N789SW

Part: SLIDE — FAILED (R2 DOOR) · airframe 66,122 hrs · 38,792 cycles

DOOR SLIDE FAILED TO DEPLOY PROPERLY. R&R PER 725-61-06 AND 725-66-01.

Part: SLIDE — PULLED (L1 DOOR) · airframe 65,899 hrs · 38,639 cycles

L1 DOOR SLIDE GIRT BAR CAUGHT ON JET BRIDGE. / REPACKED SLIDE PER MT.

Part: LENS — MISSING (CABIN) · airframe 63,080 hrs · 36,823 cycles

L1 DOOR LIGHTED EXIT SIGN MISSING DIRECTIONAL ARROW. R&R LENS IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 63,080 hrs · 36,823 cycles

L2 DOOR EMERGENCY EXIT LENS MISSING DIRECTIONAL ARROW. R&R LENS IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,965 hrs · 36,760 cycles

LT BIN EMERGENCY EXIT LIGHT INOP AT ROW 6. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,965 hrs · 36,760 cycles

LT OVERWING EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,965 hrs · 36,760 cycles

LT EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,965 hrs · 36,760 cycles

FORWARD LT EMERGENCY LIGHT INOP AT M1675. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,965 hrs · 36,760 cycles

FORWARD RT EMERGENCY LIGHT INOP AT M1675. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 62,965 hrs · 36,760 cycles

FORWARD LT EMERGENCY LIGHT INOP AT M1674. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,965 hrs · 36,760 cycles

FORWARD RT EMERGENCY LIGHT INOP AT M1674. R&R BATTERY PACK PER AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

PASSENGER CABIN SEAT TRACK CORRODED BETWEEN BS 540 TO BS 727A, RBL 25. R&R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

SEAT TRACK CORRODED BETWEEN BS 540 TO BS 727A, LBL 45. R&R SEAT TRACK IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 62,965 hrs · 36,760 cycles

VERTICAL PRESSURE BULKHEAD WEB CRACKED AT BS 663, RBL 29. REPAIRED WEB IAW ER AN EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

VERTICAL PRESSURE BULKHEAD ATTACH ANGLE CRACKED AT BS 663, RBL 34. REPAIRED ANGLE IAW ER AND EA.

Part: WEB — CORRODED (LT WING) · airframe 62,965 hrs · 36,760 cycles

LT FORWARD FUEL BOOST PUMP LOWER GROUND STRAP POSITIONS ON SPAR SKIN CORRODED. REPAIRED WEB IAW EA.

Part: STIFFENER — CORRODED (LT MLG WW) · airframe 62,965 hrs · 36,760 cycles

LT MAIN LANDING GEAR WHEEL WELL PRESSURE DECK STIFFENER CORRODED AT BS 713.5, BETWEEN LBL 63 TO LBL 68. REPAIRED STIFFENER IAW ER AND EA.

Part: ANGLE — CORRODED (LT MLG WW) · airframe 62,965 hrs · 36,760 cycles

LT MAIN LANDING GEAR WHEEL WELL PRESSURE DECK WEB CLOSEOUT ANGLE CORRODED AT BS 669, BETWEEN LBL 63 TO LBL 68. REPAIRED ANGLE IAW ER AND EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

CREASE BEAM WEB LOWER SURFACE CORRODED AT BS 691, LBL 63. R&R CREASE BEAM WEB IAW SRM AND DWG.

Part: STIFFENER — CORRODED (LT MLG WW) · airframe 62,965 hrs · 36,760 cycles

LT MAIN LANDING GEAR WHEEL WELL PRESSURE DECK STIFFENER CORRODED AT BS 704, BETWEEN LBL 63 TO LBL 68. REPAIRED STIFFENER IAW ER AND EA.

Part: STIFFENER — CORRODED (RT MLG WW) · airframe 62,965 hrs · 36,760 cycles

RT MAIN LANDING GEAR WHEEL WELL PRESSURE DECK STIFFENER CORRODED AT BS 719, BETWEEN RBL 63 TO RBL 68. REPAIRED STIFFENER IAW ER AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

FLOORBEAM CORRODED AT BS 967, LBL 27. REPAIRED FLOORBEAM IAW EA AND ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN LBL 20 TO LBL 45. REPAIRED FLOORBEAM IAW ER AND EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 500C+15, RBL 24. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A+4 TO BS 500D, LBL 24. R&R SUPPORT PER SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

STIFFENER CRACKED AT BS 663, 3" OUTBOARD OF KEEL BEAM ON THE LT SIDE. R&R STIFFENER IAW DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

AFT CARGO BAY SUB WEB THRESHOLD CORRODED. R&R THRESHOLD IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 47. R&R INTERCOSTAL IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

L1 DOOR MOP SILL CORRODED BETWEEN BS 312 TO BS 344. R&R MOPSILL IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727C+10 TO BS 767, RBL 24. R&R SUPPORT IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

FORWARD CARGO BAY SUB WEB THRESHOLD CORRODED. R&R THRESHOLD IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 887 TO BS 947, RBL 20. R&R SUPPORT PER SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

R2 DOOR MOP SILL CORRODED BETWEEN BS 968 TO BS 990. R&R MOP SILL IAW DWG AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 410, RBL 24. R&R SUPPORT PER SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,965 hrs · 36,760 cycles

AFT CARGO BAY CARGO TRACK CORRODED AT BS 936, RBL 14. R&R CARGO TRACK IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

L2 DOOR MOP SILL CORRODED BETWEEN BS 959 TO BS 986. R&R MOP SILL IAW DWG AND SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,965 hrs · 36,760 cycles

AFT CARGO BAY CARGO TRACK CORRODED AT BS 942, LBL 3. R&R TRACK IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,965 hrs · 36,760 cycles

AFT CARGO BAY CARGO TRACK CORRODED BETWEEN BS 787 TO BS 887, RBL 14. R&R TRACK IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 847 TO BS 867, RBL 20. R&R SHIELD IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

FORWARD CARGO BAY AFT BULKHEAD C ENTER PANEL LOWER SUPPORT CORRODED AT BS 500D, BETWEEN LBL 24 TO RBL 24. R&R SUPPORT PER SRM AND DWG.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 62,965 hrs · 36,760 cycles

AFT CARGO BAY CARGO TRACK TIE DOWN CORRODED AT BS 907, LBL 3. R&R TIE DOWN IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

AFT CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT CORRODED. R&R SUPPORT PER SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 494 TO BS 500A, RBL 24. R&R SUPPORT PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 20 TO RBL 45. REPAIRED FLOORBEAM IAW ER AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

INTERCOSTAL CRACKED BETWEEN BS 294 TO BS 312, RBL 35. R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

FLOORBEAM CRACKED AT BS 328, RBL 24. REPAIRED FLOORBEAM PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 24. R&R SUPPORT IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

FLOORBEAM CORRODED AT BS 967, LBL 33. REPAIRED FLOORBEAM IAW EA AND ER.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 47. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

L1 DOOR SCUFF PLATE INNER SUPPORT CORRODED BETWEEN BS 318 TO BS 340. R&R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 35. R&R INTERCOSTAL IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 794, RBL 24. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

L1 DOOR SCUFF PLATE MIDDLE SUPPORT CORRODED BETWEEN BS 318 TO BS 340. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 62,965 hrs · 36,760 cycles

RT WING INBOARD UPPER TRAILING EDGE PANEL SUPPORT CLIP JUST OUTBOARD OF WBL 70.5 CRACKED. R&R CLIP PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

FLOOR SUPPORT CRACKED AT BS 317, RBL 32. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

VAPOR BARRIER UPPER SUPPORT ANGLE CRACKED AT BS 663, RBL 8. REPAIRED ANGLE IAW ER AND EA.

Part: PLATE — CRACKED (RT WING) · airframe 62,965 hrs · 36,760 cycles

RT WING LOWER TRAILING EDGE WIGGLE PLATE AT ORSS 261 CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,965 hrs · 36,760 cycles

FLOOR SUPPORT CRACKED AT BS 284.5, BL 0. R&R SUPPORT IAW SRM & DWG.

Part: PLATE — CRACKED (LT WING) · airframe 62,965 hrs · 36,760 cycles

LT WING LOWER TRAILING EDGE WIGGLE PLATE AT ORSS 261 CRACKED. R&R WIGGLE PLATE PER SRM.

Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 62,965 hrs · 36,760 cycles

VAPOR BARRIER UPPER SUPPORT ANGLE CRACKED AT BS 663, LBL 8. REPAIRED ANGLE IAW ER AND EA.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 62,965 hrs · 36,760 cycles

LOWER COMPOSITE BULKHEAD CRACKED AT BS 663, LBL 12. REPAIRED BULKHEAD IAW SRM.

Part: COVER — MISSING (EXIT SIGN) · airframe 61,950 hrs · 36,102 cycles

RT EMERGENCY EXIT SIGN MISSING AT ROW 12. INSTALLED SIGN COVER PER AMM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 61,816 hrs · 36,022 cycles

R1 DOOR SLIDE LOOSE FROM HOUSING. SECURED THE SLIDE IAW MT.

Part: COVER — CRACKED (EMERGENCY EXIT) · airframe 61,056 hrs · 35,548 cycles

LEFT EMERGENCY EXIT DOOR LOWER HANDLE COVER CRACKED AT THE TOP. R & R THE COVER IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,138 hrs · 34,913 cycles

FUSELAGE SKIN CRACKED AT BS 633, RT SIDE EMERGENCY EXIT UPPER DOOR CUT OUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,138 hrs · 34,913 cycles

FUSELAGE SKIN CRACKED AT BS 622, RT SIDE EMERGENCY EXIT UPPER DOOR CUT OUT. REPAIRED SKIN PER EA.

Part: LIGHT — BROKEN (GALLEY) · airframe 58,751 hrs · 34,055 cycles

FWD GALLEY EXIT LIGHT BROKEN. R & R THE LIGHT ASSY IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,430 hrs · 33,860 cycles

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

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 58,241 hrs · 33,751 cycles

RIGHT WINDOW EXIT EMERGENCY LIGHT COVER MISSING. REPLACED THE COVER IAW AMM.

Part: PLATE — CRACKED (LT WING) · airframe 58,079 hrs · 33,656 cycles

LT WING AFT LOWER FIXED PANEL INBOARD WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 56,963 hrs · 32,986 cycles

RT OVERWING DOOR EMERGENCY EXIT SIGN INOP. R&R FUSE PER AMM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 56,963 hrs · 32,986 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 767 TO BS 792, RBL 22. R&R PLATE IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 56,963 hrs · 32,986 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 727+4 TO BS 767, RBL 22. R&R PLATE PER SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,963 hrs · 32,986 cycles

AFT CARGO BAY STRINGER CLIP CRACKED AT BS 727A, STR 26R. R&R CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,963 hrs · 32,986 cycles

LT FRAME WEB CRACKED AT BS 727, WL 200. REPAIRED WEB PER EA.

Part: ANGLE — CRACKED (BS 727 BULKHEAD) · airframe 56,963 hrs · 32,986 cycles

LEFT WHEEL WELL BULKHEAD WEB ANGLE CRACKED AT BS 727. R & R THE ANGLE IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (BS 727A-727B) · airframe 56,963 hrs · 32,986 cycles

AFT CARGO BAY, CARGO TRACK CORRODED BETWEEN BS 727A TO 727B, RBL 13.84. R & R THE CARGO TRACK IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 56,963 hrs · 32,986 cycles

EXTERNAL POWER RECEPTACLE DOOR CUTOUT INNER BONDED DOUBLER CRACKED AFT LOWER CORNER. R & R DOUBLER IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 56,278 hrs · 32,568 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 56,278 hrs · 32,568 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 56,278 hrs · 32,568 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 56,278 hrs · 32,568 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 56,278 hrs · 32,568 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R & R BATTERY PACK IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 55,717 hrs · 32,264 cycles

MID CABIN OVERHEAD EXIT LIGHT LENS LOOSE. R & R LIGHT IAW AMM.

Part: SIGN — UNSECURE (CABIN) · airframe 55,263 hrs · 32,007 cycles

R1 DOOR LOWER EXIT SIGN FELL OFF. REINSTALLED SIGN IAW MM.

Part: TIRE — BURST (RT MLG) · airframe 55,092 hrs · 31,909 cycles

NUMBER 3 MLG TIRE BURST ON TAKEOFF. R & R NR 3 WHEEL ASSEMBLY IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 54,970 hrs · 31,835 cycles

R2 DOOR EMER EVAC SLIDE SAFETY COVER OUT OF POSITION. REPOSITIONED SLIDE IAW SIP.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,734 hrs · 31,116 cycles

LONGITUDINAL FLOORBEAM OTBD FLANGE, AFT HOLE NR 8, CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,734 hrs · 31,116 cycles

SEAT TRACK OTBD FLANGE FASTENER HOLE NR 2, CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,734 hrs · 31,116 cycles

LONGITUDINAL FLOORBEAM OTBD FLANGE AFT HOLE NR 10, CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,734 hrs · 31,116 cycles

LONGITUDINAL FLOORBEAM INBD FLANGE, FWD AFT HOLE NR 9 & 10, CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,734 hrs · 31,116 cycles

LONGITUDINAL FLOORBEAM INBD FLANGE AFT HOLE NR 8, CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,734 hrs · 31,116 cycles

LONGITUDINAL FLOORBEAM INBD FLANGE, FWD AFT HOLE NR 9 & 10, CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,734 hrs · 31,116 cycles

LONGITUDINAL FLOORBEAM OTBD FLANGE FWD HOLE NR 9, CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,734 hrs · 31,116 cycles

BULKHEAD CRACKED AT BS 663, BETWEEN LBL 25 - 45. REPAIRED BULKHEAD IAW SRM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 52,843 hrs · 30,586 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN COVER LOOSE. R & R SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,801 hrs · 30,000 cycles

RIGHT EMER EXIT LIGHT INOPERATIVE AT ROW 11. RELAMPED LIGHT IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,801 hrs · 30,000 cycles

M01675 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: SIGN — MISSING (CABIN) · airframe 51,193 hrs · 29,651 cycles

R2 DOOR EMER EXIT SIGN MISSING. INSTALLED SIGN ASSEMBLY IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 51,193 hrs · 29,651 cycles

L2 DOOR EMER EXIT SIGN LOOSE. R & R SIGN ASSEMBLY IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 50,633 hrs · 29,335 cycles

FORWARD GALLEY EXIT SIGN LENS MISSING. INSTALLED LENS IAW MM.

Part: COVER — MISSING (EXIT SIGN) · airframe 49,937 hrs · 28,919 cycles

R2 DOOR EMER EXIT SIGN COVER MISSING. INSTALLED COVER IAW SIP.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 47,043 hrs · 27,198 cycles

NR 1 RT COCKPIT WINDOW FRAME CRACKED. R & R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 47,043 hrs · 27,198 cycles

NR 1 LT COCKPIT WINDOW FRAME CRACKED. R & R FRAME IAW ACO.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 47,043 hrs · 27,198 cycles

RT HORIZONTAL STABILIZER STATION 129.5 RIB AFT END LOWER FLANGE INBD SIDE CRACKED IN RADIUS. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 47,043 hrs · 27,198 cycles

RT HORIZONTAL STABILIZER STATION 120.3 RIB AFT END LOWER FLANGES OTBD & INBD SIDES CRACKED IN RADIUS. REPAIRED RIB IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 47,043 hrs · 27,198 cycles

LT NR 3 WINDOW FRAME E-F POST 2ND FASTENER HOLE FROM BOTTOM CRACKED. R & R FRAME IAW E.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,853 hrs · 27,083 cycles

LT EMERGENCY LIGHT ON OVERHEAD BIN INOPERATIVE AT ROW 6. RELAMPED LIGHT IAW MM.

Part: RETAINER — CRACKED (LT WING) · airframe 45,171 hrs · 26,074 cycles

LEFT WING LOWER T/E SHELF PANEL AFT SEAL RETAINER CRACKED. REMOVED AND REPLACED RETAINER PER MM.

Part: RETAINER — CRACKED (LT WING) · airframe 45,171 hrs · 26,074 cycles

LEFT WING T/E AFT BULB SEAL RETAINER CRACKED JUST OTBD OF NR 3 FLAP TRACK. REMOVED & REPLACED SEAL RETAINER PER M/M.

Part: SKIN — CRACKED (LE SLAT) · airframe 45,171 hrs · 26,074 cycles

RIGHT WING NR 6 SLAT SKIN CRACKED FROM AFT OUTBOARD FASTENER HOLE TO EDGE AT ACTUATOR ATTACH FITTING. REMOVED AND REPLACED NR 6 SLAT IAW MM.

Part: PLATE — CRACKED (RT WING) · airframe 45,171 hrs · 26,074 cycles

RIGHT WING LOWER TRAILING EDGE PANEL ATTACH WIGGLE PLATE INBOARD OF ENGINE STRUT CRACKED. REMOVED AND REPLACED WIGGLE PLATE PER MM.

Part: STRIP — LOOSE (CABIN) · airframe 44,409 hrs · 25,633 cycles

ROW 8 EMERGENCY LIGHTING STRIP BOTH SIDES COMING UP. SECURED STRIP PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,874 hrs · 25,286 cycles

GALLEY AREA EMERGENCY LIGHTS INOP AT THE ENTRY DOOR. REMOVED AND REPLACED BATTERY IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 43,874 hrs · 25,286 cycles

FWD LAV AFT WALL LOWER EXIT LIGHT IS BROKEN. REPLACED FWD LAV AFT WALL EXIT LIGHT ASSEMBLY AND OPERATIONAL CHECKED GOOD IAW AMM 33-51-01-960-802.

Part: SIGN — BROKEN (CABIN) · airframe 43,874 hrs · 25,286 cycles

AFT LAV FWD WALL LOWER EXIT LIGHT IS BROKEN. REPLACED THE EXIT SIGN ON AFT LAV, FWD WALL IAW AMM 33-51-01 ALSO OPS CHECKED OK.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

AC BAY STA 663 RT SIDE BULKHEAD CRACKED. REPAIRED BULKHEAD IAW EA.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

R1 SERVICE DOOR LOWER CENTER THRESHOLD, RELIEF CUTOUT HAS CRACK. R1 SERVICE DOOR CENTER THRESHOLD REPAIRED ON SHOP WORK ORDER 26095-8400-0001 AND EA 1-53-2076.

Part: COLLAR — MISSING (CABIN) · airframe 43,874 hrs · 25,286 cycles

AFT CABIN FLOOR FRAME AT STA 986 UNDER 2R CREASE BEAM HAS SEVERAL HI LOCK COLLARS AT LEAST 5 MISSING. INSTALLED COLLARS AT AFT CABIN FLOOR FRAME AT STA 986 UNDER 2R CREASE BEAM IAW B737 SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

PASSENGER CABIN STA 727, STR 14R, FRAME CRACKED. REMOVED AND REPLACED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

STA 400 BETWEEN STR 8R & 9R, FRAME HAS A CRACK INDICATION. FABRICATED REPAIR ANGLES AND INSTALLED PER SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

AFT CARGO COMP STA 727 PANEL BRACKET, 8" ABOVE FLOOR 8" RIGHT OF APU DUCT CRACKED AT FASTENER (MARKED). REPLACED CRACKED BRACKET AT AFT CARGO COMPARTMENT, STA 727 PANEL BRACKET, 8" ABOVE FLOOR, 8" RIGHT OF APU DUCT IAW SRM 51-40-02.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 43,874 hrs · 25,286 cycles

CARGO COMP FLOOR TRACK STA 793-818 CORROSION AT FASTENER HOLES RBL 14. REMOVED AND REPLACED TRACK IAW SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

CARGO COMP DOOR SILL WEB HAD CORROSION AT FASTENER HOLES 10-31. REMOVED AND REPLACED WEB IAW SRM.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 43,874 hrs · 25,286 cycles

LEFT HORIZONTAL STAB BOTTOM SLIDER SEAL CRACKED AFT TOP EDGE. REMOVED AND REPLACED LEFT HORIZONTAL STAB LOWER SLIDING SEAL IAW AMM 53-31-31-400-803

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

CARGO COMP RIGHT Z-ANGLE STA 747 TO 767 CORROSION AT FASTENER HOLES. REMOVED AND REPLACED IAW BOEING DWG SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

STA 747 STR 8L FRAME CRACKED AT I/B FASTENER. REMOVED AND REPLACED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

STA 867, STR 8L FRAME CRACKED AT I/B FASTENER. REMOVED AND REPLACED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

STA 400 STR 8L FRAME CRACKED AT I/B FASTENER. REMOVED AND REPLACED FRAME IAW EA.

Part: EXPANSION JOINT — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

STA 540 LBL 1 EXPANSION JOINT IS CRACKED. REMOVED EXPANSION JOINT AT BS 540 LBL 'O'-24 AT FLOOR STRUCTURE. INSTALLED NEW EXPANSION JOINT IAW SRM 51-40-02 AND BOEING DWG 143A0060 CIC AREA IAW AMM 51-21-91-620-802.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

PASSENGER CABIN STA 716 BETWEEN STR 16L AND 17L, MLG SUPPORT FRAME SIDE CORRODED. REMOVED AND REPLACED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

STA 360, STR 8R FRAME CRACKED AT I/B FASTENER. REMOVED AND REPLACED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

STA 827 STR 8R FRAME CRACKED AT I/B FASTENER. REMOVED AND REPLACED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

STA 480 STR 8L FRAME CRACKED AT I/B FASTENER. REMOVED AND REPLACED FRAME IAW EA SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

STA 480, STR 8R FRAME CRACKED AT I/B FASTENER. REMOVED AND REPLACED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

PASSENGER CABIN STA 960 TO 986 RIGHT CREASE BEAM INNER CHORD CORRODED. REMOVED AND REPLACED CREASE BEAM IAW SRM BOEING DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

PASSENGER CABIN, STA 312 TO STA 328, LBL 44.5, INTERCOSTAL CRACKED AT FASTENER HOLE. (MARKED) REMOVED AND REPLACED PASSENGER CABIN INTERCOSTAL AT STA 312 TO STA 328 LBL 44.5 IAW SRM 51-40-02 AND SRM 51-40-05 AND DWG 141A5400.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

PASSENGER CABIN BL 0, STA 344 TO 360, AFT HOLE ON INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW SRM & DWG.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 43,874 hrs · 25,286 cycles

RIGHT MLG W/W BULKHEAD VERTICAL STIFFENER CRACKED AT LOWER END BS 663, RBL 27. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 43,874 hrs · 25,286 cycles

LEFT MLG W/W VERTICAL STIFFENER CRACKED AT LOWER END COMMON BS 663 BULKHEAD LBL 27. REMOVED AND REPLACED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

RIGHT A/C BAY FWD SIDE OF BS 663 BULKHEAD STIFFENER CRACKED AT I/B END. REMOVED AND REPLACED STIFFENER IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

PASSENGER CABIN, STA 312 TO STA 328, RBL 30, INTERCOSTAL CRACKED AT BOTH FASTENER HOLES. (MARKED) REMOVED DAMAGED INTERCOSTAL AND LOCATED DRILLED AND INSTALLED NEW INTERCOSTAL IAW BOEING DRAWING 141A5400 AND SRM 51-40-02-0G-0, 51-40-05-0G-0.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

PASSENGER CABIN STA 294 TO 328, RIGHT CREASE BEAM INNER CHORD CORRODED. REMOVED AND REPLACED CREASE BEAM IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

PASSENGER CABIN BL 0 STA 277 TO 294.5 INTERCOSTAL CRACKED AT BOTH FASTENER HOLES. REMOVED AND REPLACED INTERCOSTAL IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

PASSENGER CABIN STA. 986 AT LBL 38, T-CAP CORRODED ON TOP SURFACE. REMOVED AND REPLACED T-CHORD IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,874 hrs · 25,286 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 129.50, 18 INCHES FORWARD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: STRUCTURE — CRACKED (LE SLAT) · airframe 43,874 hrs · 25,286 cycles

RIGHT WING NR 7 SLAT CRACKED BELOW ACTUATOR ROD END AT FASTENER HOLE. REMOVED NR 7 SLAT FLEX SKIN, PANELS 624CB, 624DB, 624EB. REPAIRED CRACK ON RT WING NR 7 SLAT BELOW ACTUATOR ROD END AT FASTENER HOLE IAW SRM 57-42-01-2R-8 REPAIR 8, PLUS RE-INSTALLED, A

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

CARGO COMPARTMENT STA.500C STR 25L, INTERCOSTAL ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM AND BOEING DWG.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,874 hrs · 25,286 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT REAR SPAR, 5 INCHES INBOARD OF STAB STATION 129.50. REMOVED AND REPLACED SKIN IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

CARGO COMPARTMENT STA 500C SIDE STR 25R, INTERCOSTAL ANGLE CRACKED AT BASE. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,874 hrs · 25,286 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 101.90, 20 INCHES FORWARD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 43,874 hrs · 25,286 cycles

LT WING 3 FLAP TRACK FAIRING CRACK ON LOWER AT LINK ASSY AREA. REMOVED AND REPLACED FAIRING IAW EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,874 hrs · 25,286 cycles

CARGO COMPARTMENT STA 500C STR 25L, INTERCOSTAL ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,874 hrs · 25,286 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 175.50, 10 INCHES FORWARD OF REAR SPAR. REMOVED AND REPLACED SKIN PARTS IAW SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 43,429 hrs · 25,011 cycles

RIGHT EEPLS LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS PER AMM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 43,429 hrs · 25,011 cycles

L1 WINDOW AFT POST C-D FRAME CRACKED AT UPPER CORNER. REPAIRED FRAME PER EA.

Part: LIGHT — WORN (CABIN) · airframe 43,429 hrs · 25,011 cycles

EEPLS WORN BETWEEN ROW 18 TO ROW 20. REMOVED AND REPLACED EEPLS PER AMM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 43,429 hrs · 25,011 cycles

R1 WINDOW AFT POST C-D FRAME CRACKED AT UPPER CORNER. REPAIRED FRAME PER EA.

Part: STRUCTURE — CRACKED (LT HORIZ STAB) · airframe 41,863 hrs · 24,103 cycles

LT HORIZONTAL STABILIZER CRACKED ON LOWER LEFT STAB AT STA 101.90. REPAIRED STABILIZER PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 41,863 hrs · 241,103 cycles

LT HORIZONTAL STABILIZER LOWER LEFT STAB SKIN CRACKED AT STA 129.50. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 41,863 hrs · 24,103 cycles

LT HORIZONTAL STABILIZER LOWER LEFT STAB SKIN CRACKED AT STA 147.90 AFT OF FWD SPAR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 41,863 hrs · 24,103 cycles

LT HORIZONTAL STABILIZER LOWER LEFT STAB SKIN CRACKED AT STA 129.50 AFT OF FWD SPAR. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,117 hrs · 23,678 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 5. RELAMPED LIGHT PER MM.

Part: MOUNT BRACKET — BROKEN (R1 DOOR) · airframe 41,117 hrs · 23,678 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT MOUNTING BRACKET BROKEN. REMOVED AND REPLACED BRACKET PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,117 hrs · 23,678 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,117 hrs · 23,678 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,800 hrs · 23,494 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY DOOR FLOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LAMPS.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 40,375 hrs · 23,232 cycles

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

Part: COVER — LOOSE (EXIT SIGN) · airframe 38,829 hrs · 22,329 cycles

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

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 367,423 hrs · 21,139 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 548, LBL 41. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 367,423 hrs · 21,139 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 548, LBL 14. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 367,423 hrs · 21,139 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 548, RBL 14. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 367,423 hrs · 21,139 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 548, RBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 367,423 hrs · 21,139 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 548, RBL 41. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 367,423 hrs · 21,139 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 548, RBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 367,423 hrs · 21,139 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 548, LBL 54. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 367,423 hrs · 21,139 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 548, LBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 367,423 hrs · 21,139 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 548, LBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 36,655 hrs · 21,091 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 36,547 hrs · 21,025 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT EEPLS COVER LOOSE BETWEEN ROW 4 TO ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,726 hrs · 20,530 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REMOVED AND REPLACED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,726 hrs · 20,530 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REMOVED AND REPLACED FITTING PER EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 34,251 hrs · 19,662 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SPAR SKIN CRACKED AT STA 138.70. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 33,347 hrs · 19,114 cycles

BOTH FWD EMERGENCY FLASHLIGHTS INOP. REMOVED AND REPLACED FLASHLIGHT BATTERIES PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,962 hrs · 18,279 cycles

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

Part: BRACKET — CORRODED (GIRT BAR) · airframe 30,117 hrs · 17,190 cycles

DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR FWD GIRT BAR BRACKET CORRODED AT BS 312, LBL 42. REMOVED AND REPLACED BRACKET PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 30,117 hrs · 17,190 cycles

DURING SCHEDULED 8Y CHECK, FOUND LTR WING O/B AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 30,117 hrs · 17,190 cycles

DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR AFT GIRT BAR BRACKET CORRODED AT BS 344, LBL 58. REMOVED AND REPLACED BRACKET PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,117 hrs · 17,190 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767+6, RBL 12. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,117 hrs · 17,190 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767+6, LBL 3. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,117 hrs · 17,190 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767+6, LBL 12. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,117 hrs · 17,190 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767+6, LBL 17. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,117 hrs · 17,190 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767+6, LBL 9. REPAIRED BEAM PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,761 hrs · 16,959 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT BS 147, AFT OF L/E. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,761 hrs · 16,959 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT BS 175, AFT OF L/E. REPAIRED SKIN PER SWA EA.

Part: LIGHT — BROKEN (CABIN) · airframe 29,467 hrs · 16,769 cycles

DURING SCHEDULED MV3 CHECK, FOUND R1 EMERGENCY EXIT LOWER LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,169 hrs · 16,586 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 10 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: ENGINE — FAILED (NR 1) · airframe 28,667 hrs · 16,290 cycles

INFLIGHT SHUTDOWN, CLIMBING OUT OF SNA AT FL270 NR 1 ENGINE FAILED. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 27,227 hrs · 15,402 cycles

DURING SCHEDULED HC2 CHECK, RT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 27,227 hrs · 15,402 cycles

DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,070 hrs · 15,298 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 24,729 hrs · 13,923 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 24,729 hrs · 13,923 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 23,945 hrs · 13,464 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,202 hrs · 13,021 cycles

DURING SCHEDULED MV3 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 19 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 22,311 hrs · 12,508 cycles

DURING SCHEDULED HC2 CHECK, ROW 16 ABC EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 22,311 hrs · 12,508 cycles

DURING SCHEDULED HC2 CHECK, LEFT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 22,311 hrs · 12,508 cycles

DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 1,985 hrs · 1,155 cycles

EEPLS STRIP LOOSE BETWEEN ROWS 7 & 8. REMOVED AND REPLACED LIGHTING STRIP SECTION PER MM.

Part: PIN — CORRODED (RT MLG) · airframe 19,714 hrs · 11,081 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG WALKING BEAM UPPER STRUT ATTACH PIN PITTED. REMOVED AND REPLACED ATTACH PIN PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,347 hrs · 8,605 cycles

DURING SCHEDULED SPV, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 13,972 hrs · 7,848 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 3 DEF. RELAMPED PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 11,532 hrs · 6,482 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER CRACKED AT FWD END. REMOVED AND REPLACED TRACK COVER PER MM.

Part: SLIDE — OUT OF ADJUST (CABIN) · airframe 8,047 hrs · 4,607 cycles

DURING SCHEDULED BC3 CHECK, FOUND THE R2 EMERGENCY ESCAPE SLIDE OUT OF ADJUSTMENT. ADJUSTED THE R2 ESCAPE SLIDE PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 5,634 hrs · 3,302 cycles

DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: BALLAST — OVERHEATED (CABIN) · airframe 4,540 hrs · 2,693 cycles

AIR TURNBACK, BURNING SMELL REPORTED IN CABIN. AFT GALLEY, RECIRC FAN AND GASPER FAN C/B PULLED, SMELL GOT STRONGER. FOUND SIDEWALL LIGHT BALLAST OVERHEATED AT ROW 17 ABC. REMOVED AND REPLACED SIDEWALL LIGHT BALLAST AT ROW 17 ABC PER MM.

Part: LENS — MISSING (CABIN) · airframe 4,540 hrs · 2,693 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 4,535 hrs · 2,688 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — ILLUMINATED (CABIN) · airframe 3,895 hrs · 2,313 cycles

RT OVERWING EMERGENCY EXIT LIGHT ILLUMINATED JUST PRIOR TO LANDING. CYCLED POWER FROM APU TO GROUND, LIGHT WENT OUT PER MM.

Part: SLIDE — OUT OF POSITION (FWD ENTRY DOOR) · airframe 2,718 hrs · 1,644 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (FWD ENTRY DOOR) · airframe 2,707 hrs · 1,637 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED EVAC SLIDE PER MM.