N510SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,425 hrs · 66,367 cycles

SKIN CRACKED AT BS 482B TO BS 520, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: BRACKET — LOOSE (CABIN) · airframe 70,292 hrs · 66,230 cycles

L2 DOOR EVAC SLIDE AFT GIRT BAR BRACKET LOOSE. ADJUSTED L2 DOOR GIRT BAR BRACKET IAW SIP.

Part: SIGN — UNSECURE (CABIN) · airframe 69,803 hrs · 65,725 cycles

LT OVERWING EMERGENCY EXIT SIGN FELL OFF. REINSTALLED SIGN IAW AMM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

INNER CREASE BEAM CHORD CRACKED AT STATION 947.5 + 11", LBL 53. R&R CHORD IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

RT CREASE BEAM INNER CHORD VERTICAL LEG SPLICE CRACKED AT STATION 540-8. R&R STRAP IAW DRAWING & SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

LT CREASE BEAM INNER CHORD VERTICAL LEG SPLICE CRACKED AT STATION 540- 8. R&R STRAP IAW SRM & DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

CHANNEL CRACKED AT STATION 540, BETWEEN BL 0 TO LBL 25. R&R CHANNEL IAW SRM & DRAWING.

Part: CREASE BEAM — CORRODED (R2 DOOR) · airframe 69,782 hrs · 65,701 cycles

R2 DOOR INNER CREASE BEAM CORRODED BETWEEN STATION 951 TO STATION 990. R&R BEAM IAW SRM & DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

FLOOR BEAM CRACKED AT STATION 947, LBL 58. R&R FLANGE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

FRAME WEB CRACKED AT STATION 178 RBL 17.0. REPAIRED WEB IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

FS SKIN CORRODED AT STATION 540, STRINGER 26L. REPAIRED SKIN IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

LOWER LOBE CHORD CORRODED BETWEEN STATION 270 TO 277, LBL 16. R&R CHORD IAW DRAWING & SRM.

Part: COVER — CRACKED (EVAC SLIDE) · airframe 69,782 hrs · 65,701 cycles

L2 DOOR EMERGENCY EVAC SLIDE COVER CRACKED AT AFT LOWER CORNER BY GIRT BAR STOW HOOK. R&R SLIDE IAW MT.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

FWD EE COMPARTMENT LOWER BILGE NLG FWD BULKHEAD LOWER CHORD CORRODED AT STATION 227, BETWEEN LBL 7 TO RBL 9. R&R CHORD IAW SRM.

Part: SKIN — DELAMINATED (FAIRING) · airframe 69,782 hrs · 65,701 cycles

LT WING TO BODY FAIRING NR 3378 EXTERIOR SURFACE DELAMINATED NEAR THE LOWER EDGE AS MARKED. REPAIRED SURFACE IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,782 hrs · 65,701 cycles

MAIN WW PRESSURE DECK CRACKED AT STATION 665, LBL 39.5. R&R DECK IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

SKIN CRACKED BETWEEN STATION 781 TO STATION 781.75, STRINGER 24L. REPAIRED SKIN IAW SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

SHEAR TIE CORRODED AT STATION 767, BETWEEN STRINGER 27L & STRINGER 27R. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

STRINGER CLIP CRACKED AT STATION 947 STRINGER 26L. R&R CLIP IAW SRM & DRAWING.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

SHEAR TIE CRACKED AT STATION 787 STRINGER 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

SHEAR TIE CORRODED AT STATION 727C, STRINGER 27R. R&R SHEAR TIE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

FLOOR SUPPORT UPPER ANGLE CRACKED BETWEEN STATION 927 TO STATION 947, BL 0. R&R ANGLE IAW SRM & DRAWING.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

KEEL BEAM VERTICAL SUPPORT BRACKET CRACKED AT STATION 727 STRINGER 27R. R&R BRACKET IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

FRAME CRACKED AT STATION 947, STRINGER 19L. R&R FRAME IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

STRINGER CLIP CRACKED AT STATION 947 STRINGER 25R. R&R CLIP IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

FS SKIN CRACKED BETWEEN STATION 950 TO STATION 951, STRINGER 24R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,782 hrs · 65,701 cycles

SKIN CRACKED BETWEEN STATION 783 TO STATION 785, STRINGER 22L. REPAIRED SKIN IAW EA.

Part: FASTENER — CRACKED (LT WING) · airframe 69,782 hrs · 65,701 cycles

LT WING UPPER SURFACE NR 1 ENGINE PYLON PANEL INBD ATTACH SKATE ANGLE FORWARD FASTENER HEAD CRACKED. R&R FASTENER IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,622 hrs · 65,528 cycles

FS SKIN CRACKED AT STATION 312, STRINGER 20R. REPAIRED SKIN IAW SRM.

Part: CABLE — LOOSE (EVAC SLIDE) · airframe 69,168 hrs · 65,034 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED CABLE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 68,987 hrs · 64,853 cycles

FWD ENTRY EMERGENCY LIGHT LENS LOOSE BETWEEN L1 DOOR AND FLIGHT ATT SEAT FLOOR LEVEL. REMOVED AND REPLACED LIGHT ASSY IAW M/M.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 68,143 hrs · 63,977 cycles

RIGHT AFT SERVICE DOOR EXTERIOR EMERGENCY EGRESS LIGHT INOP. REMOVED & REPLACED LIGHT BULB AND REFLECTOR ASSY PER AMM.

Part: COVER — LOOSE (CABIN) · airframe 68,005 hrs · 63,837 cycles

FWD EMERGENCY EXIT LIGHT COVER IS LOOSE. REMOVED AND REPLACED FWD EMERGENCY EXIT LIGHT COVER BY FWD ENTRY DOOR PER MM. OPS CHECKS GOOD.

Part: FLAP — CRACKED (LT WING) · airframe 67,891 hrs · 63,729 cycles

INBOARD AFT FLAP OUTBOARD LOWER CORNER CRACKED AND DELAMINATED. RESEALED END CAP ON INBOARDD AFT FLAP OUTBOARD AFT CORNER PER AMM 51-31-00.

Part: LIGHT — LOOSE (CABIN) · airframe 67,481 hrs · 63,320 cycles

OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LOOSE BETWEEN ROW 8 TO ROW 9. SECURED LIGHT PER MM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 67,390 hrs · 63,264 cycles

RIGHT WING NR 6 SPOILER DELAMINATED. REMOVED AND REPLACED NR 6 SPOILER AS PER AMM.

Part: SPINDLE — CORRODED (WING) · airframe 67,053 hrs · 63,053 cycles

NR 7 SPINDLE CORRODED. REMOVED AND REPLACED PER MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 67,022 hrs · 63,033 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: SIGN — MISSING (CABIN) · airframe 66,267 hrs · 62,526 cycles

LEFT EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER M/M.

Part: SKIN — CANNING (FUSELAGE) · airframe 66,132 hrs · 62,436 cycles

LOWER FUSELAGE SKIN OIL CANNING CONDITION BETWEEN BS 767 TO BS 807 +6, BETWEEN STR 19L TO STR 20L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,132 hrs · 62,436 cycles

SKIN CRACKED BETWEEN BS 747+16.5 TO BS 747+17.6, STR 20L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,132 hrs · 62,436 cycles

SKIN CRACKED AT BS 767, STR 23L. REPAIRED SKIN IAW AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,132 hrs · 62,436 cycles

SKIN CRACKED AT BS 767, STR 24L. REPAIRED SKIN IAW AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,132 hrs · 62,436 cycles

SKIN CRACKED AT BS 827, STR 19L. REPAIRED SKIN IAW AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,132 hrs · 62,436 cycles

SKIN CRACKED AT BS 847, STR 17L. REPAIRED SKIN IAW AAR EA.

Part: HINGE FITTING — CRACKED (RT SPOILER) · airframe 66,100 hrs · 62,416 cycles

RT WING 5 SPOILER O/B ACTUATOR HINGE FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DWG.

Part: WIRE — BROKEN (CABIN) · airframe 66,100 hrs · 62,416 cycles

LT EMERGENCY LIGHT WIRE BROKEN. REPAIRED WIRE IAW WDM AND AMM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

FWD CARGO COMPARTMENT BULKHEAD PANEL ATTACH ANGLE CRACKED AT BS 380, STR 20L. REMOVED AND REPLACED ANGLE PER BAC DWG.

Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT ANGLE BROKEN AT BS 807, STR 25R. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

STRINGER CRACKED AT BS 277, BETWEEN STR 12R TO STR 13R. REPAIRED STRINGER PER EA & REO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

SHEAR TIE CRACKED AT BS 360, STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

FRAME SUPPORT ANGLE CRACKED AT BS 325, STR 20L. REMOVED AND REPLACED ANGLE PER SRM.

Part: FITTING — MISSING (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

STRINGER END FITTING MISSING AT BS 360+3, STR 28L. REMOVED AND REPLACED FITTING IAW SRM & BAC DWG.

Part: MOUNT — WORN (R2 DOOR) · airframe 66,100 hrs · 62,416 cycles

R2 DOOR EMERGENCY EVAC SLIDE AFT MOUNT ASSY WORN. REMOVED AND REPLACED MOUNT ASSY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

R1 DOOR FUSELAGE SKIN CUTOUT CRACKED AT BS 303, STR 8R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

L2 DOOR FUSELAGE SKIN CUTOUT CORNER, LOWER FWD CORNER, BEAR STRAP CRACKED AT BS 962, STR 17L. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 671.5, RBL 24.5. REPAIRED CHORD IAW EA.

Part: BULKHEAD — CRACKED (BS 178) · airframe 66,100 hrs · 62,416 cycles

RT PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, WL 234. REMOVED AND REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED BEAM IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED CLIP IAW DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

STRINGER SPLICE ANGLE CRACKED AT BS 291, STR 9L. REMOVED ANGLE IAW SRM & BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

MAIN CABIN FRAME SUPPORT ANGLE CRACKED BS 277, BETWEEN STR 15L TO STR 16L. REPAIRED ANGLE PER BAC DWG AND SRM.

Part: STRINGER CLIP — CRACKED (BS 767L S16L) · airframe 66,100 hrs · 62,416 cycles

STRINGER CLIP CRACKED AT BS 767L, STR 16L. REMOVED & REPLACED STRINGER CLIP IAW SRM.

Part: FLOOR PANEL — CRACKED (BS 247) · airframe 66,100 hrs · 62,416 cycles

COCKPIT FLOOR SKIN CRACKED AT BS 247, RBL 24 AT FASTENER HOLE COMMON TO OPC CRADLE BRACKET. REPAIRED PER ACO.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

MAIN CABIN FRAME SUPPORT ANGLE CRACKED AT BS 277, BETWEEN STR 12R TO STR 13R. REPAIRED ANGLE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

R1 DOOR CUTOUT SUPPORT FRAME CRACKED BS 295, BETWEEN STR 7R TO STR 8R. REMOVED AND REPLACED FRAME IAW BAC DWG AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED CLIP IAW BAC DWG AND SRM.

Part: CREASE BEAM — CRACKED (BS 290-294.5) · airframe 66,100 hrs · 62,416 cycles

FWD GALLEY DOOR AREA, CREASE BEAM, INBOARD ANGLE CRACKED BETWEEN BS 290 TO BS 294.5, STR 17R. REMOVED & REPLACED ANGLE IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S15R) · airframe 66,100 hrs · 62,416 cycles

STRINGER CLIP CRACKED BS 277, STR 15R. REMOVED & REPLACED STRINGER CLIP IAW SRM.

Part: SKIN — CRACKED (RT AILERON) · airframe 66,100 hrs · 62,416 cycles

RT WING TRAILING EDGE AILERON NR 3 O/B HINGE UPPER COMPOSITE SKIN CRACKED. REMOVED AND REPLACED AILERON IAW AMM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

SUPPORT ANGLE CRACKED AT BS 277, BETWEEN STR 15R TO STR 16R. REPAIRED ANGLE PER BAC DWG AND SRM.

Part: WEB — CRACKED (COCKPIT) · airframe 66,100 hrs · 62,416 cycles

COCKPIT FLOOR CRACKED AT BS 247, RBL 16. REPAIRED FLOOR WEB PER ACO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

FLOORBEAM CAP CORRODED BS 986, BETWEEN TO BL 0 TO RBL 18. REMOVED AND REPLACED BEAM IAW REO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

FRAME CRACKED BS 344, BETWEEN STR 4L TO STR 5L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,100 hrs · 62,416 cycles

CRACKED STRINGER CLIP AT STRINGER 20R AND BS 799. REMOVED CLIP PER DWG AND SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 66,092 hrs · 62,410 cycles

LT OVERWING EXIT EXTERIOR EMERGENCY LIGHT INOP. REPAIRED BULB PER M/M.

Part: TRU — FAULTY (COCKPIT) · airframe 65,696 hrs · 62,154 cycles

AIR TURNBACK, DURING CLIMBOUT PRESSURIZATION AUTOFAIL LIGHT ILLUMINATED. FOUND TR1 CB POPPED, WOULD NOT RESET. FLIGHT ATTENDANTS CALLED ABOUT ELECTRICAL SMOKE SMELL IN CABIN. REMOVED AND REPLACED NR 1 TRANSFORMER RECTIFIER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,537 hrs · 62,052 cycles

DURING SCHEDULED CV CHECK FOUND, SKIN CRACKED AT BS 390+1, STR 1. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,537 hrs · 62,052 cycles

DURING SCHEDULED CV CHECK FOUND, SKIN CRACKED AT BS 370+5, STR 1. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,099 hrs · 62,416 cycles

SKIN CRACKED AT BS 370+ 5, STR 1. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,099 hrs · 62,416 cycles

FUSELAGE SKIN CRACKED AT BS 390+ 1, STR 1. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,337 hrs · 61,918 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 405, STR 16R. REPAIRED SKIN.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,337 hrs · 61,918 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 482A, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 65,337 hrs · 61,918 cycles

DURING SCHEDULED SPV CHECK, FOUND STUB BEAM UPPER CHORD CRACKED AT BS 616, WL 208. REMOVED AND REPLACED BEAM IAW ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,337 hrs · 61,918 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM T-CHORD CORRODED BETWEEN BS 360 TO BS 396, STR 17R. REMOVED AND REPLACED BEAM IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 65,337 hrs · 61,918 cycles

DURING SCHEDULED SPV CHECK, FOUND STUB BEAM UPPER CHORD CRACKED AT BS 616, WL 207. REMOVED AND REPLACED BEAM IAW ER.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 65,337 hrs · 61,918 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM SHEAR WEB CORRODED BETWEEN BS 380 TO BS 400, STR 17R. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,337 hrs · 61,918 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME IAW SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 65,337 hrs · 61,918 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 65,337 hrs · 61,918 cycles

DURING SCHEDULED SPV CHECK, FOUND RT INNER CREASE BEAM CHORD CRACKED AT BS 638, WL 208. REPAIRED BEAM IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,337 hrs · 61,918 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 932, STR 21L. REPAIRED SKIN IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 65,337 hrs · 61,918 cycles

DURING SCHEDULED SPV CHECK, FOUND RT CREASE BEAM WEB CRACKED BETWEEN BS 616 TO BS 639. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,337 hrs · 61,918 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 616, WL 209. REPAIRED FRAME IAW EA.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 65,337 hrs · 61,918 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR WEB CRACKED BETWEEN BS 616 TO BS 639, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,337 hrs · 61,918 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FRAME INNER CHORD CRACKED AT BS 616, WL 202. REPAIRED CHORD IAW EA.

Part: CHARGER — FAILED (CABIN) · airframe 65,329 hrs · 61,910 cycles

PASSENGER COMPLAINED OF ODOR IN CABIN IN CLIMB AND CRUISE. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 65,137 hrs · 61,764 cycles

LT WING NR 2 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 64,723 hrs · 61,490 cycles

DECLARED EMERGENCY - ON DESCENT FROM FL 350, WITH THROTTLES AT IDLE AND N1 APPROX 60 PERCENT, NOTICED A LOUD POP AND VIBRATION COMING FROM NR 2 ENGINE, ON LEVEL OFF BOTH THROTTLES SLOWLY ADVANCED AND OPERATED NORMAL, AGAIN ON DESCENT RETARDED APPROX 60 PERCENT NR 2 LOUD POP SLIGHT EGT SPIKE. STABILIZED AT IDLE, SEVERAL CONTINUOUS COMP STALLS "POPS" WHEN THROTTLE WAS ADVANCED ABOVE 60 PERCENT NO LIMITS WERE EXCEEDED. REMOVED AND REPLACED NR 2 ENGINE MEC AND FUEL PUMP ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 64,583 hrs · 61,396 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 64,136 hrs · 61,094 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING NR 6 SLAT L/E SKIN CRACKED. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,962 hrs · 60,980 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482B+13, STRINGER 16L. REPAIRED SKIN PER EA.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 63,835 hrs · 60,896 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,500 hrs · 59,266 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 772, STR 25L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 61,346 hrs · 59,159 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 60,992 hrs · 58,919 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 2 SLAT SKIN CRACKED AT STA 214.4. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CORRODED AT BS 294.5, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED T-CHORD PER SRM.

Part: HINGE FITTING — CORRODED (HORIZ STAB) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABILIZER CENTER SECTION HINGE FITTING LUGS CORRODED. REPAIRED FITTING PER AEM EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 716, BBL 0. REPAIRED WEB PER SI.

Part: SKIN — CRACKED (LE SLAT) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED AT WBS 297.40. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED AT WBS 340. REPAIRED SKIN PER SRM.

Part: HINGE FITTING — CORRODED (HORIZ STAB) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STABILIZER CENTER SECTION HINGE FITTING LUGS CORRODED. REPAIRED FITTING PER AEM EO.

Part: RIB — CRACKED (RT WING) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING RIB CRACKED AT WBL 135.5, BETWEEN STR 1 TO STR 2. REPAIRED RIB PER AEM EO.

Part: FLAP — CORRODED (LT WING) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING FORE FLAP O/B CORRODED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 522.5, RBL 5. REPAIRED SKIN PER AEM EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 27L TO STR 26R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CRACKED AT BS 727B, RBL 24.5. REPAIRED BEAM PER AEM EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD PER AEM EO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND PRESSURE BULKHEAD CRACKED AT BS 178, LBL 17.0. REPAIRED BULKHEAD PER AEM EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: SILL — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR LOWER SILL WEB CRACKED AT BS 416. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO COMPT FRAME CRACKED AT BS 482, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO COMPT FRAME CRACKED AT BS 482A, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 60,419 hrs · 58,530 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED SPLICE PER SRM.

Part: MEC — FAULTY (NR 1 ENGINE) · airframe 59,945 hrs · 58,237 cycles

INFLIGHT SHUTDOWN. DURING ILS APPROACH TO MCI, NR 1 ENGINE BEGAN TO ACCELERATE WITH NO THROTTLE MOVEMENT. A/C AT 3000 FEET, ENGINE ACCELERATED TO 95 PERCENT BEFORE SHUT DOWN. ALL PARAMETERS NORMAL, ENGINE APPEARED TO STABILIZE AT 95 PERCENT. REMOVED AND REPLACED CIT, T2 SENSOR, NR 1 ENG MEC, AND NR 1 ENG T-12 TEMPERATURE SENSORS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,741 hrs · 58,119 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,741 hrs · 58,119 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,741 hrs · 58,119 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,741 hrs · 58,119 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,741 hrs · 58,119 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787+12, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,091 hrs · 57,709 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,091 hrs · 57,709 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,091 hrs · 57,709 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,091 hrs · 57,709 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,091 hrs · 57,709 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,091 hrs · 57,709 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,062 hrs · 57,686 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 977, STR 21L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 59,022 hrs · 57,660 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,332 hrs · 57,218 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIGN LIGHT BULBS INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 58,225 hrs · 57,146 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,072 hrs · 57,038 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 930, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,072 hrs · 57,038 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 871, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (SPOILER) · airframe 57,152 hrs · 56,309 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING INBD GROUND SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (BS 760 S22L) · airframe 57,000 hrs · 56,167 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 22L. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 56,652 hrs · 55,867 cycles

DURING SCHEDULED HC1 CHECK, FOUND KEEL BEAM CRACKED AT BS 699, STR 27R. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,270 hrs · 54,803 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 798, STR 18L. REPAIRED SKIN PER SWA EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, RBL 39. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FITTING — CORRODED (T/E FLAP) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 8 FLAP TRACK OUTBOARD FITTING CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 799, RBL 17. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 1138, STR 13L. REPAIRED STRINGER CLIP PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 460, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 31. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DEBONDED (RT ELEVATOR) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT ELEVATOR UPPER SURFACE DISBONDED. REMOVED AND REPLACED ELEVATOR PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 54,879 hrs · 54,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 54,820 hrs · 54,420 cycles

RETRACTED LANDING GEAR, RT MLG UNSAFE LIGHT ILLUMINATED. CYCLED GEAR, SAME INDICATION, LIGHT WENT OUT ABOVE 10000 FT. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 54,764 hrs · 54,377 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,305 hrs · 53,997 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 780 AND BS 790, STR 18L AND STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (NR 9 SPOILER) · airframe 54,158 hrs · 53,860 cycles

RIGHT WING NR 9 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — DELAMINATED (NR 8 SPOILER) · airframe 54,158 hrs · 53,860 cycles

RIGHT WING NR 8 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,813 hrs · 53,537 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL WEB CRACKED FWD BULKHEAD BS 178, LBL 17, WL 227. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,396 hrs · 53,143 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 762 AND BS 770, STR 19L AND STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,646 hrs · 52,399 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 803, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,646 hrs · 52,399 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 971, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,646 hrs · 52,399 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 789, STR 18L. REPAIRED SKIN PER SWA EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,636 hrs · 52,389 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (BS 751 S23L) · airframe 52,528 hrs · 52,282 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 751, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 763 S21L) · airframe 52,528 hrs · 52,282 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 763, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 758 S18L) · airframe 51,964 hrs · 51,706 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 758, STR 18L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 51,897 hrs · 51,630 cycles

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

Part: SKIN — CRACKED (BS 770 S19L) · airframe 50,478 hrs · 50,172 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 50,131 hrs · 49,788 cycles

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

Part: TERMINAL — BROKEN (EMERGENCY LIGHT) · airframe 49,486 hrs · 49,111 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHTS AND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHTS INOP. REPAIRED TERMINAL END AT R1 DOOR EMERGENCY EXTERIOR LIGHT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,177 hrs · 48,784 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME #5 STOP FITTING. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,177 hrs · 48,783 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CRACKED AT BS 356, STR 4L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,177 hrs · 48,783 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CRACKED BETWEEN BS 400 TO BS 440, STR 4L. REPAIRED STRINGER PER SRM.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 49,177 hrs · 48,783 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME BUTT STRAP CRACKED AT BS 907, BETWEEN STR 4L TO STR 4R. R & R BUTT STRAP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,177 hrs · 48,783 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 361, STR 4L. R&R STRINGER SPLICE PER SRM.

Part: SPLICE — CRACKED (BS 907) · airframe 49,177 hrs · 48,783 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 48,997 hrs · 48,587 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 45,887 hrs · 45,329 cycles

FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MM.

Part: LINK — BROKEN (RT MLG) · airframe 48,272 hrs · 47,843 cycles

EXTREME VIBRATION FELT AFTER LANDING. FOUND RT MLG UPPER TORSION LINK BROKEN. RT MLG SHIMMY DAMPNER SHAFT BENT. RT MLG LOWER STRUT WARPED. NR 3 AND NR 4 MLG TIRES DAMAGED. NR 1, NR 3, NR 4 AND NR 6 L/E SLATS DAMAGED. REMOVED AND REPLACED RT MLG ASSY, RT MLG UPPER AND LOWER TORSION LINKS, RT MLG SHIMMY DAMPNER, RT MLG LOWER STRUT, NR 3 AND NR 4 MLG TIRE/WHEEL ASSY AND NR 1, NR 3, NR 4 AND NR 6 L/E SLATS PER MM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 48,230 hrs · 47,798 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 4 L/E SLAT LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SRM.

Part: SHEAR TIE — CRACKED (BS 360) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT BS 360, BETWEEN STR 15R AND STR 16R. REPAIRED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (L1 DOOR SLIDE) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR AFT FLOOR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FLOORBEAM — CORRODED (BS 360) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 360, BETWEEN RBL 51 TO RBL 61. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CAP CORRODED AT BS 986. REMOVED AND REPLACED FLOORBEAM UPPER CAP PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED & DISBONDED. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CORRODED (BS 616-639) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 616 TO BS 639. REPAIRED CREASE BEAM PER SRM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING NR 2 L/E SLAT OUTBOARD UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM T-CHORD CORRODED AT BS 312, BETWEEN LBL 54 TO RBL 54. REMOVED AND REPLACED T-CHORD PER SRM.

Part: FRAME — CHAFED (L1 DOOR) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR UPPER AFT FRAME CHAFED AT TOP EDGE. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 328, RBL 21, RBL 28 & RBL 36. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (BS 663) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 663, STR 14R. REPAIRED STRINGER PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, STR 2. REPAIRED RIB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 23R, 5 O'CLOCK POSITION. REPAIRED WEB PER SWA EA.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 7R, 2 O'CLOCK POSITION. REPAIRED WEB PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 927) · airframe 48,148 hrs · 47,702 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (BS 900) · airframe 47,976 hrs · 47,529 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 900, BETWEEN STR 24R TO STR 25R. REPAIRED SKIN PER SWA EA.

Part: SIGN — SEPARATED (CABIN) · airframe 47,909 hrs · 47,459 cycles

DURING SCHEDULED A1 CHECK, L1 DOOR EMERGENCY EXIT SIGN FELL OFF. REINSTALLED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,571 hrs · 47,128 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 522, STR 10R. REPAIRED SKIN PER SWA EA .

Part: FLAP — DELAMINATED (LT WING) · airframe 47,087 hrs · 46,639 cycles

DURING SCHEDULED A2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,910 hrs · 46,426 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,507 hrs · 46,003 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 378, LBL 2. REPAIRED SKIN PER SWA EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 46,356 hrs · 45,847 cycles

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

Part: FITTING — WORN (LT ELEVATOR) · airframe 45,625 hrs · 46,065 cycles

DURING SCHEDULED C3 CHECK, LT ELEVATOR INBOARD TAB HINGE FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD HINGE FITTING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,625 hrs · 45,065 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 932, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 45,575 hrs · 45,011 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,880 hrs · 44,326 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE EMERGENCY EXIT OVERHEAD LIGHT AND AFT ENTRY SIDEWALL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 44,793 hrs · 44,219 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 AND L2 DOOR EVAC SLIDE CABLES MISROUTED. ROUTED R2 AND L2 DOOR EVAC SLIDE CABLES PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 44,527 hrs · 43,952 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,520 hrs · 43,944 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 44,344 hrs · 43,761 cycles

R2 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 43,928 hrs · 43,355 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE DOOR CABLE PER MM.

Part: LENS — CRACKED (CABIN) · airframe 43,899 hrs · 43,318 cycles

DURING SCHEDULED PM CHECK, FOUND BULLNOSE LIGHT LENS AT ROW 8 ABC CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 43,376 hrs · 42,835 cycles

L2 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: ACTUATOR — BROKEN (RT WING SPOILER) · airframe 42,967 hrs · 42,460 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 OUTBOARD SPOILER ACTUATOR END BROKEN. REMOVED AND REPLACED NR 5 SPOILER ACTUATOR PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 42,973 hrs · 42,467 cycles

DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR ATTACHMENT POINT, STATION 90. REPAIRED SKIN CRACK PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,660 hrs · 40,288 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS CRACKED AT LBL 24, BS 669 & BS 672. REPAIRED FLOORBEAMS PER SWA EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 40,660 hrs · 40,288 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT OUTBOARD AFT T/E FLAP DELAMINATED ON BOTTOM SURFACE. REMOVED AND REPLACED RT OUTBOARD AFT T/E FLAP PER MM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 40,404 hrs · 40,052 cycles

DURING SCHEDULED C1 CHECK, FOUND CAPT'S UPPER WINDOW POST CRACKED. REPAIRED WINDOW POST PER SRM.

Part: STRIP — LOOSE (CABIN) · airframe 40,404 hrs · 40,052 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROW 6 & ROW 7 ABC. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,396 hrs · 40,042 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 882, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,498 hrs · 39,226 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19L. REPAIRED SKIN PER SRM.

Part: CABLE — MISROUTED (AFT SVC DOOR) · airframe 39,498 hrs · 39,226 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: BUSHING — WORN (COCKPIT) · airframe 38,597 hrs · 38,392 cycles

T/E FLAP HANDLE WOULD NOT MOVE PAST 5 DEGREES. REMOVED AND REPLACED T/E FLAP HANDLE BUSHING PER MM.

Part: SPOILER — CRACKED (RT WING) · airframe 38,547 hrs · 38,346 cycles

DURING WALK AROUND INSPECTION, FOUND NR 5 L/E GROUND SPOILER CRACKED. REMOVED AND REPLACED NR 5 L/E GROUND SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,422 hrs · 38,223 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 890, BETWEEN STR 24R AND STR 25R. REPAIRED SKIN PER SRM.

Part: TAB — WORN (LT ELEVATOR) · airframe 37,624 hrs · 37,451 cycles

DURING SCHEDULED A2 CHECK, SWA SI 11138-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB AND HINGE BUSHINGS FOR NR 1 AND NR 2 HINGE POINTS PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 37,624 hrs · 37,451 cycles

DURING SCHEDULED A2 CHECK, SWA SI 11138-55, FOUND RT ELEVATOR TAB HINGE BUSHINGS WORN AT NR 1, NR 3, AND NR 4 HINGE ATTACH POINTS. REMOVED AND REPLACED BUSHINGS PER MM.

Part: FEEL UNIT — FAULTY (ELEVATOR) · airframe 37,261 hrs · 37,112 cycles

ELEVATOR FEEL FORCE IS LOW, IT TAKES MUCH LESS FORCE THAN NORMAL TO ROTATE OR FLARE THE A/C. REMOVED AND REPLACED ELEVATOR FEEL AND CENTERING UNIT PER MM.

Part: BRACKET — LOOSE (AFT ENTRY DOOR) · airframe 36,904 hrs · 36,778 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FLOOR ATTACH BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SLIDE — DEPLOYED (FWD SVC DOOR) · airframe 35,342 hrs · 35,270 cycles

DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. R&R EVAC SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 34,473 hrs · 34,435 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: BLADE — FOD (#2 ENG) · airframe 34,145 hrs · 34,100 cycles

AIR TURNBACK. FOLLOWING PROBABLE BIRD STRIKE, nr 2 ENGINE HAD UNUSAL SOUND & EXCESSIVE VIBRATION. ACCOMPLISHED BIRD STRIKE INSPECTION & FOUND 4 FAN BLADES BENT. Removed and replaced ALL nr 2 ENG FAN BLADES PER MM & SWA SAM 455.

Part: SLIDE — DISLODGED (FWD SERVICE DOOR) · airframe 32,697 hrs · 32,683 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE FALLING OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 32,614 hrs · 32,608 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND BOTH FWD EMERGENCY FLASHLIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,614 hrs · 32,608 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND FUSELAGE INNER SKIN CORRODED AT STR 7L, BS 727B. REPAIRED SKIN PER SRM.

Part: SPLICE — CRACKED (CABIN) · airframe 32,614 hrs · 32,608 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND STR 4L CRACKED AT SPLICE, BS 908. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,614 hrs · 32,608 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND SHEAR TIE CRACKED AT STR 9R, BS 1040. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (CABIN) · airframe 32,614 hrs · 32,608 cycles

DURING SCHEDULED D-CHECK , FOUND BS 908, STR CRACK STR 4R. REPAIRED STR PER SRM.

Part: STRINGER — DAMAGED (CABIN) · airframe 32,614 hrs · 32,608 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND DAMAGED STR 7L AT BS 727B. REPAIRED DAMAGED STR PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,614 hrs · 32,608 cycles

DURING SCHEDULED D-CHECK AT DALFORT, FOUND SHEAR TIE CRACKED AT BS 847, BETWEEN STR 13L AND 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LIGHT — INOPERATIVE (ROW 10 - 14)

EEPLS INOP BETWEEN ROWS 10-14. RESECURED LOOSE WIRE PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS INOP, ROWS 6 TO 13. REPAIRED WIRING PER WDM.

Part: LIGHT — LOOSE (CABIN)

EEPLS FWD END LOOSE. REINSTALLED LIGHT ASSY PER MM.

Part: WIRE — LOOSE (ROW 3)

EMERGENCY ESCAPE FLOOR TRACK LIGHTS INOP FWD OF ROW 3. RECONNECTED WIRE TO LIGHT PER MM.

Part: BULB — INOPERATIVE (EMERGENCY EXIT)

DURING SCHEDULED C3 CHECK, FOUND AFT EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOP. SPLICED WIRE TO LAMP ASSY PER MM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED CHECK, FOUND NR 2 FRONT FLOOR TRACK LIGHTING TRACK INOP. REPAIRED WIRING AT ROW 2 PER MM.

Part: WIRE — DAMAGED (ROW 2)

DURING SCHEDULED CHECK, FOUND FLOOR TRACK LIGHTING LIGHT (NR 2 FROM FRONT) INOP. REPAIRED WIRING AT ROW 2 LIGHT SOCKET, OP CKS OK PER MM.

Part: WIRE — DAMAGED (ROW 2)

DURING SCHEDULED CHECK, FOUND FLOOR TRACK LIGHTING LIGHT (NR 2 FROM FRONT) INOP. REPAIRED WIRING AT ROW 2 LIGHT SOCKET, OP CKS OK PER MM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SC CHECK, FOUND RT OVERWING EXIT EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK PER BOEING MM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SC CHECK, RT OVERWING EXIT INTERIOR EMERGENCY LIGHTS DID NOT ILLUMINATE, LIGHT LOCATED ABOVE DOOR AND LIGHT FORWARD OF DOOR. REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER PER M/M.

Part: WIRE — BROKEN (CABIN)

AFT EMERGENCY EXIT FLOOR TRACK LIGHINTING INOPERATIVE(APPROX 10FT). REPAIRED BROKEN WIRE PER M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND OVER WING RT SIDE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK BASE PER BOEING MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING INT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, SYS OPS NORMAL PER BOEING MM, PER BOEING SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING PRE-FLIGHT INSPECTION, FIRST 3 FLOOR PROX LIGHTS AT FRONT OF AIRCRAFT ARE INOP. REPAIRED FLOOR TRACK AT ROW 3ABC.

Part: SKIN — DAMAGED (BS 1006)

DURING SCHEDULED C3 CHECK, FOUND A FUSELAGE SKIN DAMAGE AT BS 1006, RIGHT SIDE BELOW WL 208. REPAIRED PER BOEING SRM.

Part: SLIDE — LOW PRESS (AFT ENTRY)

DURING SCHEDULED RON CHECK, FOUND AFT ENTRY DOOR SLIDE PRESSURE LOW. REPLACED PER BOEING M/M.

Part: SKIN — GOUGED (BS 969)

DURING SCHEDULED BC4 CHECK, FOUND FUSLAGE SKIN GOUGED AT BS 969, S17L. REPAIRED PER SWA RA 1-553-1523.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED BC4 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHTING INOPERATIVE AT AFT SERVICE DOOR. REPLACED BATTERY AND CHARGER HOUSING PER BOEING M/M.

Part: CHARGERS — INOPERATIVE (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY AND FWD SERVICE DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BOTH BATTERY CHARGERS ASSEMBLIES PER BOEING M/M.

Part: HOUSING — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD ENTRY DOORS EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LT LIGHT SOCKET AND RT AND LT BATTERY PACK HOUSINGS PER BOEING M/M.

Part: CHARGER — INOPERATIVE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR EXIT LIGHT INOP. REPLACED BATTERY CHARGER PER BOEING M/M.

Part: WIRE — DISCONNECTED (CABIN)

DURING PREFLIGHT, FOUND EMERGENCY EXIT LIGHTS INOP AT ROW 12. FOUND AND RECONNECTED WIRE AT SOCKET PER BOEING M/M.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LEFT POWER SUPPLY HOUSING PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND AFT DOOR SLIDE LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: STRINGER — CRACKED (BS 303.9)

DURING SCHEDULED 1/2 D-CHECK, FOUND NR 1 STRINGER WEB CRACKED AT BS 303.9 LEFT SIDE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: DOOR FRAME — CRACKED (BS 294)

DURING SCHEDULED 1/2 D-CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED AT FWD LOWER CORNER, BS 294. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: WEB — CRACKED (BS 344)

DURING SCHEDULED 1/2 D-CHECK, FOUND WEB CRACKED AT BS 344, BL 0 AT UPPER FWD CORNER. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: ENGINE — OVERTEMP (NBR 1)

EXPERIENCED NUMBER 1 ENGINE FLAMEOUT. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND AFT TURBINE SECTION DAMAGE. REPLACED ENGINE ASSEMBLY AND PERFORMED POWER ASSURANCE RUN PER BOEING M/M.