53-10-15-2R-4

Part: DOUBLER — CRACKED (ZN 100 FUS LOWER) · airframe 23,226 hrs · 11,391 cycles

EXTERNAL POWER DOOR WILL NOT SIT FLUSH<[01] REMOVED AND REPLACED LOWER LATCH AND FOUND LOWER DOOR SURROUND DOUBLER BENT AND CRACKED. PERFORMED EA 23-153-03732. OK TO CONTINUE AS TLD

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 22,305 hrs · 10,846 cycles

AFT LEFT IB FLASHLIGHT INOP. R & R FLASHLIGHT BATTERY IAW AMM 25-64-00 OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 21,079 hrs · 10,132 cycles

LH FWD EXTERIOR EMERGENCY LAMP INOP<[01] R/R LH SLIDE EMERGENCY LAMP PER AMM 33-51-04 OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 21,079 hrs · 10,132 cycles

RH SLIDE EMERGENCY LIGHT INOP<[01] R/R RH SLIDE EMERGENCY LAMP PER AMM 33-51-04 OPS CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,662 hrs · 9,324 cycles

FWD ENTRY AND FWD SERVICE DOOR EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED 2 EA. BATTERY PACKS. EMERGENCY LIGHTS TEST NORMAL IAW AMM 33-51-06.

Part: WEB — CORRODED (BS 847-867) · airframe 19,661 hrs · 9,323 cycles

AFT CARGO RT SIDE THRESHOLD WEB WAS CORRODED BS 847 - 867. REMOVED CORROSION AND FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2. LOCATED, DRILLED, AND INSTALLED A NEW THRESHOLD WEB IAW SRM 51-40-02.

Part: STRAP — CORRODED (BS 770) · airframe 19,661 hrs · 9,323 cycles

AFT CARGO FLOOR PANEL ATTACH STRIP HAD CORROSION AT BS 770. REMOVED AND REPLACED THE TEE FITTING ASSY IAW SRM 51-40-02. REMOVED AND REPLACED THE FLOOR PANEL STRAP IAW SRM 51-40-02.

Part: ANGLE — CORRODED (BS 767-807) · airframe 19,661 hrs · 9,323 cycles

AFT CARGO RIGHT SIDE TRANSITION ANGLE WEB FORWARD OF DOOR WAS CORRODED BS 767 - 807. REMOVED CORROSION AND FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED THE SHIELD, INSTALLED RIVETS IAW SRM 51-40-01.

Part: ATTACH ANGLE — CRACKED (BS 967) · airframe 19,661 hrs · 9,323 cycles

AFT CARGO LEFT SIDE BS 867 ATTACH ANGLE CRACKED AT LOWER FRAME LAVATORY POST. LOCATED, DRILLED, AND INSTALLED A NEW ATTACH ANGLE IAW SRM 51-40-02.

Part: ANGLE — CORRODED (BS 500A-500I) · airframe 19,661 hrs · 9,323 cycles

FORWARD CARGO BAY RT TRANSITION ANGLE, BS 500A-500I, RBL-24, HAD NUMEROUS AREAS OF CORROSION. REMOVED AND REPLACED THE RT TRANSITION ANGLE IAW SRM 51-40-02.

Part: ANGLE — CORRODED (BS 500A-500I) · airframe 19,661 hrs · 9,323 cycles

FORWARD CARGO BAY, RT FLOOR TRANSITION ANGLE, BS 500A-500I, RBL 24, HAS NUMEROUS AREAS OF CORROSION. REMOVED AND REPLACED THE R/H TRANSITION ANGLE IAW SRM 51-40-02.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 19,661 hrs · 9,323 cycles

CABIN FLOORBOARD 241AF WAS DENTED AND PEELING FIBERS. R & R FLOORBOARD IAW AMM 53-21-00.

Part: WEB — CRACKED (RT NACELLE) · airframe 19,662 hrs · 9,324 cycles

NR 2 ENGINE OTBD. FAN COWL, STRUCTURE BELOW HOLD OPEN ROD CRACKED. REMOVED AND REPLACED THE WEB IAW SRM 51-40-02.

Part: ANGLE — CORRODED (BS 727H-727J) · airframe 19,661 hrs · 9,323 cycles

AFT CARGO, BS 727H-727J, RT TRANSITION ANGLE WAS CORRODED AROUND NUT-PLATE HOLES. CUT OUT SECTION OF THE TRANSITION ANGLE IAW SRM 53-00-53-2R-5. LOCATED AND DRILLED A NEW TRANSITION ANGLE IAW SRM 53-00-53-2R-5. TREATED AND PRIME IAW SRM 53-00-53-2R-5. INSTALLED THE REPAIR IAW SRM 53-00-53-2R-5.

Part: ANGLE — CORRODED (BS 727J-767) · airframe 19,661 hrs · 9,323 cycles

AFT CARGO, BS 727J-767, LT TRANSITION ANGLE WAS CORRODED AROUND NUT-PLATE HOLES. CUT OUT SECTION OF THE LT TRANSITION ANGLE BS 727B+10-757 IAW SRM 53-00-53-2R-5. LOCATED, DRILLED, TREATED, AND PRIMED A NEW SECTION OF TRANSITION ANGLE, AND REPAIR SPLICES IAW SRM 53-00-53-2R-5, INSTALLED REPAIR IAW SRM 53-00-53-2R-5.

Part: STRAP — CORRODED (BS 727I) · airframe 19,661 hrs · 9,323 cycles

AFT CARGO BS 727I+5, FLOOR PANEL SUPPORT STRAP WAS CORRODED AROUND NUT-PLATE HOLES. REMOVED & REPLACED THE STRAP IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (RT NACELLE) · airframe 19,661 hrs · 9,323 cycles

CRACKED INTERCOSTAL AT OIL SERVICE DOOR OPENING, RIGHT OUTBOARD FAN COWL. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02.

Part: HANDLE — LOOSE (R1 DOOR) · airframe 19,661 hrs · 9,323 cycles

FWD SERVICE DOOR (R-1) INTERIOR HANDLE HAS PLAY AT CAM PLATE. / [01] REMOVED AND REPLACED FWD GALLEY SERVICE DOOR WASHERS UNDER DOOR HANDLE CAM PLATE PER AMM 52-41-11.

Part: PANEL — PULLED (RT NACELLE) · airframe 19,661 hrs · 9,323 cycles

NR 2 ENGINE HAS CRACKED LOUVERED PANEL AT 1 O'CLOCK BLEED AIR VALVE. SCREW IS PULLED THROUGH PANEL. REPLACED THE PANEL IAW AMM 72-23-07.

Part: FLOOR SUPPORT — CRACKED (BS 540 RBL 1) · airframe 19,661 hrs · 9,323 cycles

FLOOR SUPPORT RBL 1 CRACKED AT BS 540. REMOVED AND REPLACED IAW SRM. 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 540 LBL1) · airframe 19,661 hrs · 9,323 cycles

FLOOR SUPPORT, LBL 1 FOUND CRACKED AT BS 540. REMOVED AND REPLACED IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (LT WING TE) · airframe 19,661 hrs · 9,323 cycles

LT WING UPPER TRAILING EDGE PANEL BETWEEN NR 5 AND 6 SPOILER, ATTACH ANGLE CRACKED. REMOVED THE DAMAGED ATTACH ANGLE IAW SRM 51-40-02. MATCH DRILLED THE NEW ANGLE IAW SRM 51-40-05. INSTALLED A NEW ATTACH ANGLE IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (LT WING TE) · airframe 19,661 hrs · 9,323 cycles

LEFT WING TRAILING EDGE. UPPER FIXED TRAILING EDGE PANEL, INBD OF DEFLECTION RIB. LOWER SUPPORT BRACKET FOUND CRACKED ON THE OTBD UPPER FLANGE. REMOVED DAMAGED SUPPORT BRACKET IAW SRM 51-40-02. MATCH DRILLED A NEW SUPPORT BRACKET IAW SRM 51-40-05. PREFORMED NDT PART 6 51-00-00 PROCEDURE. HFEC INSPECTION ON DAMAGE CUT OUT, NO FAULTS FOUND. PREFORMED NDT PART 6 51-00-00 PROCEDURE 16, HFEC OPEN HOLE INSPECTION ON MATCH DRILLED SUPPORT BRACKET, NO FAULTS FOUND. INSTALLED FASTENERS TO LOWER SUPPORT BRACKET IAW SRM 51-40-02. REMOVED AND REPLACED LEFT WING TRAILING EDGE. UPPER FIXED TRAILING EDGE PANEL, INBOARD OF DEFLECTION RIB. LOWER SUPPORT BRACKET IAW SRM 51-40-02

Part: BRACKET — CRACKED (RT WING TE) · airframe 19,661 hrs · 9,323 cycles

RIGHT WING T/E BRACKET UNDER FIXED T/E PANEL INBD OF DEFLECTION CONTROL RIB HAS CRACK THRU RIVET HOLE O/B SIDE. REMOVED THE CRACKED BRACKET IAW SRM 51-40-02. MATCHED DRILLED A NEW BRACKET IAW SRM 51-40-05. INSTALLED THE NEW BRACKET IAW SRM 51-40-02.

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 19,661 hrs · 9,323 cycles

INBD OF THE AFT LEFT LAVATORY, EMERGENCY EXIT LIGHT ON THE AISLE WALL IS BLANK.

Part: NONE — INOPERATIVE (R/H OVERWING EXI) · airframe 19,354 hrs · 9,154 cycles

EMERGENCY EXIT SIGN LIGHT ASSY FWD OF RIGHT FWD OVER WING EMERGENCY EXIT DOOR INOP / [01] REMOVED AND REPLACED BATTERY PACK CHARGER ASSY. AT M1695 IAW M/M 33-51-06

Part: NONE — INOPERATIVE (L/H OVERWING DOO) · airframe 19,354 hrs · 9,154 cycles

EMERGENCY EXIT SIGN LIGHT ASSY FWD OF LEFT FWD OVER WING EMERGENCY EXIT DOOR INOP / [01] REMOVED AND REPLACED M1694 EMERGENCY LIGHTS CHARGER PACK ASSY PER AMM 33-51-06 AND REPLACED EMERGENCY EXIT LIGHT ASSY PER AMM 33-51-01

Part: NONE — INOPERATIVE (L/H OVERWING DOO) · airframe 19,354 hrs · 9,154 cycles

EMERGENCY EXIT SIGN LIGHT ASSY FWD OF LEFT FWD OVER WING EMERGENCY EXIT DOOR INOP / [01] REMOVED AND REPLACED M1694 EMERGENCY LIGHTS CHARGER PACK ASSY PER AMM 33-51-06 AND REPLACED EMERGENCY EXIT LIGHT ASSY PER AMM 33-51-01

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 18,396 hrs · 8,608 cycles

FWD FLASH LIGHT INOP / [01] R&R FWD F/A FLASH LIGHT ASSY REF AMM 25-64-00 OPS CK GOOD

Part: FLASHLIGHT — INOPERATIVE (PAX CABIN) · airframe 18,101 hrs · 8,431 cycles

FWD FLT ATTENDANT JUMPSEAT EMERGENCY FLASHLIGHT INDICATOR LIGHT IS BLINKING RED / [01] R/R FWD OTB EMERGENCY FLASHLIGHT BATTERY REF 25-64-00

Part: MEGAPHONE — INOPERATIVE · airframe 17,296 hrs · 7,990 cycles

AFT F/A MEGAPHONE INOP / [01] REPLACED MEGAPHONE AND OPERATION TEST IAW AMM 25-64-00. NO FURTHER DEFECTS NOTED. A/C OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (AFT CABIN) · airframe 16,843 hrs · 7,737 cycles

ONE AFT RIGHT EMERGENCY FLASHLIGHT INOP ; / [01] R & R AFT R/H FLASHLIGHT BATTERY <BR>PER AMM 25-64-00.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 16,553 hrs · 7,582 cycles

RIGHT ENGINE AFT STRUT FAIRING ASSEMBLY CRACKED AT THE FORWARD INBOARD FLANGE. FAIRING ASSEMBLY PART NUMBER 313A2752-1 ; / [01] EA 21-154-03780; [02] REPAIRED PER EA 21-154-03780

Part: FLOOR PANEL — CRACKED (FWD CARGO)

FWD CARGO PANEL 121ZCC HAS 3 CRACKS 1' LONG 21' FROM FRONT EDGE; 2' LONG 32' FROM FRONT EDGE AND 3' LONG 14' FROM AFT EDGEPERFORMED INTERIM REPAIR ON PANEL 121ZCC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPANT PANEL. PERMANTENT ACTION REQUIRED / REMOVED AND REPLACED CARGO PANEL 121ZCC PER AMM 25-52-09AMT 102665

Part: FLOOR PANEL — CRACKED (FWD CARGO)

FWD CARGO PANEL 120ZAC HAS A CRACK 5' LONG 18' FROM LH EDGEPERFORMED INTERIM REPAIR ON PANEL 120ZAC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPENT PANEL. PERMANENT ACTION REQUIRED / REMOVED AND REPLACED CARGO PANEL 120ZAC PER AMM 25-52-09AMT 102665

Part: FLOOR PANEL — CRACKED (FWD CARGO)

FWD CARGO PANEL 121ZDC HAS 2 CRACKS 3' LONG 36' FROM AFT EDGE AND 24' LONG 8' FROM FRONT EDGE PERFORMED INTERIM REPAIR ON PANEL 121ZDC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPANT PANEL. PERMANENT ACTION REQUIRED / REMOVED AND REPLACED CARGO PANEL 121ZDC PER AMM 25-52-0AMT 102665

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 13,888 hrs · 6,219 cycles

FWD CARGO PANEL 120ZEC HAS A CRACK 3' LONG 24' FROM LH EDGE PERFORMED INTERIM REPAIR ON PANEL 120ZEC PER EA1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FUTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPANT PANEL. REPETITIVE ACTION REQUIRED /

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 13,888 hrs · 6,219 cycles

FWD CARGO PANEL 122ZCC HAS A CRACK 8' LONG 2' FROM AFT EDGE PERFORMED INTERIM REPAIR ON PANEL 122ZCC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPANT PANEL. REPETITIVE ACTION REQUIRED /

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 13,888 hrs · 6,219 cycles

FWD CARGO PANEL 122ZFC HAS A CRACK 2' LONG 32' FROM AFT EDGE PERFORMED INTERIM REPAIR ON PANEL 122ZFC PER EA 1-A25-3722 REV. 4. EVERY 8 DAYS PERFORM DETAILED VISUAL INSPECTION OF THE REPARRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FUTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPANT PANEL. REPETITIVE ACTION REQUIRED /

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 13,888 hrs · 6,219 cycles

FWD CARGO PANEL 121ZCC HAS 3 CRACKS 1' LONG 21' FROM FRONT EDGE; 2' LONG 32' FROM FRONT EDGE AND 3' LONG 14' FROM AFT EDGEPERFORMED INTERIM REPAIR ON PANEL 121ZCC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPANT PANEL. REPETITIVE ACTION REQUIRED /

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 13,888 hrs · 6,219 cycles

FWD CARGO PANEL 121ZDC HAS 2 CRACKS 3' LONG 36' FROM AFT EDGE AND 24' LONG 8' FROM FRONT EDGE PERFORMED INTERIM REPAIR ON PANEL 121ZDC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPANT PANEL. REPETITIVE ACTION REQUIRED /

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 13,888 hrs · 6,219 cycles

FWD CARGO PANEL 122ZEC HAS A CRACK 18' LONG 1' FROM AFT EDGE. PERFORMED INTERIM REPAIR ON PANEL 122ZEC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R &R THE DISCREPANT PANEL. REPETITIVE ACTION REQUIRED /

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 13,888 hrs · 6,219 cycles

FWD CARGO PANEL 120ZAC HAS A CRACK 5' LONG 18' FROM LH EDGEPERFORMED INTERIM REPAIR ON PANEL 120ZAC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPENT PANEL. REPETITIVE ACTION REQUIRED /

Part: PANEL — CRACKED (FWD CARGO BAY) · airframe 13,857 hrs · 6,203 cycles

FWD CARGO PANEL 120ZEC HAS A CRACK 3' LONG 24' FROM LH EDGE PERFORMED INTERIM REPAIR ON PANEL 120ZEC PER EA1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FUTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPANT PANEL. REPETITIVE ACTION REQUIRED.

Part: PANEL — CRACKED (FWD CARGO BAY) · airframe 13,857 hrs · 6,203 cycles

FWD CARGO PANEL 122ZFC HAS A CRACK 2' LONG 32' FROM AFT EDGE PERFORMED INTERIM REPAIR ON PANEL 122ZFC PER EA 1-A25-3722 REV. 4. EVERY 8 DAYS PERFORM DETAILED VISUAL INSPECTION OF THE REPARRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FUTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPANT PANEL. REPETITIVE ACTION REQUIRED.

Part: PANEL — CRACKED (FWD CARGO BAY) · airframe 13,857 hrs · 6,203 cycles

FWD CARGO PANEL 122ZCC HAS A CRACK 8' LONG 2' FROM AFT EDGE PERFORMED INTERIM REPAIR ON PANEL 122ZCC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPANT PANEL. REPETITIVE ACTION REQUIRED.

Part: PANEL — CRACKED (CARGO COMPT) · airframe 13,857 hrs · 6,203 cycles

FWD CARGO PANEL 120ZAC HAS A CRACK 5' LONG 18' FROM LH EDGEPERFORMED INTERIM REPAIR ON PANEL 120ZAC PER EA 1A253722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPENT PANEL. REPETITIVE ACTION REQUIRED.

Part: PANEL — CRACKED (FUSELAGE) · airframe 13,857 hrs · 6,203 cycles

FWD CARGO PANEL 121ZCC HAS 3 CRACKS 1' LONG 21' FROM FRONT EDGE; 2' LONG 32' FROM FRONT EDGE AND 3' LONG 14' FROM AFT EDGEPERFORMED INTERIM REPAIR ON PANEL 121ZCC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPANT PANEL. REPETITIVE ACTION REQUIRED.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 13,857 hrs · 6,203 cycles

FWD CARGO PANEL 121ZDC HAS 2 CRACKS 3' LONG 36' FROM AFT EDGE AND 24' LONG 8' FROM FRONT EDGE PERFORMED INTERIM REPAIR ON PANEL 121ZDC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPANT PANEL. REPETITIVE ACTION REQUIRED /

Part: PANEL — CRACKED (FWD CARGO BAY) · airframe 13,857 hrs · 6,203 cycles

FWD CARGO PANEL 122ZEC HAS A CRACK 18' LONG 1' FROM AFT EDGE. PERFORMED INTERIM REPAIR ON PANEL 122ZEC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R &R THE DISCREPANT PANEL. REPETITIVE ACTION REQUIRED.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 10,213 hrs · 4,426 cycles

LT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED. / REMOVED & REPLACED LH UPPER SLIDER IAW 737 NG AMM 53-31-31.AMT 142757INSP 43511 (P44)

Part: LIGHT — LOOSE (CABIN) · airframe 6,784 hrs · 2,931 cycles

LT AFT LAV EXTERNAL EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSY PER MM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 4,754 hrs · 2,095 cycles

RT PHOTOLUMINESCENT STRIP DAMAGED AT ROW 1. R&R STRIP PER AMM.