N396SW

Part: SENSOR — DEFECTIVE (NR 2 ENGINE) · airframe 70,099 hrs · 55,973 cycles

AIR TURNBACK, NR 2 ENGINE SURGING DURING CLIMBOUT. R&R NR 2 ENGINE COMPRESSOR INLET TEMP SENSOR IAW MM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 69,551 hrs · 55,593 cycles

RIGHT FORWARD EMERGENCY FLOOR PHOTOLUMINESCENT STRIP ESCAPE HATCH DAMAGED. R & R PHOTOLUMINESCENT STRIP IAW AMM.

Part: SHEAR WEB — CRACKED (BS 348-351) · airframe 69,551 hrs · 55,593 cycles

SHEAR WEB CRACKED BETWEEN BS 348.2 TO 351.2, BETWEEN STRINGERS 15 - 17L. R&R SHEAR WEB IAW DWG.

Part: FAIRING — CRACKED (RT WING TE FLAP) · airframe 69,551 hrs · 55,593 cycles

RIGHT WING INBOARD FLAP OUTBOARD FLAP TRACK FAIRING AFT END, FAIRING CRACKED AT FORWARD INBOARD SIDE. REPAIRED THE FAIRING IAW SRM.

Part: FLOORBEAM — CRACKED (BS 294) · airframe 69,551 hrs · 55,593 cycles

FLOORBEAM LOWER CORNER HOLE CRACKED AT BS 294.5, WL 208. REPAIRED THE FLOORBEAM IAW ER AND EA.

Part: SUPPORT BRACKET — CRACKED (LT WING-NACELLE) · airframe 69,551 hrs · 55,593 cycles

LEFT NACELL TO WING FAIRING PANEL 57710 SUPPORT BRACKET CRACKED. R & R THE SUPPORT BRACKET IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (BS 277) · airframe 69,551 hrs · 55,593 cycles

INTERCOSTAL CRACKED AT BS 277, STRINGER 14R. REPAIRED INTERCOSTAL IAW ER AND EA.

Part: SUPPORT BRACKET — CRACKED (WING TO NACELLE) · airframe 69,551 hrs · 55,593 cycles

RIGHT NACELLE TO WING FAIRING PANEL 58710 SUPPORT BRACKET CRACKED. R & R THE SUPPORT BRACKET IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 69,551 hrs · 55,593 cycles

R1 DOOR SILL WEB CORRODED. R & R WEB IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,551 hrs · 55,593 cycles

FLOORBEAM TOP CAP CORRODED AT BS 986, BETWEEN RBL 31 TO RBL 43. REPAIRED TOP CAP IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,551 hrs · 55,593 cycles

L1 DOOR LOWER HINGE CUTOUT CRACKED AT BS 304, STR 13L. REPAIRED CUTOUT IAW ER & EA.

Part: RIB — CRACKED (RT WING) · airframe 69,551 hrs · 55,593 cycles

RIGHT WING FUEL TANK RIB CRACKED AT WBL 135.5, 5 AFT OF STRINGER 3. REPAIRED THE RIB IAW EA.

Part: STRAP — CORRODED (BS 1026) · airframe 69,551 hrs · 55,593 cycles

FLOOR STRAP CORRODED AT BS 1026, RBL 3. R & R THE FLOOR STRAP IAW SRM AND DWG.

Part: BEARING — CORRODED (TE FLAP) · airframe 69,551 hrs · 55,593 cycles

LT WING OTBD FLAP NR 2 SPINDLE BEARING CORRODED ON LOWER SURFACE OF CARRIAGE BEARING SUPPORT. R & R NR 2 SPINDLE BEARING IAW AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,551 hrs · 55,593 cycles

FORWARD GALLEY DOOR BOTTOM SIDE OF FLOOR STRUCTURE CORRODED AT BS 294.5. R & R SKIN IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 69,551 hrs · 55,593 cycles

FORWARD GALLEY DOOR INNER CHORD CORRODED BETWEEN BS 294.5 TO BS 330. R & R CHORD IAW SRM.

Part: THRESHOLD — CORRODED (BS 955-991) · airframe 69,551 hrs · 55,593 cycles

R2 DOOR THRESHOLD PLATE CORRODED BETWEEN BS 955 TO 991, WL 208. R & R THRESHOLD IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 69,551 hrs · 55,593 cycles

LEFT WING AFT MOUNT FRAME FOR PANEL 5735 FORWARD INBOARD CORNER SUPPORT ANGLE CRACKED. R & R THE SUPPORT ANGLE IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,551 hrs · 55,593 cycles

FLOOR FRAME STRAP CRACKED AT BS 344, BL 0. R & R STRAP IAW SRM AND DWG.

Part: LENS — LOOSE (CABIN) · airframe 69,298 hrs · 55,431 cycles

LEFT OVERHEAD EMERGENCY EXIT HATCH LIGHT LENS LOOSE. R & R LENS IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,298 hrs · 55,431 cycles

RT WING INBD AFT FLAP DELAMINATED UPPER AND LOWER SURFACES. R & R AFT FLAP IAW MM.

Part: REGULATOR — FAULTY (BLEED AIR SYS) · airframe 68,665 hrs · 55,020 cycles

DIVERSION & DECLARED EMER. AT FC 36 DEGREES CABIN ALTITUDE HORN SOUNDED, ALTIMETER LIGHT DID NOT ILLUMINATE. NO MASKED POPPED, OUTFLOW VLV DID NOT OPEN ON THE GND. R & R NR 2 ENG HIGH STAGE PRESS REGULATOR IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,266 hrs · 54,741 cycles

EMERGENCY BULLNOSE LIGHT INOPERATIVE AT ROW 5 DEF. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,104 hrs · 54,634 cycles

FORWARD ENTRY DOOR AFT EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SKIN — CRACKED (RT WING) · airframe 68,104 hrs · 54,634 cycles

RIGHT WING UPPER SKIN AFT OF REAR SPAR, CRACKED FASTENER HOLE AT RSS 249.5. REPAIRED SKIN IAW ER & EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 68,104 hrs · 54,634 cycles

RT WING INBOARD FLAP OUTBOARD TRACK FAIRING INBOARD AFT SUPPORT ANGLE CRACKED. R&R ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (RT WING) · airframe 68,104 hrs · 54,634 cycles

RIGHT WING UPPER SKIN AFT OF REAR SPAR, CRACKED FASTENER HOLE AT RSS 266. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,104 hrs · 54,634 cycles

LEFT WING UPPER SKIN AT TE, AFT OF REAR SPAR, RSS 255.5 FASTENER HOLE CRACKED. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,104 hrs · 54,634 cycles

RIGHT WING UPPER SKIN AFT OF REAR SPAR, CRACKED FASTENER HOLE AT RSS 240. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,104 hrs · 54,634 cycles

LEFT WING UPPER SKIN AT TE, AFT OF REAR SPAR RSS 239, FASTENER HOLE CRACKED. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,104 hrs · 54,634 cycles

LEFT WING UPPER SKIN AT TE, AFT OF REAR SPAR, RSS 251 FASTENER HOLE CRACKED. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,104 hrs · 54,634 cycles

RIGHT WING UPPER SKIN AFT OF REAR SPAR, CRACKED FASTENER HOLE AT RSS 271. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 68,104 hrs · 54,634 cycles

RIGHT WING UPPER SKIN AFT OF REAR SPAR, CRACKED AT FASTENER HOLE AT RSS 256. REPAIRED SKIN IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 68,104 hrs · 54,634 cycles

RIGHT WING REAR SPAR WEB, CRACKED AT RSS 222, COMMON TO UPPER CHORD, UPPER ROW. REPAIRED WEB IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 68,104 hrs · 54,634 cycles

RIGHT WING UPPER REAR SPAR CHORD, CRACKED AT RSS 222. REPAIRED CHORD IAW ER & EA.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 68,104 hrs · 54,634 cycles

RIGHT MLG AFT SUPPORT FITTING, CORRODED INSIDE OF UPPER INBD HOLE. REPAIRED FITTING ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 68,104 hrs · 54,634 cycles

LEFT WING UPPER REAR SPAR, CHORD CRACKED AT RSS 222. REPAIRED CHORD IAW EA.

Part: LINK — CORRODED (RT MLG) · airframe 68,104 hrs · 54,634 cycles

RIGHT MLG SWING LINK CORRODED. REPAIRED LINK IAW EA.

Part: LINK — CORRODED (LT MLG) · airframe 68,104 hrs · 54,634 cycles

LEFT MLG SWING LINK CORRODED. REPAIRED LINK IAW EA.

Part: PIN — CORRODED (RT MLG) · airframe 68,104 hrs · 54,634 cycles

RIGHT MLG TRUNNION PIN CORRODED. R & R PIN IAW MM.

Part: TRANSMISSION — LOOSE (TE FLAP) · airframe 67,800 hrs · 54,444 cycles

DIVERSION, DECLARED EMER. NR 1 FLAP FAIRING CAME OUT OF TRACKS. R & R NR 2 FLAP TRANSMISSION IAW AMM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 67,548 hrs · 54,270 cycles

AFT LT WINDSCREEN PHOTO LUMINESCENT STRIP WORN. R & R STRIP IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,714 hrs · 53,669 cycles

FUSELAGE SKIN CRACKED AT LOWER FORWARD CORNER OF EXTERNAL POWER DOOR CUT OUT. REPAIRED SKIN IAW EA.

Part: WEB — CRACKED (R1 DOOR) · airframe 65,937 hrs · 53,127 cycles

R1 DOOR LOWER WEB AFT CORNER CRACKED ALONG THE EDGE OF THE STOP FITTING. R & R DOOR IAW AMM & EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 65,937 hrs · 53,127 cycles

LEFT WING INBD AFT FLAP DELAMINATED ON INBD END. R & R AFT FLAP IAW AMM.

Part: SLAT — CRACKED (RT WING) · airframe 65,937 hrs · 53,127 cycles

RIGHT WING NR 6 SLAT TE CRACKED. R & R NR 6 SLAT IAW AMM.

Part: LOGIC CARD — DEFECTIVE (E&E BAY) · airframe 65,382 hrs · 52,747 cycles

AFTER RAISING GEAR HAD LT GEAR RED LIGHT WITH HANDLE IN UP POSITION. PUT HANDLE IN OFF POSITION & HAD RED & GREEN LT GEAR LIGHTS. RAN QRH, PUT HANDLE BACK IN UP POSITION & RED LT GEAR LIGHTS REMAINED ILLUMINATED. R & R LOGIC CARD 987 IAW MM.

Part: FITTING — CORRODED (NLG) · airframe 65,330 hrs · 52,712 cycles

RIGHT NOSE GEAR LOWER LOCK ACTUATOR BRACKET CORRODED. REPAIRED FITTING IAW EA.

Part: FITTING — CORRODED (NLG) · airframe 65,330 hrs · 52,712 cycles

LEFT NOSE GEAR LOWER LOCK ACTUATOR BRACKET CORRODED. REPAIRED FITTING IAW EA.

Part: LENS — MISSING (CABIN) · airframe 65,067 hrs · 52,536 cycles

LEFT EMER LIGHT LENS MISSING AT ROW 18. INSTALLED LENS IAW MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 64,940 hrs · 52,458 cycles

R2 DOOR SLIDE LOOSE. R & R SLIDE ASSEMBLY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 64,202 hrs · 51,961 cycles

EMERGENCY LIGHT LENS LOOSE ABOVE SEAT ROW 2 ABC. SECURED LENS IAW MM.

Part: TEE FITTING — CORRODED (RT MLG WW) · airframe 63,970 hrs · 51,782 cycles

RIGHT MLG WW HORIZONTAL TEE CORRODED AT BS 710. R & R TEE IAW EO & EA.

Part: TEE FITTING — CORRODED (RT MLG WW) · airframe 63,970 hrs · 51,782 cycles

RIGHT MLG WW VERTICAL TEE CORRODED AT BS 710. R & R TEE IAW EO & EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

CHANNEL CRACKED AT BS 348.5 BETWEEN STRINGER 17L TO 16L. R & R CHANNEL IAW SRM.

Part: STIFFENER — CRACKED (FLAP FAIRING) · airframe 63,970 hrs · 51,782 cycles

LEFT WING NR 3 FLAP TRACK FAIRING STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.

Part: FITTING — CRACKED (RT SPOILER) · airframe 63,970 hrs · 51,782 cycles

RIGHT WING GND SPOILER OTBD FITTING CRACKED. R & R FITTING IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

FRAME CRACKED AT BS 787 BETWEEN STRINGER 26R TO 25R. REPAIRED FRAME IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

STRAP CRACKED BETWEEN BS 348.2 TO 351.2 STRINGER 16L. R & R STRAP IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

STRINGER SPLICE CRACKED AT BS 907 STRINGER 3L. R & R SPLICE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

FRAME CRACKED AT BS 360 BETWEEN STRINGER 28L TO 28R. REPAIRED FRAME IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

TIE CLIP CRACKED AT BS 360, STRINGER 9L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

TIE CLIP CRACKED AT BS 360 STRINGER 10L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

TIE CLIP CRACKED AT BS 360 STRINGER 8L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

TIE CLIP CRACKED AT BS 360, STRINGER 5L. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 63,970 hrs · 51,782 cycles

ANGLE CRACKED ON PLATE NR 2 TRANSMISSION. R & R ANGLE IAW SRM & DWG.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

AFT PRESS BULKHEAD Z STIFFENER CORRODED AT BS 1016, BL 0. REPAIRED Z STIFFENER IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

FRAME INNER CHORD CRACKED AT BS 348.2 STRINGER 17L. R & R CHORD IAW EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

STRINGER SPLICE CORRODED AT BS 360 STRINGER 28L. R & R SPLICE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

TIE CLIP CRACKED AT BS 380 STRINGER 28L. R & R TIE CLIP IAW SRM & DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

STRINGER SPLICE CORRODED AT BS 360 STRINGER 27L. R & R SPLICE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

SHEAR TIE CORRODED AT BS 344 STRINGER 26R. R & R SHEAR TIE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

CLIP ANGLE CRACKED AT BS 348.2 STRINGER 15L. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

SUPPORT ANGLE CRACKED AT BS 294.5 STRINGER 23L. R & R SUPPORT IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

TIE CLIP CRACKED AT BS 380 STRINGER 21L. R & R TIE CLIP IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360 STRINGER 7L. R & R CHANNEL IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

ANGLE CRACKED AT BS 312 STRINGER 21L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

ANGLE CRACKED AT BS 312+9 STRINGER 21L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

ANGLE CRACKED AT BS 328+9 STRINGER 21L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 63,970 hrs · 51,782 cycles

ANGLE CRACKED ON PLATE NR 1 TRANSMISSION. R & R ANGLE IAW SRM & DWG.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

AFT PRESS BULKHEAD WEB CORRODED AT BS 1016 RBL 5. REPAIRED WEB IAW EA NO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

ANGLE CRACKED AT BS 328 STRINGER 21L. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE FITTING CRACKED AT BS 303.9, STRINGER 13L. R & R FITTING IAW SRM & DWG.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

KEEL BEAM WEB CRACKED AT BS 710. R & R WEB IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

TIE CLIP CRACKED AT BS 500A STRINGER 22R. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

TIE CLIP CRACKED AT BS 727C STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

CHANNEL CRACKED AT BS 727 BL 0. R & R CHANNEL IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

TIE CLIP CRACKED AT BS 500B STRINGER 23L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

TIE CLIP CRACKED AT BS 947.5, STRINGER 25R. R & R TIE CLIP IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

ANGLE CRACKED AT BS 500C STRINGER 26R. R & R ANGLE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

TIE CLIP CRACKED AT BS 500C STRINGER 27L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

TIE CLIP CRACKED AT BS 400, STRINGER 21L. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

ANGLE CRACKED BETWEEN BS 927 TO 947.5, BL 0. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

STUB FRAME CRACKED AT BS 951 BETWEEN STRINGER 16R TO 17R. REPAIRED STUB FRAME IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 19L. R & R TIE CLIP IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,970 hrs · 51,782 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED ON LOWER SURFACE. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — DELAMINATED (RT AILERON) · airframe 63,970 hrs · 51,782 cycles

RIGHT WING AILERON LOWER SURFACE DELAMINATED. R & R AILERON IAW AMM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

PLATE CRACKED AT BS 794 STRINGER 25R. R & R PLATE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

CLIP ANGLE CRACKED AT BS 540 RBL 0.5. R & R ANGLE IAW SRM & DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 63,970 hrs · 51,782 cycles

RIGHT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

SHEAR TIE CORRODED AT BS 500D BETWEEN STRINGER 28L TO 28R. R & R SHEAR TIE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 380 TO 400 BL 0. R & R ANGLE IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

FORWARD CARGO COMPARTMENT CHANNEL CRACKED AT BS 540 BL 0. R & R CHANNEL IAW DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 500D TO 520 STRINGER 25R. R & R ANGLE IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,970 hrs · 51,782 cycles

RIGHT WING OTBD LOWER SURFACE INBD END OF OTBD AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

UPPER CHORD OF FLOORBEAM CORRODED AT BS 967 LBL 5. REPAIRED BEAM IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

CLIP ANGLE CRACKED AT BS 540 LBL 0.5. R & R ANGLE IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

FORWARD CARGO DOOR CUT OUT FWD FRAME CRACKED AT BS 440 STRINGER 24R. R & R CUT OUT IAW EO & EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

CHANNEL CRACKED AT BS 540 BETWEEN BL 0 & RBL 24. R & R CHANNEL IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

ANGLE CRACKED AT BS 947.5+12, BETWEEN STRINGER 24L TO 25L. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

SKIN CRACKED AT BS 797 STRINGER 24R+2. REPAIRED SKIN IAW EA.

Part: BRACKET — CORRODED (R2 DOOR) · airframe 63,970 hrs · 51,782 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR BRACKET PLATE CORRODED. R & R BRACKET ASSEMBLY IAW MM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 63,970 hrs · 51,782 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT STAB STATION 120.30. R & R RIB IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

STRAP CRACKED AT BS 328 LBL 46. R & R STRAP IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

STRAP CRACKED AT BS 328 LBL 10. R & R STRAP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

WEB CRACKED BETWEEN BS 312 TO 328 RBL 32. R & R WEB IAW SRM & DWG.

Part: BRACKET — CORRODED (L2 DOOR) · airframe 63,970 hrs · 51,782 cycles

L2 DOOR EMER EVAC SLIDE GIRT BAR BRACKET PLATE CORRODED. R & R BRACKET ASSEMBLY IAW MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

WEB CRACKED BETWEEN BS 344 TO 360 BL 0. R & R WEB IAW SRM & DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 63,970 hrs · 51,782 cycles

LEFT LE HORIZONTAL STABILIZER RIB CRACKED AT STATION 151.75. R & R RIB IAW SRM & DWG.

Part: BRACKET — CORRODED (L1 DOOR) · airframe 63,970 hrs · 51,782 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR BRACKET PLATE CORRODED. R & R BRACKET ASSEMBLY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

AFT CARGO DOOR WAY SKIN CUT OUT CRACKED AT BS 797 STRINGER 24R+2. REPAIRED SKIN IAW EO & EA.

Part: BRACKET — CORRODED (R1 DOOR) · airframe 63,970 hrs · 51,782 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR BRACKET PLATE CORRODED. R & R BRACKET ASSEMBLY IAW MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

STRAP CRACKED AT BS 344 RBL 48. R & R STRAP IAW SRM.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 63,970 hrs · 51,782 cycles

LEFT WING TO BODY FAIRING ACCESS PANEL 3578L CRACKED. REPAIRED PANEL IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,970 hrs · 51,782 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.79, LBL 39. REPAIRED WEB IAW EO & EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,970 hrs · 51,782 cycles

WHEEL WELL PRESS DECK WEB CRACKED AT BS 663+1, LBL 24.5+6.5. REPAIRED WEB IAW EO & EA.

Part: SUPPORT ANGLE — CRACKED (NR 2 NACELLE) · airframe 63,970 hrs · 51,782 cycles

NUMBER 2 ENG STRUT ACCESS 5857R SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 669.25, BBL 0.07. REPAIRED CHORD IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A RT AT FWD LOWER HOLE POSITION. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A LT AT FWD LOWER HOLE POSITION. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (GALLEY DOOR) · airframe 63,970 hrs · 51,782 cycles

AFT GALLEY DOOR SKIN LOWER FWD CORNER CRACKED AT BS 958, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727 STRINGER 18A LT FWD LOWER HOLE. REPAIRED CHORD IAW EA NO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

FORWARD GALLEY SERVICE DOOR CUT OUT, AFT LOWER CORNER SKIN CRACKED AT BS 332 STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 666 LBL 24.5. REPAIRED CHORD IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,970 hrs · 51,782 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A RT AT AFT LOWER HOLE POSITION. REPAIRED CHORD IAW EA.

Part: FLAP — LOOSE (RT WING) · airframe 62,461 hrs · 50,714 cycles

RT WING INBD AFT FLAP LOOSE. SECURED AFT FLAP IAW MM.

Part: FLAP — LOOSE (RT WING) · airframe 62,461 hrs · 50,714 cycles

RT WING OTBD AFT FLAP LOOSE. SECURED AFT FLAP IAW MM.

Part: STIFFENER — CRACKED (RT AILERON) · airframe 62,461 hrs · 50,714 cycles

RT WING AILERON STIFFENER CRACKED INBD OF NR 2 HINGE. R & R STIFFENER IAW SRM.

Part: SIGN — UNSECURE (CABIN) · airframe 62,453 hrs · 50,706 cycles

OVERHEAD EMERGENCY EXIT SIGN FELL OFF AT ROW 3. SECURED SIGN IAW MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 61,707 hrs · 50,196 cycles

R1 DOOR SLIDE LOOSE. REPOSITIONED SLIDE IAW MM.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 60,888 hrs · 49,601 cycles

STRONG OIL ODOR THROUGHOUT CABIN & APPEARS TO BE MORE PRONOUNCED WITH RT PACK RUNNING. R&R COALESCE WATER SEPARATOR BAGS LT & RT. R&R RECEIVE FAN FILTER IAW MM.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 60,855 hrs · 49,575 cycles

RT WING NR 7 FLAP TRACK AFT ATTACH POINT TO AFT SPAR CORRODED. R&R NR 7 FLAP TRACK IAW AMM.

Part: SHIM — CORRODED (FLAP TRACK) · airframe 60,855 hrs · 49,575 cycles

RT WING OTBD FLAP NR 7 FLAP TRACK TAPERED SHIM CORRODED ON LOWER SIDE. REPAIRED SHIM IAW SRM.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 60,855 hrs · 49,575 cycles

RT WING OTBD FLAP TRACK NR 7 CORRODED ON TRACK ATTACHMENT AREA TO AFT SPAR. R&R FLAP TRACK IAW MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 60,765 hrs · 49,514 cycles

R1 DOOR SLIDE EVACUTION LOOSE. SECURED SLIDE ASSEMBLY IAW MT.

Part: SLIDE — SEPARATED (L1 DOOR) · airframe 60,364 hrs · 49,197 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY SEPARATED FROM HOUSING, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 60,128 hrs · 49,025 cycles

FORWARD OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER M/M.

Part: SPOILER — DELAMINATED (LT WING) · airframe 59,899 hrs · 48,870 cycles

LEFT WING NR 4 GROUND SPOILER BOARD O\B END DELAMINATED. REMOVED AND REPLACED NR 4 GROUND SPOILER PER AMM.

Part: ANGLE — CRACKED (LT WING) · airframe 58,949 hrs · 48,194 cycles

PREVIOUS REPAIR ANGLE CRACKED AT LEFT WING STA 545 AFT OF AILERON SPRING. REMOVED AND REPLACED ANGLE PER SRM 51-10-02, 51-40-02.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 58,949 hrs · 48,194 cycles

NR 3 SLAT DELAMINATED AT UPPER SURFACE, I/B END. REPAIRED SLAT PER SRM.

Part: SIGN — LOOSE (CABIN) · airframe 58,949 hrs · 48,194 cycles

EMERGENCY EXIT SIGN LOOSE CENTER AISLE AT SEAT ROW 2 DEF. REMOVED AND REPLACED PER AMM.

Part: LENS — LOOSE (CABIN) · airframe 58,723 hrs · 48,039 cycles

FWD PASSENGER COMPARTMENT OVERHEAD EMERGENCY EXIT LENS COVER UNSECURED. RE-SECURED LENS PER STANDARD INDUSTRY PRACTICES.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 58,182 hrs · 47,634 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER EA & ER.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

VERTICAL STIFFENER CRACKED AT BS 727 BULKHED I/B SIDE OF RIGHT KEEL BEAM. REMOVED & REPLACED STIFFENER PER SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 827 TO BS 847. REMOVED AND REPLACED WEB IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

FRAME CORRODED AT BS 787, BETWEEN STR 26R AND STR 27R. REMOVED AND REPLACED FRAME PER SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

FRAME CORRODED AT BS 500C, STR 28R. REPAIRED FRAME PER ER AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

FRAME CORRODED AT BS 767, BETWEEN STR 23L TO STR 23R. REMOVED & REPLACED FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

FRAME CORRODED AT BS 747, BETWEEN STR 23L TO 23R. REMOVED AND REPLACED FRAME PER ER AND EA.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

AFT CARGO BAY SUPPORT CHANNEL CORRODED BETWEEN BS 727D TO 727E, BL 0. REMOVED AND REPLACED CHANNEL PER DWG & SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 58,182 hrs · 47,634 cycles

LEFT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

FRAME CORRODED AT BS 947, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

AFT CARGO BAY FLOOR CHANNEL CORRODED AT BS 727D+6, RBL 3. REPAIRED CHANNEL IAW EA.

Part: SKIN — CHAFED (LE SLAT) · airframe 58,182 hrs · 47,634 cycles

LEFT WING NR 2 SLAT LOWER SURFACE TRAILING EDGE CHAFED AT O/B END. REMOVED AND REPLACED NR 2 SLAT PER M/M.

Part: SKIN — CRACKED (LE SLAT) · airframe 58,182 hrs · 47,634 cycles

LEFT WING NR 3 SLAT LOWER SURFACE SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

AFT CARGO BAY FLOOR CHANNEL CORRODED AT BS 772, LBL 8. REPAIRED CHANNEL IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 712, LBL 24.8. REPAIRED WEB PER ER AND EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

VERTICAL STIFFENER CRACKED AT BS 727B, LBL 45.5. REMOVED AND REPLACED STIFFENER PER SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

VERTICAL COMPRESSION BEAM CRACKED AT BS 727, RBL 45.5. REMOVED AND REPLACED FITTING IAW BOEING DWG AND SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 58,182 hrs · 47,634 cycles

VERTICAL STIFFENER CRACKED AT BS 727B, RBL 45. REMOVED AND REPLACED STIFFENER PER DWG AND SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,206 hrs · 46,869 cycles

L1 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED LIGHT IAW CMM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

STRINGER CLIP DAMAGED AT BS 294.5, STRINGER 4R. REMOVED AND REPLACED STR CLIP PER SRM AND BAC DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

STRINGER CLIP CRACKED AT BS 294.5, STRINGER S4R. REMOVED AND REPLACED STR CLIP PER SRM AND BAC DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

STRINGER CLIP CRACKED AT BS 380A, STR 8L. REMOVED AND REPLACED CLIP PER SRM & BAC DRAWING.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

STRINGER CLIP DAMAGED AT BS 500A, STR 8R. REMOVED AND REPLACED CLIP PER SRM & BAC DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

RT FUSELAGE SKIN CRACKED AT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

RT FUSELAGE SKIN CRACKED AT BS 847+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

RT FUSELAGE SKIN CRACKED AT BS 767+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

RT FUSELAGE SKIN CRACKED AT BS 787+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 867+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 827+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

RT FUSELAGE SKIN CRACKED AT BS 460+10, UPPER AFT WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 827+10, UPPER AFT WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 807+10, UPPER AFT WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 767+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 887+10, LOWER FWD WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 847+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 787+10 LOWER FORWARD WINDOW CORNER CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 807+10 LOWER FORWARD WINDOW CORNER CTOUT. REPAIRED SKIN IAW EA AND REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 767+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 500A+10 LOWER AFT WINDOW CORNER CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 420+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

FUSELAGE SKIN CRACKED AT LT BS 400+10 UPPER FORWARD WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 500B+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

FUSELAGE SKIN CRACKED AT LT BS 500+10 UPPER FORWARD WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 500B+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 460+10, LOWER AFT WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 460+10, UPPER FORWARD WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 360+10 LOWER AFT WINDOW CORNER CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 440+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 500C+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA AND REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

FUSELAGE SKIN CRACKED AT RT BS 480+10 LOWER AFT WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 380+10, UPPER FORWARD WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 520+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA AND REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

RT FUSELAGE SKIN CRACKED AT BS 460+10, UPPER FWD WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 520+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 480+10 UPPER FORWARD WINDOW CORNER CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

RT FUSELAGE SKIN BS 380+10 LOWER AFT WINDOW CORNER CRACKED. REPAIRED SKIN PER BAC SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

FUSELAGE SKIN CRACKED AT LT BS 500A+10 UPPER FORWARD WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

RT FUSELAGE SKIN CRACKED AT BS 420+10, LOWER AFT WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 380+10 LOWER AFT WINDOW CORNER CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

FUSELAGE SKIN CRACKED AT RT BS 500B+10 LOWER AFT WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

FUSELAGE SKIN CRACKED AT LT BS 400+10 LOWER AFT WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 420+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 480+10, LOWER AFT WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

RT FUSELAGE SKIN CRACKED AT BS 440+10, UPPER FWD WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 500+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 500C+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

RT FUSELAGE SKIN BS 400+10 UPPER FORWARD WINDOW CORNER CRACKED. REPAIRED SKIN PER BAC SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

FUSELAGE SKIN CRACKED AT RT BS 500+10 LOWER AFT WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

FUSELAGE SKIN CRACKED AT RT BS 500+10 LOWER AFT WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

LT FUSELAGE SKIN CRACKED AT BS 440+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,206 hrs · 46,869 cycles

FUSELAGE SKIN CRACKED AT RT BS 460+10 LOWER AFT WINDOW CORNER. REPAIRED SKIN PER SRM & SB.

Part: LENS — LOOSE (CABIN) · airframe 57,206 hrs · 46,869 cycles

L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS IAW SOPM.

Part: LENS — LOOSE (CABIN) · airframe 57,206 hrs · 46,869 cycles

AFT CEILING BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS IAW BSOPM.

Part: LENS — LOOSE (CABIN) · airframe 57,200 hrs · 46,864 cycles

AFT GALLEY OVERHEAD EMERGENCY EXIT BULLNOSE SIGN LENS LOOSE. SECURED LENS IAW M/M.

Part: MOUNT — CRACKED (EVAC SLIDE) · airframe 57,200 hrs · 46,864 cycles

R2 DOOR EMERGENCY EVAC SLIDE AFT SLIDE MOUNT CRACKED. REMOVED AND REPLACED MOUNT IAW M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,107 hrs · 46,792 cycles

FUSELAGE SKIN CRACK AT BS 796, STR 4R. REPAIRED SKIN PER EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 57,107 hrs · 46,792 cycles

LONGITUDINAL BEAM CLIP CRACKED AT BS 639, LBL 45.5. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,107 hrs · 46,792 cycles

FUSELAGE SKIN CRACK AT BS 727B+11.5, STR 4R. REPAIRED SKIN PER EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 57,107 hrs · 46,792 cycles

RT STUB BEAM TO LONGITUDINAL BEAM ATTACH CLIP CRACKED AT BS 639, RBL 45.5. REPAIRED CLIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,107 hrs · 46,792 cycles

FUSELAGE SKIN CRACK AT BS 856.5, STR 4L. REPAIRED SKIN PER EA ANR ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,107 hrs · 46,792 cycles

FUSELAGE SKIN CRACK AT BS 820, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,107 hrs · 46,792 cycles

FUSELAGE SKIN CRACK AT BS 794, STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,530 hrs · 46,364 cycles

DURING SCHEDULED RON CHECK, FOUND CRACK IN UPPER FUSELAGE STA 727A TO 727B+2, STR 4R LAP. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,530 hrs · 46,364 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACK AT FS 727A+7.5-8 INCH AT CHEM MILL, STR 4R. REPAIRED EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,043 hrs · 46,015 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 908+12, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,043 hrs · 46,015 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 908+16, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,595 hrs · 45,668 cycles

DURING SCHEDULED RON, CHECK FOUND SKIN CRACKED AT BS 500D+10, STR 10L. REPAIRED SKIN IAW EA.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 55,199 hrs · 45,367 cycles

L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,165 hrs · 45,341 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 887+13, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,165 hrs · 45,341 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 747+9, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,748 hrs · 45,019 cycles

DURING SCHEDULED RON CHECK FOUND, SKIN CRACKED AT BS 747+10, STR 4L. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,772 hrs · 45,039 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 54,479 hrs · 44,813 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REPAIRED LIGHT PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,434 hrs · 44,784 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 380+12, STR 4L. REPAIRED PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,151 hrs · 44,572 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 837, STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,871 hrs · 44,365 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR SKIN CUTOUT AT AFT UPPER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,871 hrs · 44,365 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR SKIN CUTOUT AT AFT UPPER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,867 hrs · 44,364 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,867 hrs · 44,364 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME WEB CRACKED AT BS 303.9, STR 16L. REPAIRED WEB PER ACO AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 727B, RBL 21. REPAIRED BEAM PER EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING I/B AFT FLAP LOWER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8. REPAIRED CHORD PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CORRODED BETWEEN BS 867 TO BS 874, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN PER EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 380, STR 15L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER FITTING CRACKED AT BS 332, STR 8R. REMOVED AND REPLACED FITTING PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 4.9. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 773, LBL 8. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 773, LBL 13. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 1.5. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME WEB CRACKED AT BS 303.9, STR 16L. REPAIRED WEB PER ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM VERTICAL WEB CRACKED AT BS 709, RBL 24.8. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BS 400. REMOVED AND REPLACED WEB PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 8 TO RBL 44. REPAIRED BEAM PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 954, RBL 55. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 4.2. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 4.8. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,155 hrs · 43,840 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 48. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,635 hrs · 43,440 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 753.5, STR 4L. REPAIRED SKIN PER EA.

Part: SLAT — DELAMINATED (WING) · airframe 52,186 hrs · 43,101 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT I/B T/E DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,186 hrs · 43,101 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: COMPRESSOR BLADE — DAMAGED (NR 1 ENGINE) · airframe 51,432 hrs · 42,527 cycles

AIR TURNBACK / DECLARED EMERGENCY / ENGINE SHUTDOWN. LOUD "POPPING" NOISES FROM NR 1 ENGINE DURING ROTATION. ENGINE INDICATIONS NORMAL. PUSHED THRUST LEVERS UP & NOISES CEASED FOR 6-7 SECONDS. THEN RESUMED. INDICATIONS STILL NORMAL. DECLARED EMERGENCY, TURNED DOWN WING, THEN N1 (NR 1 ENG) ROLLED BACK TO 50 PERCENT. SHUT DOWN NR 1. FOUND SEVERAL 9TH STAGE COMPRESSOR BLADES MISSING MATERIAL. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 51,187 hrs · 42,355 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MT.

Part: FLAP — DELAMINATED (LT WING) · airframe 49,090 hrs · 40,821 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B FOREFLAP UPPER SURFACE DELAMINATED. R&R FOREFLAP PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 49,090 hrs · 40,821 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 5 SLAT UPPER O/B WEDGE DELAMINATED. R&R SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,173 hrs · 40,162 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 450, RBL 1. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 377, STR 28R. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND NR 2 SLAT L/E LOWER SKIN CRACKED I/B OF ACTUATOR. REPAIRED SKIN PER SRM.

Part: STRIP — DELAMINATED (CABIN) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT EEPLS STRIP DELAMINATED. REMOVED AND REPLACED STRIP PER MM.

Part: STRIP — DELAMINATED (CABIN) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT EEPLS STRIP DELAMINATED. REMOVED AND REPLACED STRIP PER MM.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 440, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING I/B MID FLAP WEDGE PANEL DELAMINATED. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 867, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 727D, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 747, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 727D, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 787, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 740, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED BS 727A, STR 8. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 747, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 827, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS. 827, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8R. REPAIRED PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME WEB CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,322 hrs · 39,567 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 46,645 hrs · 39,098 cycles

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

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 46,645 hrs · 39,098 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LIGHT ASSY PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 46,600 hrs · 39,062 cycles

EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 17 DEF. R&R STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 46,205 hrs · 38,779 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 44,441 hrs · 37,446 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 43,814 hrs · 36,951 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: STRIP — LOOSE (CABIN) · airframe 43,261 hrs · 36,502 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 13 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,213 hrs · 36,465 cycles

BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 3 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: TAB — CRACKED (LT ELEVATOR) · airframe 42,485 hrs · 35,896 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT ELEVATOR TAB CRACKED AT PUSH ROD FITTING INBOARD LUG. REMOVED AND REPLACED TAB PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,485 hrs · 35,896 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 3 O'CLOCK POSITION. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,485 hrs · 35,896 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 394, RBL 1.625. REPAIRED SKIN PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,485 hrs · 35,896 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 5 O'CLOCK POSITION. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,485 hrs · 35,896 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 8 O'CLOCK POSITION. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,485 hrs · 35,896 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 880, LBL 65, WL 208. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: SKIN — CRACKED (BS 434) · airframe 42,485 hrs · 35,896 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 434, LBL 1.625. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 378) · airframe 42,485 hrs · 35,896 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING DUCT CUTOUT BS 378, LBL 2.375. REPAIRED SKIN PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 42,485 hrs · 35,896 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 41,692 hrs · 35,293 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 40,961 hrs · 34,672 cycles

DURING SCHEDULED A2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 3 DEF. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,756 hrs · 34,525 cycles

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

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 39,641 hrs · 33,647 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED INBOARD SURFACE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LENS — LOOSE (CABIN) · airframe 39,641 hrs · 33,647 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CABIN CEILING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: TRANSMISSION — FAULTY (TE FLAPS) · airframe 39,460 hrs · 33,502 cycles

DIVERSION, FLAPS WOULD NOT EXTEND PAST 10 USING NORMAL EXTENSION, USING ALT EXTENSION FLAPS WENT TO 11 AND 12 THEN STOPPED. NO ROLL OR FLAP ASYMMETRY NOTED. REMOVED AND REPLACED NR 1 FLAP TRANSMISSION PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 37,749 hrs · 32,238 cycles

DURING SCHEDULED C2 CHECK, FOUND CENTER AISLE EMERGENCY EXIT SIGN LENS LOOSE AT ROW 2. SECURED LENS PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 37,304 hrs · 31,868 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: BOLT — WORN (LT ELEVATOR TAB) · airframe 36,757 hrs · 31,451 cycles

DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB CONTROL PUSHROD BOLT AND HARDWARE PER MM.

Part: SKIN — PEELING (RT WING FLAP) · airframe 35,612 hrs · 30,520 cycles

RIGHT WING INBOARD T/E FOREFLAP PREVIOUS REPAIR PEELING. TEMP REPAIRED PER SWA EA, THEN LATER AT PHX, REMOVED AND REPLACED FOREFLAP PER MM.

Part: FAN — OVERHEATED (E&E BAY) · airframe 39,900 hrs · 35,392 cycles

DIVERSION, F/A'S REPORTED SMOKE SMELL FROM FWD AND MID CABIN, NO SMOKE AT ANYTIME. REMOVED AND REPLACED GASPER FAN PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 38,864 hrs · 34,549 cycles

DURING SPV, FOUND 5 EACH CRACKS ON BULKHEAD VERTICAL BEAM WEB AT BS 178, LBL 5.7 TO RBL 17.1. REMOVED AND REPLACED BEAM WEB SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,942 hrs · 29,223 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 440, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,942 hrs · 29,223 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 480, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,942 hrs · 29,223 cycles

DURING SCHEDULED D CHECK, FOUND 2 EACH CRACKS ON FLOOR WEB AT BS 188 TO BS 196, RBL 28-LBL 28. REMOVED AND REPLACED FLOOR WEB SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,942 hrs · 29,223 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT RT BS 188, RBL 30-LBL 30, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: FITTING — CORRODED (TAIL) · airframe 33,942 hrs · 29,223 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL FIN RT AND LT REAR SPAR CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED FIN PER ER.

Part: RIB — CRACKED (RT WING TANK) · airframe 33,942 hrs · 29,223 cycles

DURING SCHEDULED D CHECK, FOUND RT WING TANK UPPER RIB CHORD AT WING STATION 114, STRINGER 1, CRACKED. REPAIRED RIB PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,943 hrs · 29,224 cycles

DURING SCHEDULED D CHECK, FOUND 12 EA FUSELAGE FRAMES CRACKED AT BS 727B, BS 727D, BS 747, BS 787, BS 827, BS 867, BS 907, BS 380, BS 400, BS 440, BS 480 AND BS 500A, BETWEEN STR 8R- STR 9R. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,943 hrs · 29,224 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, WL 200, RT SIDE. REPAIRED FRAME PER T1-153-018.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,943 hrs · 29,224 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 460 TO BS 500+10, RT SIDE. REPAIRED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,943 hrs · 29,224 cycles

DURING SCHEDULED D CHECK, FOUND 7EA FUSELAGE FRAMES CRACKED AT BS 727B, BS 727D, BS 747, BS 867, BS 907, BS 380, AND BS 400, BETWEEN STR 8L- STR 9L. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,942 hrs · 29,223 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 827, STRINGER 8L, CRACKED. REMOVED AND REPLACD FRAME SECTION PER SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,942 hrs · 29,223 cycles

DURING SCHEDULED D CHECK, FOUND FLOOR WEB AT BS 380 TO BS 410, LBL 68, CORRODED. REMOVED AND REPLACED SHEAR WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,942 hrs · 29,223 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 787, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 33,942 hrs · 29,223 cycles

DURING SCHEDULED D CHECK, FOUND ZEE CHORD AT BS 270, LBL 11, CORRODED. REMOVED AND REPLACED CHORD SECTION PER SRM.

Part: FITTING — CORRODED (GIRTBAR) · airframe 33,942 hrs · 29,223 cycles

DURING SCHEDULED D CHECK, FOUND L1 DOOR EVAC SLIDE FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED GIRT BAR FITTINGS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,942 hrs · 29,223 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 344, RBL 1 TO RBL 8, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,942 hrs · 29,223 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM WEB AT BS 1016, LBL 1 TO RBL 37, CORRODED. REMOVED AND REPLACED FLOORBEAM WEB SECTION PER SRM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 66,198 hrs · 72,095 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT GALLEY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,982 hrs · 28,450 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX AFT LEG, CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR UPPER HINGE PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,742 hrs · 28,261 cycles

DURING SPV, FOUND BULKHEAD WEB AT BS 178, LBL 14, CRACKED. REPAIRED WEB PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 32,038 hrs · 27,711 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FORE FLAP PER MM.

Part: BEARING — WORN (BOTH ELEVATORS) · airframe 30,249 hrs · 26,231 cycles

DURING SCHEDULED C2 CHECK, BOTH LT AND RT ELEVATORS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR INPUT ARM BEARINGS PER MM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 30,249 hrs · 26,231 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BULKHEAD — CRACKED (AC BAY) · airframe 29,332 hrs · 25,517 cycles

DURING SCHEDULED C1 CHECK, FOUND SECONDARY HEAT EXCHANGER OUTBOARD SUPPORT BULKHEAD WEB CRACKED, BS 585 & LBL 40.875. REPAIRED BULKHEAD WEB PER SWA EA.

Part: LINE — LEAKING (HYD SYS) · airframe 29,221 hrs · 25,418 cycles

DIVERSION, A-SYSTEM HYDRAULICS QUANTITY DROPPED TO BETWEEN .25 & .5. FOUND GROUND SPOILER HYD LINE LOOSE. TIGHTENED HYD LINE, LEAK & OPS CHECK GOOD. PER MM

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 27,162 hrs · 23,738 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: ACTUATOR — FAILED (L/E FLAP) · airframe 25,631 hrs · 22,540 cycles

DIVERSION, AT FL 350 L/E FLAP TRANSIT LIGHT ILLUMINATED, NR 2 L/E FLAP LIGHT ON OVERHEAD ILLUMINATED. REMOVED AND REPLACED NR 2 L/E FLAP ACTUATOR PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 25,504 hrs · 22,443 cycles

AIR TURNBACK, F/O'S FRONT WINDOW SHATTERED AT FC 310. REMOVED AND REPLACED F/O'S FRONT WINDOW AND CONTROLLER PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 25,496 hrs · 22,434 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT OTBD AFT FLAP DELAMINATED AT T/E. REMOVED AND REPLACED RT OTBD AFT FLAP PER MM..

Part: WEB — CRACKED (FUSELAGE) · airframe 25,496 hrs · 22,434 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 185 AND LBL 1.0. REPAIRED WEB PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 24,616 hrs · 21,717 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY. RE INSTALLED SLIDE PER MM.

Part: COLLAR — WORN (NLG) · airframe 24,597 hrs · 21,701 cycles

NOSE WHEEL STEERING FAILED DURING START OF T/O ROLL, TILLER JAMMED TO THE LEFT, WAS PHYSICALLY UNABLE TO MOVE IT TO NEUTRAL OR TO THE RIGHT. REMOVED AND REPLACED STEERING COLLAR ASSY AND BEARINGS PER MM ANDSWA RA, ALSO REMOVED AND REPLACED UPPER AND LOWER LINKS PER MM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 23,674 hrs · 20,954 cycles

DURING SCHEDULED C3 CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 22,848 hrs · 20,248 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT MID CABIN. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 22,771 hrs · 20,183 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: COVER — LOOSE (CABIN) · airframe 22,311 hrs · 19,791 cycles

EEPLS TRACK COVERS LOOSE AT EMERGENCY EXIT ROW. SECURED TRACK COVERS PER MM.

Part: COVER — MISSING (CABIN) · airframe 22,026 hrs · 19,565 cycles

EEPLS TRACK COVER MISSING. INSTALLED TRACK COVER PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 21,858 hrs · 19,430 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC AND ENTRY DOOR EMERGENCY EVAC SLIDE ASSYS OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSYS PER MM.

Part: LENS — CRACKED (ENTRY DOOR) · airframe 21,858 hrs · 19,430 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 20,803 hrs · 18,589 cycles

DURING SCHEDULED C4 CHECK, FOUND SEVERAL EEPLS TRACKS BROKEN. REMOVED AND REPLACED TRACK COVERS PER MM.

Part: FRAME — CRACKED (BULKHEAD) · airframe 20,503 hrs · 18,340 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 RIGHT & LEFT SIDE CHORDS CRACKED. REMOVED AND REPLACED CHORDS PER ACO 7342-53 & 7338-53.

Part: COVER — MISSING (PAX DOOR) · airframe 19,738 hrs · 17,719 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM.

Part: COVER — MISSING (CABIN)

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVER MISSING BY OVERWING EXIT. REPLACED COVER PER MM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED ON LOWER END. REPAIRED FRAME PER BOEING REPAIR DRAWING.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM AT FASTENER HOLE, BS 986, RBL 38. REPAIRED BEAM PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH CRACKS, BS 178 BULKHEAD, RBL 5 AND LBL 5. REPAIRED BULKHEAD PER SRM.

Part: WIRE — BROKEN (ROW 1)

FLOOR TRACK LIGHTING COVER MISSING AT ROW 1. ALSO, WIRES EXPOSED AND BROKEN. REPAIRED WIRES AND REPLACED COVER PER MM.

Part: ANGLE — CRACKED (FUSELAGE)

DURING SCHEDULED C4 CHECK, FOUND FLOOR LT PACK INLET SUPPORT ANGLE CRACKED. REPAIRED SUPPORT ANGLE PER SWA RA NR 1-A53-1876.

Part: SKIN — SCRAPED (FUSELAGE)

EXPERIENCED TAIL DRAG DURING TAKEOFF CAUSING SKIN DAMAGE TO BOTTOM SIDE AT BS 967, 1006, 986.5 AND 1016, PRESSURE DOME. REPAIRED PER BOEING SRM AND SWA RA 1-353-1512.