N3756

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 77,698 hrs · 29,698 cycles

FWD GALLEY OVERHEAD EXIT LIGHT INOP. R & R BATTERY PACK AT FWD GALLEY PER AMM 33-51. OPS CHECK GOOD.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 76,394 hrs · 29,066 cycles

(LOG 1080752) CRACK WAS FOUND OF: 0.625IN LENGTH ON LH WINDOW FRAME RADIUS AREA. LH WINDOW FRAME WAS REPAIRED PER ER/A 619132-14ADTR REV. A.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 76,394 hrs · 29,066 cycles

(LOG 1079382) CRACK WAS FOUND OF: 0.375IN LENGTH ON RH WINDOW FRAME RADIUS AREA. RH WINDOW FRAME WAS REPAIRED PER ERA 619132-14ADTR REV. A.

Part: FRAME — NOT REPORTED (ZONE 200) · airframe 76,368 hrs · 29,052 cycles

(LOG 1077573) ACCOMPLISH AMDS 5311-01251-02A - LEFT HAND STA 727 FRAME INNER CHORD 737 REPAIR SECTION 02. ACCOMPLISHED AMDS 5311-01251-02A - LEFT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02.

Part: FRAME — NOT REPORTED · airframe 76,368 hrs · 29,052 cycles

(LOG 1077578) ACCOMPLISH AMDS 5311-01251-02B - RIGHT HAND STA 727 FRAME INNER CHORD 737 SECTION 02. ACCOMPLISHED AMDS 5311-01251-02B - RIGHT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02.

Part: RAIL — CORRODED (ZONE 100) · corrosion level 2 · airframe 76,368 hrs · 29,052 cycles

(LOG 1075683) CORROSION ON OUT OF LIMITS RAIL SUPPORTS OF BILGE AREA BTW STA 727D-727E, STA 767-787 RBL 3, 8 LBL 3. RAIL SUPPORTS OF BILGE AREA BTW STA 727D-727E, STA 767-787 RBL 3, 8 LBL 3 WERE REPAIRED PER B737-800 SRM 53-00-53-2R PROCEDURE 2, REPAIR 2.

Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 76,368 hrs · 29,052 cycles

(LOG 1073967) A.A.5714-01004-01: CRACK WAS FOUND OF 0.8IN OF LENGTH APPROX ON LH PRESSURE DECK WEB AT STA 663 BTW LBL 40 AND 45 AT WING BOX. CRACK ON LH PRESSURE DECK WEB AT STA 663 BTW LBL 40 AND 45 AT WING BOX REA WAS REPAIRED PER B737-800 SRM 57-10-10-2R-3 REPAIR 3.

Part: FRAME — DENTED (ZONE 100) · airframe 76,394 hrs · 29,066 cycles

(LOG 1074950) DENT ON FRAME STA 500B AND BTW S25L TO S26L AT FWD CARGO COMP. DENT ON FRAME STA 500B AND BTW S25L TO S26L AT FWD CARGO COMP WAS REPAIRED PER B737-800 SRM 53-30-07-2R PROCEDURE 1.

Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 76,368 hrs · 29,052 cycles

(LOG 1073925) CRACK WAS FOUND OF 0.8 IN OF LENGTH APPROX ON LH PRESSURE DECK WEB AT STA 663 BTW LBL 40 AND 45 AT WING BOX. CRACK ON LH PRESSURE DECK WEB AT STA 663 BTW LBL 40 AND 45 AT WING BOX REA WAS REPAIRED PER B737-800 SRM 57-10-10-2R-3 REPAIR 3.

Part: FRAME — DENTED (ZONE 100) · airframe 76,368 hrs · 29,052 cycles

(LOG 1074947) DENT ON FRAME STA 500B AND BTW S25L TO S26L AT FWD CARGO COMP. DENT ON FRAME STA 500B AND BTW S25L TO S26L AT FWD CARGO COMP WAS REPAIRED PER B737-800 SRM 53-30-07-2R

Part: FRAME — DENTED (ZONE 100) · airframe 76,368 hrs · 29,052 cycles

(LOG 1072894) DENT ON FRAME STA 460 AND BTW S24L TO S25L AT FWD CARGO COMP. DENT ON FRAME STA 460 AND BTW S24L TO S25L AT FWD CARGO WAS REPAIRED PER B737-800 SRM 53-30-07-2R PROCEDURE 2, REPAIR 2.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,368 hrs · 29,052 cycles

(LOG 1067984) CORROSION OUT OF LIMITS (UT) THICKNESS MEASUREMENT ON FLOOR BEAM STA 985 AT PASSENGER CABIN. CORROSION ON FLOOR BEAM STA 985 AT PASSENGER CABIN RBL46 TO RBL33 AND LBL42 TO LBL44 WAS REPAIRED PER ER/A 464736-14MA REV.A.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,368 hrs · 29,052 cycles

(LOG 1065025) CORROSION ON FLOOR BEAM STA 952 BTW RBL 55 TO RBL 45 AT PASSENGER CABIN. CORROSION ON FLOOR BEAM STA 952 BTW RBL 55 TO RBL 45 AT PASSENGER CABIN WAS REPAIRED PER B737-800 SRM 53-70-51-2R PROCEDURE 5 REPAIR 5.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 76,368 hrs · 29,052 cycles

(LOG 1065412) CORROSION ON INTERCOSTAL BTW STA 986-992 OVER S-20LH AT AFT CARGO COMPARTMENT. INTERCOSTAL BTW STA 986-992 OVER S-20LH AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLED PER B737-800 SRM 51-40-02-0G PAR 7.C AND DWG 147A8801 REV: M.

Part: FRAME — CRACKED (ZONE 200) · airframe 76,368 hrs · 29,052 cycles

(LOG 1060034) CRACK ON FRAME STA 400 STGR 8L AT PASSENGER CABIN. CRACK ON FRAME STA 400 STGR 8L AT PASSENGER CABIN WAS REPAIRED PER ER/A 627278-14AD REV. ORIGINAL.

Part: ATTACH ANGLE — CRACKED (ZONE 200) · airframe 76,368 hrs · 29,052 cycles

CRACK OF 0.600 IN ON ATTACH ANGLE AT THE DRAIN HOLE/SLOT RH SIDE BTW RBL 25 AND RBL 45. CRACK OF 0.600 IN ON ATTACH ANGLE AT THE DRAIN HOLE/SLOT RH SIDE BTW RBL25 AND RBL45 (REF. CARD 5714-01004-02 STEP 13) ASSOCIATED AA 5714-01004 ADDED FOR AC 3756.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,368 hrs · 29,052 cycles

(LOG 1049586) CORROSION ON Z ANGLE FLOOR SUPPORTS (2 EAS) BTW STA 992 LBL 43 AND RBL 43 AT PAX CABIN. Z ANGLE FLOOR SUPPORTS (2 EAS) BTW STA 992 LBL 43 AND RBL 43 AT PAX CABIN WERE REPLACED AND INSTALLED PER B 737-800 SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,368 hrs · 29,052 cycles

(LOG 1046337) CORROSION ON FLOOR SUPPORT STA 294 RBL14 AT CPAX. FLOOR SUPPORT STA 294 RBL14 AT CPAX WAS REPLACED AND INSTALLED PER B737-800 SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,368 hrs · 29,052 cycles

(LOG 1046016) CORROSION ON FLOOR SUPPORTS BTW STA 951 TO STA 985 LBL 16 ALSO STA 951 BTW RBL 18 TO RBL 47 AT PASSENGER CABIN. FLOOR SUPPORTS BTW STA 951 TO STA 985 LBL 16 ALSO STA 951 BTW RBL 18 TO RBL 47 AT PASSENGER CABIN WERE REPLACED AND INSTALLED PER B737-800 SRM 51-40-02-0G.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,368 hrs · 29,052 cycles

(LOG 1041697) CORRSION ON FLOOR FITTINGS STA 311 AND 344 LBL 54 AT CPAX. FLOOR FITTINGS STA 311 AND 344 LBL 54 AT CPAX WERE REPLACED AND INSTALLED PER B737-800 SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,368 hrs · 29,052 cycles

(LOG 1036291) CORROSION ON INTERCOSTAL BTW STA 951 TO STA 960 LBL 48 AT PASSENGER CABIN. INTERCOSTAL BTW STA 951 TO STA 960 LBL 48 AT PASSENGER CABIN WAS REPLACED AND INSTALLED PER B737-800 SRM 51-40-02-0G.

Part: ACCESS DOOR — OPEN (ZONE 100) · airframe 76,035 hrs · 28,908 cycles

(LOG 7063600) ON INITIAL CLIMBOUT, THE LANDING GEAR LEVER WAS UP, BUT LANDING GEAR WAS STILL DOWN. RAN THE QRH AND WE WERE ABLE TO PUT THE GEAR UP. DE-BRIEFED FLIGHT CREW, SUSPECT MAN GEAR EXT ACCESS DOOR WAS OPEN. AFTER DOOR WAS CYCLED WHEN QRH CHECKLIST WAS RUN, GEAR OPERATED NORMAL.

Part: PUMP — INOPERATIVE (LT FUEL BOOST) · airframe 75,763 hrs · 28,794 cycles

SHIP 3756 -DIV- DIVERTED TO IND DUE TO RT CENTER BOOST PUMP INOP WHILE LT CENTER BOOST PUMP ALREADY ON MEL. CORRECTIVE ACTION: APPLIED MEL FOR BOTH CENTER BOOST PUMPS AND ADDED FUEL. CONTINUED TO ATL. SUBSEQUENTLY REPLACED LT AND RT CENTER UFIS.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 74,775 hrs · 28,322 cycles

(LOG 6050972) DURING SERVICE CHECK FOUND ROW 20, 21, 22 SEAT MOUNTED EMERGENCY LIGHTS INOP. R/R BATTERY PACK FOR ROW 20, 21, 22 PER B737 AMM 33-51. OPS CHECK GOOD.

Part: ENGINE — FIRE (LT ENGINE) · airframe 73,939 hrs · 27,979 cycles

SHIP 3756 -FIRE- DURING TAXI ANOTHER AIRCRAFT REPORTED A SMALL FLAME FROM THE LEFT ENGINE EXHAUST PLUG. CORRECTIVE ACTION: PERFORMED HIGH POWER RUN AND INSPECTED EXHAUST AREA FOR OIL LEAKS WITH NO TROUBLE FOUND.

Part: WIRE HARNESS — FAULTED (ANTI ICE VALVE) · airframe 73,139 hrs · 27,628 cycles

SHIP 3756 -DIV- TO SLC DUE TO A NUMBER 2-ENGINE COWL VALVE OPEN LIGHT ILLUMINATING. CORRECTIVE ACTION: MAINTENANCE PERFORMED OPS TEST OF ANTI ICE VALVE AND SWITCH PANEL. OPS OK REPLACED HARNESS PER B 737 AMM 71-51.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,224 hrs · 27,232 cycles

SHIP 3756 -FCNT/DE- DECLARED EMERGENCY DUE TO TRAILING EDGE FLAPS LOCKED OUT ON APPROACH. CORRECTIVE ACTION: MAINTENANCE REPLACED #4 T GEARBOX PER B737 AMM 27-51.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 71,351 hrs · 26,848 cycles

(LOG 4600354) DURING SVC CK, FOUND EEPLS FROM ROW 23 TO ALL THE WAY BACK INOP. R+R'D BATTERY PACK PER AMM 33-51 AND OP CHECKS GOOD.

Part: LIGHT — INOPERATIVE · airframe 70,265 hrs · 26,334 cycles

(LOG 9498702) DURING INSPECTION FOUND SEAT ROW 18 EMERGENCY LIGHTS MISCONFIGURED PER S/C PAPERWORK. RPLCD LIGHT ASSY PER B737 AMM 33-51. OPS NML.

Part: HARNESS — DAMAGED · airframe 68,572 hrs · 25,569 cycles

(LOG 2423025) DURING INSPECTION FOUND SEAT 1C FLOOR PROXIMITY LIGHT INOP. FOUND HARNESS TO THE SEAT MOUNTED FLOOR PROXIMITY LIGHTS AT SEAT 1C WERE BROKEN. REMOVED AND REPLACED THE WIRE HARNESS TO THE PROXIMITY LIGHTS IN REF TO B737 AMM 33-51.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,856 hrs · 24,346 cycles

(LOG 8123420) DURING INSPECTION FOUND ROW 10-15 EMERGENCY LIGHTS INOPERATIVE. R/R BATTERY & CHARGER ASSY PER B737 AMM 33-51. OPS CHK NORMAL.

Part: TRUNNION — CORRODED (RT MLG) · corrosion level 2 · airframe 65,507 hrs · 24,216 cycles

(LOG 1890417) DURING INSPECTION FOUND INBD LOWER LUG FOR RMLG FWD TRUNNION H BLOCK: INBD FACE OF LUG PITTED. REPAIRED PER B737 SRM 57-20-90.

Part: TRUNNION — CORRODED (LT MLG) · corrosion level 2 · airframe 65,507 hrs · 24,216 cycles

(LOG 1890422) DURING INSPECTION FOUND LMLG UPR I/B FWD TRUNNION LUG CORROSION ON I/B AND O/B FACE. REPAIRED PER B737 SRM 57-20-90.

Part: BUSHING — WORN (LT MLG TRUNNION) · airframe 65,507 hrs · 24,216 cycles

(LOG 1890050) DURING INSPECTION FOUND LMLG LWR O/B FWD TRUNNION LUG WORN BUSHING. BUSHING REPLACED ON NON-ROUTINE 14 PER B737 SRM 57-20-90.

Part: BUSHING — WORN (LT MLG TRUNNION) · airframe 65,507 hrs · 24,216 cycles

(LOG 1890051) DURING INSPECTION FOUND LMLG UPR I/B FWD TRUNNION LUG WORN BUSHING. BUSHING REPLACED ON NON-ROUTINE 15 PER B737 SRM 57-20-90.

Part: TRUNNION — CORRODED (LT MLG) · corrosion level 2 · airframe 65,507 hrs · 24,216 cycles

(LOG 1890421) DURING INSPECTION FOUND LMLG UPR I/B FWD TRUNNION LUG CORROSION ON I/B AND O/B FACE. REPAIRED PER B737 SRM 57-20-90.

Part: BUSHING — WORN (LT MLG TRUNNION) · airframe 65,507 hrs · 24,216 cycles

(LOG 1890046) DURING INSPECTION FOUND LMLG UPR O/B FWD TRUNNION LUG WORN BUSHING. BUSHING REPLACED ON NON-ROUTINE 13 PER B737 SRM 57-20-90.

Part: BUSHING — WORN (LT TRUNNION) · airframe 65,507 hrs · 24,216 cycles

(LOG 1890054) DURING INSPECTION FOUND LMLG LWR I/B FWD TRUNNION LUG WORN BUSHING. BUSHING REPLACED ON NON-ROUTINE 16 PER B737 SRM 57-20-90.

Part: TRUNNION — CORRODED (LT MLG) · corrosion level 2 · airframe 65,507 hrs · 24,216 cycles

(LOG 1890418) DURING INSPECTION FOUND LMLG UPR O/B FWD TRUNNION LUG CORROSION ON I/B AND O/B FACE. REPAIRED PER B737 SRM 57-20-90.

Part: TRUNNION — CORRODED (RT MLG) · corrosion level 2 · airframe 65,507 hrs · 24,216 cycles

(LOG 1890385) DURING INSPECTION FOUND RMLG FWD TRUNNION UPPER I/B LUG CORROSION ON I/B FACE. REPAIRED PER B737 SRM 57-20-90.

Part: TRUNNION — CORRODED (LT MLG) · corrosion level 2 · airframe 65,507 hrs · 24,216 cycles

(LOG 1890420) DURING INSPECTION FOUND LMLG LWR O/B FWD TRUNNION LUG CORROSION ON I/B AND O/B FACE. REPAIRED PER B737 SRM 57-20-90.

Part: BATTERY PACK — INOPERATIVE · airframe 65,371 hrs · 24,151 cycles

(LOG 7313938) DURING INSPECTION FOUND EMERGENCY EXIT LIGHTS INOP RIGHT SIDE ROW 23 AND AFT. REMOVED AND REPLACED BATTERY PACK M1672 PER B737 AMM 33-51. EMERGENCY EXIT LIGHTS OPS CHK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,324 hrs · 24,138 cycles

(LOG 7313944) DURING INSPECTION FOUND 3 EMERGENCY EXIT LIGHTS AT THE LEFT OVER WING EXITS AND 1 ON THE RT ARE INOP. REPLACED BATTERY PACK BP1694. CKS GOOD PER B737 AMM 33-51

Part: SKIN — DAMAGED (RUDDER TE) · airframe 64,147 hrs · 23,688 cycles

DURING INSPECTION FOUND DAMAGE TO RUDDER TRAILING EDGE 6FT FROM TOP. REPAIRED DAMAGE, IAW B737 SRM 55-40-01-1A-1 FIG5 938895. ACCOMPLISHED SECTION 1 TIME LIMITED REPAIR, PER ERA 589622-14 REV ORIGINAL.

Part: WARNING MESSAGE — ILLUMINATED · airframe 63,342 hrs · 23,300 cycles

MISC/DE: ON FINAL WHILE EXTENDING FLAPS, RECEIVED A FLAP LOCKOUT MESSAGE AND HAD TO GO AROUND. RESET MESSAGE PER QRH. ATC DECLARED EMERGENCY. LOCKOUT RESET AND AIRCRAFT LANDED SAFELY. CORRECTIVE ACTION: T/S PER FIM WITH NTF. FSEU SUBSEQUENTLY REPLACED ON ODI FOLLOW UP LOG AS A PRECAUTION.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,334 hrs · 22,821 cycles

(LOG 7177206) L-2 DOOR EMERGENCY EXIT LIGHT AND AFT ISLE EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED M1673 POWER SUPPLY BATTERY PER B737 AMM 33-51. ALL LIGHTS OP'S CK'S GOOD.

Part: MODULE — FLUCTUATES (NR 4) · airframe 61,891 hrs · 22,628 cycles

(LOG 7146300) IAS UNRELIABLE IN CRUSE. ALT UNRELIABLE & OTHER ABNORMALITIES DURING DECENT ON NBR 2 SIDE. ALL INDICATIONS CAME BACK AT 4500. R&R RT STATIC ADM PER B737 AMM 31-21-04 PERFORMED PITOT AND STATIC LEAK CK'S PER B737 AMM 34-11-00. LEAK CK'S GOOD.

Part: FRAME — DENTED (FUSELAGE) · airframe 60,135 hrs · 21,886 cycles

(LOG 1184866) DURING INSPECTION FOUND DENTED FRAME LOCATED STA 500F AND BTW STR 24L TO STR 25L AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON FRAME BS500F BETWEEN STR24L TO STR25L AT FWD CARGO COMPARTMEN AS PER PRI 579504-14 REV O REV 1 AND ERA 579504-14.

Part: FRAME — DENTED (FUSELAGE) · airframe 60,134 hrs · 21,885 cycles

(LOG 1181237) DURING INSPECTION FOUND DENTED FRAME AT BS 727F AND BTW S-23L TO S-24L AT AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON FRAME AT B 727F AND BTW 5-23L TO 5-24L AT AFT CARGO COMPARMENT AS PER PRI # 579451-14 REV.0 REV. 1 AND ER/A # 579451-14.

Part: ANGLE — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 60,134 hrs · 21,885 cycles

(LOG 1179697) DURING INSPECTION FOUND CORROSION INTERNAL STRUCTURE BTW STR 2L AND STR 3L AT LEVEL OF BS 1104 AND WL 300 APPROX HORIZONTAL STABILIZER CENTER SECTION IN TAIL COMPARTMENT. REPLACED ANGLE LOCATED INTERNAL STRUCTURE BTW STR 2L AND STR 3L AT LEVEL OF BST 1104 AND WL 300 APPROX HORIZONTAL STABILIZER CENTER SECTION IN TAIL COMPARTMENT AS PER SRM 51-10-02 STEP 9 AND DRAWING NR 4878700 REV B.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,134 hrs · 21,885 cycles

(LOG 1176362) DURING INSPECTION FOUND CORROSION WEB - INTERCOSTAL LOWER SURFACE LOCATED BETWEEN BS767 TO BS787 AT LEVEL STR25R AT AFT CARGO COMPARTMENT. REPLACED WEB INTERCOTAL LOWER SURFACE LOCATED BETWEEN BS 767 TO BS 787 AT LEVEL STR 25 R AT AFT CARGO COMPARMENT ASPER SRM 51-40-02,SRM 51-1002 ITEM 9 AND DRAWING 146A0081 REV. A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,134 hrs · 21,885 cycles

(LOG 1170289) DURING INSPECTION FOUND CRACKED FRAME AT BS500D AND BETWEEN S-8L TO S-9L AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME BST 500F BTW STR 8L TO STR 9L AT PASSENGER CABIN AS PER ER/A 579465-14AD REV ORIGINAL AND PRI 579465-14AD REV 0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,134 hrs · 21,885 cycles

(LOG 1170307) DURING INSPECTION FOUND CRACKED FRAME LOCATED BS 727B AND STR 8R TO STR 9R AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME BST 727B AND BTW STR 8R TO STR 9R AT PASSENGER CABIN AS PER ER/A 579465-14AD REV ORIGINAL AND PRI 579465-14A REV 0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,134 hrs · 21,885 cycles

(LOG 1170295) DURING INSPECTION FOUND CRACKED FRAME AT BS500F BETWEEN S-8L TO S-9L AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME BST 500F BTW STR 8L TO STR 9L AT PASSENGER CABIN AS PER ER/A 579465-14AD REV ORIGINAL AND PRI 579465-14AD REV 0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,134 hrs · 21,885 cycles

(LOG 1170299) DURING INSPECTION FOUND CRACKED FRAME BS500C AND BETWEEN S-8L TO S-9L AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME BST 500F BTW STR 8L TO STR 9L AT PASSENGER CABIN AS PER ER/A 579465-14AD REV ORIGINAL AND PRI 579465-14AD REV 0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,134 hrs · 21,885 cycles

(LOG 1170327) DURING INSPECTION FOUND CRACKED FRAME LOCATED BS 500A AND STR 8R TO STR 9R AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME BST 500A BTW STR 8L TO STR 9L AT PASSENGER CABIN AS PER ER/A 579465-14AD REV ORIGINAL AND PRI 579465-14A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,134 hrs · 21,885 cycles

(LOG 1170318) DURING INSPECTION FOUND CRACKED FRAME BS440 BETWEEN S-8L TO S-9L AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME BST 440 BTW STR 8L TO STR 9L AT PASSENGER CABIN AS PER ERA 579465-14AD REV ORIGINAL AND PRI 579465-14A REV 0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,134 hrs · 21,885 cycles

(LOG 1170319) DURING INSPECTION FOUND CRACKED FRAME LOCATED BS 500F AND STR 8R TO STR 9R AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME BST 500F AND BTW STR 8R TO STR 9R AT PASSENGER CABIN AS PER ER/A 579465-14AD REV ORIGINAL AND PRI 579465-14A REV 0.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 60,134 hrs · 21,885 cycles

(LOG 1171768) DURING INSPECTION FOUND AFT CARGO BIN CORROSION ON FIXED FLOOR PANEL AROUND NUTPLATE HOLE FS 847, STR 25R ALSO AT FS 837, STR 25R 837 UNDERSIDE OF C2 DOORWAY THRESHOLD CLOSEOUT WEB. REPLACED INTERCOSTAL AND FASTENERS LOC. BS 867 TO BS 887 5-25R IN AFT CARGO COMPARTMENT AND SHIELD LOC. BS 849 TO BS 8705- 25R IN AFT CARGO COMPARTMENT AS PER SRM 51-10-02 ITEM 9 AND DRAWINGS 146A0081 REV A AND 146A7502 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,134 hrs · 21,885 cycles

(LOG 1170302) DURING INSPECTION FOUND CRACKED FRAME LOCATED AT BS727B AND BETWEEN STR8L TO STR9L AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME BST 727B AND BTW STR 8L TO STR 9L AT PASSENGER CABIN AS PER ERA 579465-14AD REV ORIGINAL AND PRI 579465-14AD REV 0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,134 hrs · 21,885 cycles

(LOG 1170016) DURING INSPECTION FOUND CRACKED FRAME LOCATED BS 480 AND STR 8R TO STR 9R AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME BST 480 AND BTW STR 8R TO STR 9R AT PASSENGER CABIN AS PER ERA 579465-14 AD REV ORIGINAL AND PRF 579465-14 AD REV0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,134 hrs · 21,885 cycles

(LOG 1170045) DURING INSPECTION FOUND CRACKED FRAME BS500A AND BETWEEN S-8L TO S-9L AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME BST 500A AND BTW STR 8L TO 9L AT PASSENGER CABIN AS PER ER/A579465-14AD REV.ORIGINAL AND PR 579465-14AD REV 0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,134 hrs · 21,885 cycles

(LOG 1170028) DURING INSPECTION FOUND CRACKED FRAME BS380 BETWEEN S-8L TO S-9L AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME BS 380 BTW STR 8 L TO STR AL AT PASSENGER CABIN AS PER ERA 579465-14 AD REV. ORIGINAL AND PRI 579465-14AD REV O.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 60,134 hrs · 21,885 cycles

(LOG 1166543) DURING INSPECTION FOUND CORROSION LOWER SILL AT FWD CARGO COMPARTMENT. REPLACED LOWER SILL AT PWD CARGO COMPARMENT AS PER SRM 51-40-02, SRM 51-10-02 ITEM 9 AND DWG # 14348330 REV A.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,134 hrs · 21,885 cycles

(LOG 1165146) DURING INSPECTION FOUND CORROSION FLOOR STRUCTURE SUPPORT FITTING LOCATED BS 277 TO BS 294.5 AND RBL 42 AT FWD GALLEY AREA. REPLACED FLOOR STRUCTURE SUPPORT FITTING LOCATED BS 277 TO BS 294.5 AND RBL 42 AT FWD GALLEY AREA AS PER SRM 51-10-02, 51-40-02 AND DWG 141A5710 REV B.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 60,134 hrs · 21,885 cycles

SHIP 3756 CRACK FLOOR STRUCTURE PLATE OF CHANNEL LOCATED BS 540 AND LBL 24.5 TO LBL 45.5 AT PASSENGER CABIN . CORRECTIVE ACTION: REPLACED CHANNEL LOC FLOOR STRUCTURE BS 540 AND LBL 24.5 TO LBL 45.5 AT PASSENGER CABIN AS PER SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DRAWING 143A5240 REV 0 (1155420).

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 60,134 hrs · 21,885 cycles

SHIP 3756 CRACK EXTERNAL SKIN LOWER SURFACE LOCATED STAB STA 101.90 RT HORIZONTA L STAB . CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOWER SURFACE LOC STAB STA 101.90 RT HORIZONTAL STABILIZER AS PER SRM 55-10-01 REPAIR 11 (1152284).

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHTS) · airframe 60,104 hrs · 21,871 cycles

DURING INSPECTION, FOUND BATTERY PACK AT M1695 DEFECTIVE. R/R EMERGENCY LIGHT BATTERY PACK M1695 IAW WORK CARD 3350-7413. OPS CKS NORMAL.

Part: BRAKE — FIRE (NR 2) · airframe 57,472 hrs · 20,771 cycles

ON ARRIVAL, NOTICED THE NR 2 BRAKE GLOWING AND A GREASE FIRE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BRAKE ASSEMBLY. CLEANED AND INSPECTED AXLE, NO DAMAGE NOTED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,100 hrs · 20,274 cycles

DURING INSPECTION, FOUND THE MID CABIN EXIT SIGN MISSING OVER AISLE HALF WAY BACK TO AFT CABIN. MAINTENANCE THE REPLACED LENS.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 55,975 hrs · 20,224 cycles

DURING INSPECTION, FOUND WEAR ON THE FLIGHT CREW SEAT TRACK CAPS AND FIRST OFFICER`S SEAT. REPLACED IAW AMM 25-11-01.

Part: DOUBLER — CRACKED · airframe 55,960 hrs · 20,223 cycles

DURING INSPECTION, FOUND A CRACK ON THE INTERNAL DOUBLER AFT AREA, ON THE POWER RECEPTACLE CUT OUT. REPAIRED IAW SRM 53-10-15, REPAIR 4.

Part: PIN — CORRODED (TRUNNION) · airframe 52,169 hrs · 18,952 cycles

DURING INSPECTION, FOUND THE RIGHT MAIN LANDING GEAR AFT TRUNNION PIN WAS CORRODED. REPLACED THE AFT TRUNNION PIN.

Part: LENS — MISSING (CABIN) · airframe 51,838 hrs · 18,830 cycles

DURING INSPECTION FOUND EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. MAINTENANCE REINSTALLED EMERGENCY EXIT LENS COVER.

Part: SEAT TRACK — DAMAGED (BS 727) · airframe 39,725 hrs · 14,775 cycles

DURING INSPECTION FOUND PASSENGER CABIN, OTBD SEAT TRACK, LBL 45, OTBD FLANGE, BS 727+18, FLOORBOARD ATTACH HOLE IS ELONGATED. MX C/W PRI 517807-14 REVISION 0, REVISION 1, REVISION 2, REVISION 3 AND ERA 517807-14, REVISION ORIGINAL.

Part: SEAT TRACK — DAMAGED (BS 727D) · airframe 39,725 hrs · 14,775 cycles

DURING INSPECTION, FOUND SCALLOP BROKEN OFF SEAT TRACK AT BS 727D + 6 LBL 45.5. MX FABRICATED REPAIR PARTS, INSTALLED REPAIR PARTS. COMPLIED WITH REVIEW OF FINAL ERA 517644-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 440) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND FRAME CRACKED AT BS 440 STRINGER 8R. REPAIRED IAW PRI516859-14AD ORIGINAL AND ERA 516859-14AD ORIGINAL.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND JUST FWD OF STATION 727B, RBL 45.50, SEAT TRACK OTBD FLANGE FORWARD & AFT FASTENER HOLES ARE CRACKED. MX PERFORMED PERMANENT REPAIR TO SEAT TRACK STATION RBL 45.50 IAW ERA 516852-14, REV ORIGINAL REV 1 OF PRI 516852-14, REV 0.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION FOUND JUST FORWARD OF BS 727B LBL 45.50, SEAT TRACK OTBD FLANGE AFT FASTENER HOLE IS CRACKED. MX C/W PRI 516852-14, REV 0 AND ERA 516852 REV ORIGINAL.

Part: FRAME — CRACKED (BS 380) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND FRAME CRACKED AT BS 380 STRINGER 8R. MX REPAIRED IAW PRI 516859-15AD ORIGINAL AND ERA 516859-14AD ORIGINAL.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND JUST FWD OF BS 727B, LBL 24.75, SPLICE STRAP INBD FLANGE AFT FASTENER HOLE IS CRACKED. MX PERFORMED PERMANENT REPAIR IAW ERA 516852-14 REV ORIGINAL REV-1 OF PRI 516852-14, REV0.

Part: FRAME — CRACKED (BS 480) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND FRAME CRACKED AT STATION 480, STRINGER 8L. REPAIRED IAW PRI 516859-14 AD, ORIGINAL AND ERA 516859-14AD ORIGINAL.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION FOUND JUST FWD OF BS 727B, LBL 45.50 SEAT TRACK INBD FLANGE AFT FASTENER HOLE IS CRACKED. MX PERFORMED PERMANENT REPAIR TO SEAT TRACK AT BS 727B, LBL 45.50 IAW ERA 516852-14, REV ORIGINAL, REV-1 OF PRI 516852-14, REV 0.

Part: FRAME — CRACKED (BS 400) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND FRAME CRACKED AT BS 400, STRINGER 8R. MX REPAIRED IAW PRI 516859-14 AD ORIGINAL AND ER/A 516859-14, AD ORIGINAL.

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND LT HORIZONTAL STABILIZER LOWER SKIN IS GOUGED AT STAB STATION 155. 11" AFT OF FORWARD SPAR. MX CUTOUT DAMAGE AND REPAIRED IAW SRM 55-10-01, REPAIR 11.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND ATTACH ANGLE AT LT ZEE ANGLE AREA HAS CORROSION. MX INSTALLED NEW SUPPORT ANGLE IAW DWG 143A9481, REV B AND SRM 51-40-02.

Part: SEAT TRACK — WORN (BS 520) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND MAIN CABIN, SEAT TRACK AT BS 520 RBL 24 IS WORN. MX REPAIRED WORN SECTION IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — WORN (BS 520) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND MAIN CABIN, SEAT TRACK AT BS 520 RBL 45 IS WORN. MX REPAIRED SEAT TRACK IAW 53-00-52, REPAIR 4.

Part: SEAT TRACK — WORN (BS 520) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUIND MAIN CABIN, SEAT TRACK AT BS 520 LBL 45 IS WORN. MX REPAIRED SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — WORN (MAIN CABIN) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND MAIN CABIN, SEAT TRACK IS WORN. MX REPAIRED SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — WORN (BS 520) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND MAIN CABIN, SEAT TRACK AT STATION 520 LBL45 IS WORN. MX REPAIRED SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: SUPPORT CHANNEL — CRACKED (VERTICAL STAB) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND VERTICAL STAB INTERNAL STRUCTURE, SUPPORT CHANNEL CRACKED AT LT AND RT ENDS ABOVE AND AFT OF STAB FORWARD TERMINAL FITTINGS. MX INSTALLED NEW SUPPORT CHANNEL A, TAG A22712 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 958) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND AFT WET AREA, BS 958, RBL 48, FLOOR SUPPORT STRUCTURE CORRODED. MX R & R FLOOR SUPPORT STA 958, RBL 48 IAW DWG 147A5650.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION FOUND FORWARD GALLEY BS 328, RBL 10, FLOORBEAM UPPER TEE CORRODED. MX REPAIRED IAW SRM 53-10-51 REPAIR 8.

Part: FLOORBEAM — GOUGED (BS 460) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND FORWARD CARGO BAY FLOORBEAM AT BS 460 + 3 LBL 3 GOUGED AND DENTED. MX REMOVED DAMAGE IAW SRM 53-00-53, REPAIR 2. FABRICATED AND INSTALLED ALL REPAIR PARTS IAW SRM 53-00-53, REPAIR 2.

Part: WEB — CORRODED (THRESHOLD) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND AFT CARGO DOOR CUTOUT LOWER SILL THRESHOLD WEB CORRODED. MX R & R SILL THRESHOLD WEB IAW SRM 51-40-02, PAGE 3, PAR. 5 AND DOC 146A8123.

Part: FITTING — CORRODED (GIRT BAR) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND FWD ENTRY DOOR LOWER INNER CREASE BEAM, BS 344, GRIT BAR FITTING CORRODED TASK 53-380. MX REMOVED TIE DOWN AND INSTALLED A NEW PN 141A52204 IAW DWG 141A5220, SRM 51-40-02, PGS 1-10.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION FOUND BS 727B, LBL 45.50 SEAT TRACK INBD FLANGE AFT FASTENER HOLE IS CRACKED. MX PERFORMED PERMANENT REPAIR TO SEAT TRACK IAW ERA 516852-14, REV 0, REV 1 OF PRI 516852-14.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION FOUND BS 727B LBL 24.75 SEAT TRACK SPLICE STRAP INBD FLANGE AFT FASTENER HOLE IS CRACKED. MX PERFORMED PERMANENT REPAIR TO SEAT TRACK IAW ERA 516852-14 REV 0, REV 1 OF PRI 516852-14.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND BS 727B, RBL 45.50, SEAT TRACK INBD FLANGE FORWARD & AFT FASTENER HOLES ARE CRACKED. MX PERFORMED PERMANENT REPAIR TO SEAT TRACK IAW ERA 516852-14, REV 0, REV 1 OF PRI 516852-14.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION FOUND BS 727B, RBL 45.50 SEAT TRACK OTBD FLANGE FWD & AFT FASTENER HOLES ARE CRACKED. MX PERFORMED PERMANENT REPAIR TO SEAT TRACK IAW ERA 516852-14 REV 0, REV 1 OF PRI 516852-14.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION FOUND AFT WET AREA, R2 DOOR CREASE BEAM, INNER ANGLE IS CORRODED. MX REMOVED CREASE BEAM AND INSTALLED NEW IAW DWG 147A8501.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 39,698 hrs · 14,766 cycles

DURING INSPECTION, FOUND FWD GALLEY BS 328 LBL 12 FLOORBEAM UPPER TEE CORRODED. REPAIRED IAW SRM 53-10-51, REPAIR 11.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 38,887 hrs · 14,482 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHT AT 10-13DEF NOT WORKING AT SEAT. REPAIRED WIRE AT SEAT 10DEF, CHECKED NORMAL. IAW WDM 33-51.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 38,436 hrs · 14,324 cycles

DURING TEST THE EMERGENCY LIGHT BATTERY PACK FAILED 15 MIN TEST. MX REPLACED BATTERY PACK. OPS CHECKED OK IAW AMM 33-51.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,251 hrs · 13,954 cycles

DURING TEST, FOUND LEFT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. MX REPLACED OPEN FUSE ON BATTERY PACK M1694 REF WDM 33-51-13, PG 2 OPS CHECK OK.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,161 hrs · 13,922 cycles

DURING TEST, FOUND AISLE EMERGENCY LIGHTS INOPERATIVE AT 16DAND 17C. MX REPLACED OPEN FUSE ON BATTERY PACK M1695 IAW WDM 33-51-13. OPS CHECK OK.

Part: LIGHT — INOPERATIVE (SEAT 31D) · airframe 36,821 hrs · 13,802 cycles

DURING INSPECTION, FOUND SEAT 31D EMERGENCY AISLE WHITE LIGHT INOPERATIVE. MX R & R SEAT END COVER, LIGHT SHROUD AND LIGHT ASSY. OPS CHECKED GOOD.

Part: ENGINE — SHUTDOWN (NR 1) · airframe 36,804 hrs · 13,795 cycles

DURING CLIMB, NR 1 ENGINE EXPERIENCED AUTOSHUTDOWN. ACFT RETURNED TO DEPARTURE. MX FOUND DAMAGE ON THE LT HORIZ STABILIZER L/E. MX REPLACED THE LT HORIZONTAL STABILIZER AND THE NR 1 ENGINE. OPS CHECK OK, ACFT RETURNED TO SERVICE.

Part: OVEN — SPARKS (FWD GALLEY) · airframe 36,763 hrs · 13,779 cycles

DURING FLIGHT, THE FORWARD GALLEY OVEN BEGAN EMITTING SPARKS AND SMOKE. ACFT DIVERTED. MX FOUND OVEN MOTOR DAMAGED. PULLED AND SECURED OVEN CIRCUIT BREAKER. OVEN REPLACED AND ACFT RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 35,318 hrs · 13,277 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTING BETWEEN ROWS 10 AND 15 TO BE INOPERATIVE. MAINTENANCE REPLACED FUSES AND RETERMINATED CONNECTOR AND LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: FITTING — CORRODED (MLG TRUNNION) · airframe 32,819 hrs · 12,433 cycles

COMPLETED STEP 3 OF EA 12-487906-12 REV A ON OPN NR 0601ME06& 0301ME03 RT, LT. ACCOMPLISH REPAIR AT EACH LOCATION WHERE CORROSION IS FOUND ON THE OUTER SURFACE OF A LUG AROUND THE EDGE OF THE BORE ONLY (I.E. NO CORROSION IN THE BORE). REPAIRS TO BORES/FACES WERE COMPLETED PER B737SRM 57-20-90 REP NR 3.