N705SW

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 74,236 hrs · 44,399 cycles

AFT INBOARD EMERGENCY FLASHLIGHT CHARGE INDICTOR NOT BLINKING. R&R BATTERY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 73,803 hrs · 44,087 cycles

R2 DOOR OVER DOOR EMERGENCY EXIT SIGN BROKEN. R&R SIGN PER AMM.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 73,762 hrs · 44,059 cycles

AFT CARGO DOOR SURROUND LOWER SILL CRACKED. R&R SILL WEB IAW SRM, DWG, AND EA.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 72,351 hrs · 43,161 cycles

CARGO FIRE PANEL DISCHARGE LIGHT ILLUMINATED. AFTER APPROXIMATELY/ 15 MIN LIGHT EXTINGUISHED. R&R PANEL IAW MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 70,582 hrs · 42,086 cycles

AFT FLASHLIGHT STRAP BROKEN. R&R STRAP PER SIP.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 69,936 hrs · 41,679 cycles

L1 DOOR EMERGENCY SLIDE LOOSE. SECURED SLIDE PER SIP.

Part: COVER — CRACKED (EMERGENCY EXIT) · airframe 69,695 hrs · 41,533 cycles

LEFT EMERGENCY EXIT RED PULL HANDLE COVER CRACKED. R & R COVER IAW AMM.

Part: GIRT BAR — LOOSE (L2 DOOR SLIDE) · airframe 69,626 hrs · 41,485 cycles

L2 DOOR EMERGENCY SLIDE GIRT BAR CLOTH OUT OF ADJUST. INSTALLED THE CLOTH ON HOOK AND LOOP STRIP IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,626 hrs · 41,485 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,626 hrs · 41,485 cycles

EMERGENCY LIGHT BATTERY M1669 INOPERATIVE. R & R THE BATTERY IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,626 hrs · 41,485 cycles

L2 DOOR AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 69,626 hrs · 41,485 cycles

LEFT EMERGENCY LIGHT LENS MISSING AT ROW 14. INSTALLED A NEW LENS IAW AMM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,626 hrs · 41,485 cycles

EMERGENCY LIGHT BATTERY M1672 INOPERATIVE. R & R THE BATTERY IAW AMM.

Part: BRACKET — CRACKED (BS 945) · airframe 69,626 hrs · 41,485 cycles

FLOOR SUPPORT BULKHEAD BRACKET CRACKED AT BS 945, LBL 11. R & R THE BRACKET IAW SRM AND DWG.

Part: CONNECTOR — MISSING (EMERGENCY LIGHT) · airframe 69,626 hrs · 41,485 cycles

L2 DOOR AFT INTERIOR EMERGENCY EXIT LIGHT MISSING A CONNECTOR. REPLACED THE CONNECTOR IAW AMM AND WDM.

Part: SKIN — CORRODED (BS 971) · airframe 69,626 hrs · 41,485 cycles

SKIN AROUND DOOR THRESHOLD DRAIN CORRODED AT BS 971. REPAIRED THE SKIN IAW ER AND EA.

Part: SKIN — CORRODED (BS 953) · airframe 69,626 hrs · 41,485 cycles

SKIN AROUND POTABLE WATER DRAIN CORRODED AT BS 953. REPAIRED THE SKIN IAW ER AND EA.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 69,626 hrs · 41,485 cycles

AFT CARGO DOOR CENTER SCUFF PLATE CRACKED FORWARD END. R & R THE SCUFF PLATE IAW AMM AND EA.

Part: FITTING — CRACKED (LT WING SLAT) · airframe 69,626 hrs · 41,485 cycles

LEFT WING NR 4 SLAT FITTING CRACKED. R & R NR 4 SLAT ASSEMBLY IAW AMM.

Part: FITTING — CRACKED (RT WING SLAT) · airframe 69,626 hrs · 41,485 cycles

RIGHT WING NR 7 SLAT FITTING CRACKED. R & R NR 7 SLAT ASSEMBLY IAW AMM.

Part: FITTING — CRACKED (LT WING SLAT) · airframe 69,626 hrs · 41,485 cycles

LEFT WING NR 3 SLAT FITTING CRACKED. R & R THE NR 3 SLAT ASSEMBLY IAW AMM.

Part: HOOK AND LOOP — LOOSE (ESCAPE ROPE) · airframe 69,626 hrs · 41,485 cycles

RIGHT OVERWING EMERGENCY EXIT ESCAPE ROPE COVER HOOK AND LOOP LOOSE. SECURED THE HOOK AND LOOP IAW SOPM.

Part: COLLAR — CORRODED (LOCK FASTENER) · airframe 69,626 hrs · 41,485 cycles

LEFT WING STRINGER U14 SPLICE STIFFENER PANEL 532FB LOCK FASTENER COLLARS CORRODED. R & R THE LOCK FASTENER COLLARS IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,626 hrs · 41,485 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED, 3RD FROM INBOARD END. R&R RIB IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,626 hrs · 41,485 cycles

RT HORIZONTAL STABILIZER LEADING EDGE, 4TH RIB FROM INBOARD END CRACKED LOWER END. R&R RIB PER SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,626 hrs · 41,485 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE, 5TH RIB FROM INBOARD END CRACKED AT HSS 114.55, LOWER END. R & R THE RIB IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,626 hrs · 41,485 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE, 9TH RIB FROM INBOARD END CRACKED AT BS 141.75, LOWER END. R & R THE RIB IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 69,626 hrs · 41,485 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, BL 0. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: FRAME — CRACKED (BS 727) · airframe 69,626 hrs · 41,485 cycles

RIGHT FRAME CRACKED AT BS 727, WL 200. REPAIRED THE FRAME IAW EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,626 hrs · 41,485 cycles

RIGHT HORIZONTAL STABILIZER INNER SPAR RIB CRACKED AT HSS 92.70, THIRD STIFFENER FROM THE FORWARD SIDE REPAIRED THE RIB IAW SRM, DWG, & EA.

Part: SIDEWALL SUPPORT — CORRODED (BS 727D-767) · airframe 69,626 hrs · 41,485 cycles

AFT CARGO, RT FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN BS 727D TO 762, RBL 22. R & R THE SIDEWALL SUPPORT IAW DWG AND SRM.

Part: SHIELD — CORRODED (BS 777) · airframe 69,626 hrs · 41,485 cycles

AFT CARGO FORWARD SIDE SHIELD CORRODED AT BS 777, RBL 22. R & R THE SHIELD IAW SRM & DWG.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 69,626 hrs · 41,485 cycles

LEFT WING OTBD AFT FLAP INBOARD TRAILING EDGE CORNER DELAMINATED. R & R THE AFT FLAP ASSEMBLY IAW AMM.

Part: SIDEWALL SUPPORT — CORRODED (BS 727-807) · airframe 69,626 hrs · 41,485 cycles

AFT CARGO, LT FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN BS 727 TO 807, LBL 22. R & R THE SIDEWALL SUPPORT IAW DWG & SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 69,626 hrs · 41,485 cycles

VAPOR BARRIER CRACKED AT BS. 663, RBL 12 LOWER SECTION. REPAIRED BARRIER IAW SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 69,626 hrs · 41,485 cycles

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

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 69,626 hrs · 41,485 cycles

LEFT OVERHEAD BIN EMERGENCY LIGHT LENS CRACKED AT ROW 14. R & R THE LENS IAW AMM.

Part: FLOORBEAM — CRACKED (BS 663) · airframe 69,137 hrs · 41,165 cycles

CABIN FLOORBEAM CORRODED AT BS 663, RBL 45. REPAIRED THE FLOORBEAM IAW EA.

Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 69,137 hrs · 41,165 cycles

MLG WHEEL WELL PRESSURE WEB ANGLE CRACKED AT BS 663, RBL 60. REPAIRED ANGLE IAW EA.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 69,137 hrs · 41,165 cycles

RIGHT MLG WHEEL WELL PRESSURE BULKHEAD WEB CRACKED AT STA 663, RBL 48. REPAIRED THE BULKHEAD WEB IAW EA.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 69,137 hrs · 41,165 cycles

FORWARD EMERGENCY FLASHLIGHT TAMPER STRAP BROKEN. R&R STRAP PER AMM.

Part: O-RING — FAULTY (NR 1 ENGINE) · airframe 69,019 hrs · 41,085 cycles

DIVERSION/DECLARED EMERGENCY, DURING CRUISE, ENGINE 1 SIDE LOW PRESSURE LIGHT ILLUMINATED. R&R O RING PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,599 hrs · 40,825 cycles

AFT ENTRY EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 67,163 hrs · 39,911 cycles

R1 DOOR EMERGENCY EXIT SIGN LENS COVER FELL OFF. R & R THE COVER IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 67,086 hrs · 39,871 cycles

FORWARD ENTRY INSIDE EMERGENCY LIGHT LENS BROKEN. R&R LIGHT ASSEMBLY IAW MM.

Part: WEB — CRACKED (LT MLG WW) · airframe 66,997 hrs · 39,810 cycles

LEFT WHEEL WELL BULKHEAD CEILING BEADED WEB CRACKED AT BS. 663, LBL 32. REPAIRED THE WEB IAW EA.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 65,163 hrs · 38,761 cycles

RIGHT WING TRAILING EDGE FIXED PANEL SUPPORT ANGLE THAT ATTACHES TO THE MID SPAN DEFLECTION CONTROL IS CRACKED. R&R THE ATTACH ANGLE IAW DWG & SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 65,163 hrs · 38,761 cycles

LEFT WING TRAILING EDGE FIXED PANEL SUPPORT ANGLE THAT ATTACHES TO THE MID SPAN DEFLECTION CONTROL CRACKED. R & R THE SUPPORT ANGLE IAW DWG & SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 65,158 hrs · 38,757 cycles

RIGHT WING LEADING EDGE NR 7 SLAT SKIN CRACKED. REPAIRED THE SKIN IAW EA.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 63,995 hrs · 38,077 cycles

L1 DOOR INNER DOOR PAN CUTOUT REVEAL ANGLE CRACKED AT DOOR LOWER HINGE POINT. R & R ANGLE IAW SRM & DWG.

Part: SKIN — DEFORMED (FUSELAGE) · airframe 63,995 hrs · 38,077 cycles

L1 DOOR FUSELAGE SKIN LOWER HINGE CUTOUT DEFORMED. R & R SKIN IAW DWG AND SRM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 63,503 hrs · 37,800 cycles

RIGHT EMER LIGHTS INOPERATIVE, BETWEEN ROW 9 - 11. R & R POWER SUPPLY ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,503 hrs · 37,799 cycles

R2 DOOR INTERIOR EMER EXIT SIGN LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 63,503 hrs · 37,799 cycles

L2 DOOR INTERIOR EMER EXIT SIGN BULB INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 63,503 hrs · 37,799 cycles

RIGHT OVERWING INTERIOR EMER EXIT SIGN BULB INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,503 hrs · 37,799 cycles

MAIN ENTRY OVERHEAD EMER EXIT LIGHT INOPERATIVE AT LOCATION M1674. R & R BATTERY PACK IAW AMM.

Part: HOUSING — CRACKED (EXIT SIGN) · airframe 63,503 hrs · 37,799 cycles

OVERWING EXIT CTR CEILING EXIT SIGN HOUSING CRACKED. R & R SIGN HOUSING IAW AMM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 63,503 hrs · 37,799 cycles

LEFT OVERHEAD BIN EMER EXIT LIGHT CONNECTOR BROKEN AT ROW 14. R & R CONNECTOR IAW WDM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,503 hrs · 37,799 cycles

FRAME CORRODED AT BS 303.9, LBL 55. REPAIRED FRAME IAW EA.

Part: SHEAR WEB — DAMAGED (FUSELAGE) · airframe 63,503 hrs · 37,799 cycles

SHEAR WEB DAMAGED, BETWEEN BS 986 - 1016, LBL 40. R & R SHEAR WEB IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,503 hrs · 37,799 cycles

FORWARD ENTRY DOOR THRESHOLD SUPPORT ANGLE ATTACHED TO MOP SILL CORRODED, BETWEEN BS 318 - 340. R & R ANGLE IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,503 hrs · 37,799 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED AT BS 500D, STRINGER 9R. R & R INTERCOSTAL IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,503 hrs · 37,799 cycles

ANGLE CRACKED AT BS 295, RBL 56. REPAIRED ANGLE IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,503 hrs · 37,799 cycles

FLOORBEAM ANGLE ASSEMBLY CORRODED AT BS 967, RBL 42. REPAIRED ANGLE IAW SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,503 hrs · 37,799 cycles

SHEAR WEB CORRODED, BETWEEN BS 986 - 1016, RBL 41. R & R SHEAR WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,503 hrs · 37,799 cycles

UPPER FLANGE OF FLOORBEAM CORRODED AT BS 987, BETWEEN LBL 29 - 35. REPAIRED FLOORBEAM IAW ER & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,503 hrs · 37,799 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727D+10 - 847. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,503 hrs · 37,799 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 460 - 500D, LBL 24. REPAIRED SUPPORT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,503 hrs · 37,799 cycles

LEFT WING NR 2 SLAT SKIN CRACKED ON LOWER SURFACE AT ACTUATOR ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,503 hrs · 37,799 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727C+10 - 767. R & R SUPPORT IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,503 hrs · 37,799 cycles

FORWARD CARGO BAY RT SHIELD CORRODED, BETWEEN BS 420 - 440. R & R SHIELD IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,122 hrs · 37,559 cycles

AFT PRESS BULKHEAD WEB CRACKED AT BS 1016, STRINGER 23R. REPAIRED WEB IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,122 hrs · 37,559 cycles

AFT PRESS BULKHEAD WEB CRACKED, AT BS 1016, BETWEEN STRINGER 15R - 23R. REPAIRED WEB IAW EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 62,860 hrs · 37,410 cycles

LEFT MLG TRUNNION FITTING LUG FACES CORRODED. R & R FITTING IAW EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 62,860 hrs · 37,410 cycles

RIGHT MLG TRUNNION FITTING LUG FACES CORRODED. R & R FITTING IAW EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 62,860 hrs · 37,410 cycles

RIGHT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING IAW EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 62,860 hrs · 37,410 cycles

LEFT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 61,458 hrs · 36,587 cycles

RIGHT HORIZONTAL STABILIZER STATION 92.70, RIB CRACKED 10" AFT FROM LE. REPAIRED STABILIZER IAW SRM.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 58,788 hrs · 35,100 cycles

FUSELAGE KEEL BEAM ACCESS PANEL 192E FWD RT ATTACH BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 58,788 hrs · 35,100 cycles

LEFT OF CTR FLOORBOARD SUPPORT FRAME CRACKED BETWEEN BS 344 TO 360. R & R SUPPORT IAW AMM.

Part: SUPPORT — CRACKED (RT MLG WW) · airframe 58,788 hrs · 35,100 cycles

RIGHT MAIN WW VERTICAL SUPPORT FRAME CRACKED AT BS 663, RBL 25. R & R SUPPORT IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 58,788 hrs · 35,100 cycles

FUSELAGE RT RAM AIR DUCT FWD SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM & EA.

Part: SUPPORT BRACKET — CRACKED (RT MLG WW) · airframe 58,788 hrs · 35,100 cycles

RIGHT WW RAM AIR EXHAUST SUPPORT BRACKET CRACKED AT BS 663, RBL 15.54. R & R BRACKET IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 58,788 hrs · 35,100 cycles

RIGHT OF CTR FLOORBOARD SUPPORT FRAME CRACKED BETWEEN BS 344 TO 360. R & R SUPPORT IAW SRM.

Part: COVER — LOOSE (CABIN) · airframe 56,973 hrs · 34,034 cycles

R1 DOOR EMERGENCY EXIT FWD SIDEWALL LIGHT COVER LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: FITTING — CRACKED (LT WING) · airframe 56,964 hrs · 34,027 cycles

LEFT WING UPPER CLIP AT REAR SPAR, INBD OF BOOST PUMP AT WBL 94.24 CRACKED. R & R CLIP IAW SRM & DWG.

Part: LIGHT — CRACKED (CABIN) · airframe 56,964 hrs · 34,027 cycles

RIGHT EEPLS CRACKED BETWEEN BS 340 TO BS 727B. R & R EEPLS IAW AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 56,964 hrs · 34,027 cycles

LEFT EEPLS CRACKED BETWEEN BS 340 TO BS 727B. R & R EEPLS IAW AMM.

Part: BRACKET — CRACKED (LT WING SLAT) · airframe 56,869 hrs · 33,965 cycles

LEFT WING NR 1 SLAT BRACKET CRACKED. R & R BRACKET IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,095 hrs · 32,936 cycles

FRAME CRACKED AT STATION 500C, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,095 hrs · 32,936 cycles

RT NR 1 COCKPIT WINDOW FRAME UPPER FASTENER HOLE CRACKED IN VERTICAL LEG. R&R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,095 hrs · 32,936 cycles

LT NR 1 WINDOW FRAME UPPER OTBD CORNER OF CD POST CRACKED. R&R FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,095 hrs · 32,936 cycles

FRAME CRACKED AT STATION 907, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,095 hrs · 32,936 cycles

FRAME CRACKED AT STATION 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,095 hrs · 32,936 cycles

FRAME CRACKED AT STATION 727B, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,095 hrs · 32,936 cycles

LT NR 1 WINDOW FRAME UPPER OTBD CORNER OF CD POST UPPER TWO FASTENER HOLES IN VERTICAL LEG OF FRAME CRACKED. R&R FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,095 hrs · 32,936 cycles

FRAME CRACKED AT STATION 907 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,095 hrs · 32,936 cycles

FRAME CRACKED AT STATION 727D STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,095 hrs · 32,936 cycles

FRAME CRACKED AT STATION 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 55,095 hrs · 32,936 cycles

LT HORIZONTAL STABILIZER STATION 129.50,17.5-19.0 INCHES AFT OF LE CRACKED IN RIB. REPAIRED RIB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,094 hrs · 32,936 cycles

RT NR 3 WINDOW FRAME FASTENER HOLE CRACKED THIRD HOLE UP FROM BOTTOM. REPAIRED FASTENER HOLE IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,095 hrs · 32,936 cycles

LT SIDE SECOND HOLE UP FROM BOTTOM ON NR 3 WINDOW FRAME HOLE CRACKED. R&R FRAME IAW DRAWING.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 55,095 hrs · 32,936 cycles

LT HORIZONTAL STABILIZER STATION 101.9 RIB CRACKED AT 28.5 -30.0 INCHES AFT OF LE. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 55,095 hrs · 32,936 cycles

LT HORIZONTAL STABILIZER STATION 101.9, 37.5-39.0 INCHES AFT OF LE RIB CRACKED. REPAIRED RIB IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,296 hrs · 32,439 cycles

LEFT EMERGENCY EGRESS AISLE LIGHT INOP AT ROW 13. R & R LIGHT IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 51,839 hrs · 30,913 cycles

OVERWING CEILING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER AMM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 51,560 hrs · 30,721 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 120.30 RIB. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 51,560 hrs · 30,721 cycles

LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 138.70 RIB. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 51,560 hrs · 30,721 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 129.50 RIB. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 51,560 hrs · 30,721 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 101.90 RIB. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,571 hrs · 29,037 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 48,571 hrs · 29,037 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR BEAM CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 48,571 hrs · 29,037 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 48,571 hrs · 29,037 cycles

DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — CRACKED (CABIN) · airframe 439,366 hrs · 26,339 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CABIN EMERGENCY LIGHT BATTERY PACK M1673 INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING TANK STIFFENER CRACKED AT BS 540+7, LBL 15. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING TANK STIFFENER CRACKED AT BS 540+7, RBL 55. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING TANK STIFFENER CRACKED AT BS 540+7, LBL 55. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING TANK STIFFENER CRACKED AT BS 540+7, LBL 42. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING TANK STIFFENER CRACKED AT BS 540+7, RBL 7. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING TANK STIFFENER CRACKED AT BS 540+7, RBL 42. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING TANK STIFFENER CRACKED AT BS 540+7, LBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING TANK STIFFENER CRACKED AT BS 540+7, LBL 7. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING TANK STIFFENER CRACKED AT BS 540+7, LBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 663 BETWEEN LBL 34 TO RBL 41. REPAIRED WEB PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772 AT RBL 3. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, BETWEEN RBL 26 TO RBL 38. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 8. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, BETWEEN RBL 6 TO LBL 12. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,521 hrs · 26,106 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT BS 986, BETWEEN RBL 36 TO RBL 8. REMOVED AND REPLACED FLOORBEAM UPPER T-CHORD PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 42,349 hrs · 25,389 cycles

R2 DOOR EVAC SLIDE OUT OF POSITION. RE-INSTALLED SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 41,091 hrs · 24,579 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: COVER — LOOSE (CABIN) · airframe 40,962 hrs · 24,504 cycles

FWD GALLEY EEPS LIGHT COVER LOOSE. REMOVED AND REPLACED BASE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 3,980 hrs · 23,788 cycles

R1 DOOR EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 39,714 hrs · 23,736 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE LT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,714 hrs · 23,736 cycles

DURING SCHEDULED HC2 CHECK, LT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: TRACK — WORN (CABIN) · airframe 39,714 hrs · 23,736 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK WORK AT ROW 16. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — DAMAGED (EVAC SLIDE) · airframe 39,714 hrs · 23,736 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE COVER LATCH INOP. REMOVED AND REPLACED SLIDE PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,714 hrs · 23,736 cycles

DURING SCHEDULED HC2 CHECK, RT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 39,714 hrs · 23,736 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 39,598 hrs · 23,665 cycles

DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EVACUATION SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED SLIDE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 38,618 hrs · 23,070 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. REPLACED LENS PER MM.

Part: SKIN — CRACKED (T/E FLAP) · airframe 38,305 hrs · 22,869 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT LT AFT INBOARD FLAP. REPAIRED PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 37,285 hrs · 22,270 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 37,065 hrs · 22,136 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. FOUND LOOSE WIRE AT TB505YA1. SECURED WIRE PER WDM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 37,064 hrs · 22,135 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 37,065 hrs · 22,135 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM.

Part: FLAP TRACK — LOOSE (LT WING) · airframe 37,065 hrs · 22,135 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING OUTBOARD T/E AFT, NR 2 FLAP TRACK LOOSE. REMOVED AND REPLACED FLAP TRACK PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 35,095 hrs · 20,898 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 157.10. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 35,095 hrs · 20,898 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,072 hrs · 20,338 cycles

DURING SCHEDULED MV1 CHECK, FOUND RIGHT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: COVER — MISSING (CABIN) · airframe 33,094 hrs · 19,811 cycles

EEPLS COVER MISSING AT ROW 9 ABC. INSTALLED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 33,094 hrs · 19,811 cycles

EEPLS COVER MISSING AT ROW 10 ABC. INSTALLED COVER PER MM.

Part: HYDRAULIC LINE — CHAFED (MLG W/W) · airframe 32,526 hrs · 19,500 cycles

AIR TURNBACK, AT FL 350 MASTER CAUTION AND HYDRAULIC LIGHTS ILLUMINATED, HYDRAULIC B-SYSTEM QUANTITY AT -0-. FOUND B-HYDRAULIC SYSTEM SPOILER PRESSURE LINE CHAFED. REMOVED AND REPLACED SPOILER PRESSURE LINE PER MM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 31,868 hrs · 19,117 cycles

ON APPROACH GEAR WARNING LIGHT ILLUMINATED, CYCLED GEAR, NORMAL INDICATIONS. REMOVED AND REPLACED DOWN LOCK ACTUATOR PER MM.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 30,153 hrs · 18,157 cycles

AIR TURNBACK, AT FIRST POWER REDUCTION NR 1 ENGINE COMPRESSOR STALLED, 4 TO 5 BANGS, ENGINE RAN NORMAL AFTER THE STALLS. REMOVED AND REPLACED NR 1 ENGINE PER MT AND MM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 29,332 hrs · 17,670 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986.5, BETWEEN BL 0 TO LBL 44. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 29,322 hrs · 17,670 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986.5, BETWEEN BL 0 TO RBL 44. REPAIRED FLOORBEAM PER SWA EA & SRM.

Part: FRAME — CORRODED (BS 332) · airframe 29,322 hrs · 17,670 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FRAME CORRODED AT R1 DOOR CUTOUT, AFT FRAME, BS 332, WL 211. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,322 hrs · 17,670 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 40 TO RBL 60. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (BS 508-512A) · airframe 29,322 hrs · 17,670 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 508 & BS 512A, BL 0. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 967) · airframe 29,322 hrs · 17,670 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 967, RBL 27.5. REPAIRED FLOORBEAM PER SRM.

Part: LIGHT — BROKEN (FWD GALLEY) · airframe 26,964 hrs · 16,338 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,285 hrs · 15,978 cycles

DURING SCHEDULED MV2 CHECK, FOUND SEVERAL CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 26,104 hrs · 15,875 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR STRAPS LOOSE. SECURED STRAPS PER MM.

Part: COVER — DISLODGED (EMER EXIT SIGN) · airframe 25,062 hrs · 15,286 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN FELL OFF. REINSTALLED SIGN COVER PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,890 hrs · 14,037 cycles

DURING SCHEDULED HC1 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 6 ABC, INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,890 hrs · 14,037 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: GLOWSTRIP — OUT OF POSITION (CABIN) · airframe 22,748 hrs · 13,947 cycles

DURING SPV, FOUND PHOTOLUMINESCENT STRIP OUT OF POSITION. PLACED PHOTOLUMINESCENT STRIP IN PROPER POSITION PER ACO.

Part: BATTERY — INOPERATIVE (R2 DOOR) · airframe 22,033 hrs · 13,563 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,018 hrs · 12,985 cycles

DURING SCHEDULED MS CHECK, FOUND MID CABIN AISLE AND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BATTERY PACK PER MM.

Part: LENS — LOOSE (SVC DOOR) · airframe 18,113 hrs · 11,325 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE VIEWING WINDOW LENS LOOSE. SECURED LENS PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 17,487 hrs · 10,952 cycles

EEPLS WIRING ON THE LT SIDE AT ROW 9 IS NOT SECURE. SECURED THE EEPLS WIRING AT ROW 9 PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 17,349 hrs · 10,881 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB HINGE ATTACH POINTS NR 2 AND NR 4 WORN. REMOVED AND REPLACED HARDWARE AND BUSHINGS AT NR 2 AND NR 4 HINGE ATTACH POINTS PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 17,349 hrs · 10,881 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11075, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHING AT NR 1 HINGE ATTACH POINT PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 17,194 hrs · 10,787 cycles

EEPLS INOP AT FWD CABIN. REMOVED AND REPLACED (2 EA) LIGHT ASSY'S AND REPAIRED WIRING PER MM.

Part: HINGE — WORN (RT ELEVATOR) · airframe 16,587 hrs · 10,442 cycles

DURING SCHEDULED A2 CHECK, FOUND RT ELEVATOR TAB NR 2 AND NR 3 HINGE ATTACH POINTS WORN. REMOVED AND REPLACED NR 2 AND NR 3 HINGES PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 15,996 hrs · 10,114 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB HARDWARE AND BUSHINGS ON ALL 4 HINGE ATTACH POINTS PER MM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 15,752 hrs · 9,976 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT PRESSURE BULKHEAD HAS OIL CANNING AT 2 O'CLOCK POSITION. REPAIRED BULKHEAD PER SAW EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,713 hrs · 9,956 cycles

DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 15,503 hrs · 9,836 cycles

EEPLS WIRES LOOSE IN MID CABIN. REPAIRED EEPLS WIRES PER MM.

Part: TOILET — CLOGGED (LAVATORY) · airframe 15,330 hrs · 9,737 cycles

DIVERSION, BOTH LAV'S (FWD AND AFT) WOULD NOT FLUSH. UNCLOGGED AFT LAV AND REMOVED AND REPLACED FWD LAV PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 13,341 hrs · 8,588 cycles

DURING SCHEDULED SERVICE CHECK, (SI 11038-55) RT ELEVATOR TAB BUSHINGS WORN AT HINGES NR 1 AND NR 4. REMOVED AND REPLACED BUSHINGS PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 13,341 hrs · 8,588 cycles

DURING SCHEDULED SERVICE CHECK, (SI 11038-55) LT ELEVATOR TAB BUSHINGS WORN AT HINGES NR 2, NR 3 AND NR 4. REMOVED AND REPLACED BUSHINGS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 12,799 hrs · 8,269 cycles

EEPLS WIRES EXPOSED AT ROW 8. REINSTALLED COVER PER MM.

Part: BUSHING — WORN (RH ELEVATOR) · airframe 12,273 hrs · 7,980 cycles

DURING SCHEDULED SERVICE CHECK, RH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R HINGE BUSHINGS # 1 - # 4 PER MM.

Part: BUSHING — WORN (RH ELEVATOR) · airframe 11,790 hrs · 7,683 cycles

DURING SCHEDULED SERVICE CHECK, SI 11052-55, FOUND RH ELEVATOR TAB # 3 HINGE BUSHING WORN. R&R HINGE BUSHING PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 11,120 hrs · 7,301 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB INBD HINGE BUSHING WORN. REMOVED AND REPLACED BUSHING AND BOLT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,998 hrs · 7,230 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS LIGHT INOP AT ROW 15. RELAMPED EEPLS PER MM.

Part: CASTING — CRACKED (RT MLG WW) · airframe 10,172 hrs · 6,739 cycles

DURING SCHEDULED C3 CHECK, FOUND RT MLG WHEEL WELL AFT SUPPORT WEB & SUPPORT CASTING CRACKED. REMOVED AND REPLACED WEB AND CASTING PER SRM.

Part: TRACK — LOOSE (CABIN) · airframe 9,733 hrs · 6,475 cycles

FLOOR TRACK LIGHTING LOOSE. SECURED TRACK LIGHTING PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 8,975 hrs · 6,003 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE ASSY PER MM.

Part: ENGINE — FAILED (NR 2) · airframe 7,462 hrs · 5,077 cycles

AIR TURNBACK / IN FLT ENG SHUT-DOWN. SHORTLY AFTER TAKEOFF, A LOUD BANG NOISE AND FAILURE OF NR 2 ENG. AFTER LANDING, METAL WAS FOUND LAYING IN TAILPIPE SECTION. REMOVED AND REPLACED NR 2 ENG PER MM.

Part: SKIN — CRACKED (BS 222)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE EXTERNAL SKING WITH 2 EACH .125 INCH LONG CRACKS BELOW CAPT'S SLIDING WINDOW, BS 222.. REPAIRED SKIN PER SRM.

Part: CONTROLLER — INOPERATIVE (COCKPIT)

DIVERSION, ACFT RADAR INOP. DIVERTED TO BHM. REMOVED AND REPLACED RADAR CONTROL PANEL PER MM.

Part: LAMP — FAILED (ROW 13 ABC)

DURING SCHEDULED SC CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 13ABC INOP. RELAMPED PER BOEING MM.

Part: LAMP — FAILED (CABIN)

DURING SCHEDULED SC CHECK, FOUND BIN EMERGENCY LIGHT INOP AT ROW 13 ABC. RELAMPED PER M/M, OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (NR 2 ENGINE EEC)

AIRCRAFT WITH NR 2 ENGINE SHUTDOWN, APU ELEC ON LINE, NR 1 THROTTLE AT IDLE, UNCOMMANDED ENG ACCELERATION TO 85 PERCENT N1, APPROX 10 SEC, THEN RETURNED TO IDLE. (LOG PAGE 169881). FOUND J2 CONNECTOR ON EEC LOOSE, CLEANED AND SECURED OPERATED ENG PER BOEING MM. NO FAULTS FOUND.