N317WN

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 77,446 hrs · 54,471 cycles

AFT CARGO FWD LT FIRE PROTECTION MX LIGHT ILLUMINATED DURING CRUISE FLIGHT. R & R SMOKE DETECTOR IAW MM.

Part: WIRE — DAMAGED (CABIN) · airframe 77,304 hrs · 54,368 cycles

FORWARD ENTRY DOOR, LOWER EMER EXIT LIGHT INOPERATIVE. REPAIRED WIRE IAW WDM & AMM.

Part: LIGHT — DAMAGED (EXIT SIGN) · airframe 77,304 hrs · 54,368 cycles

FORWARD LAVATORY, WALL MOUNTED EMER EXIT SIGN LIGHT DAMAGED. REPAIRED SIGN LIGHT IAW AM & WDM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 77,304 hrs · 54,368 cycles

R2 DOOR LOWER SILL WEB CORRODED, BETWEEN BS 970 - 986, RBL 45. R & R SILL WEB IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,304 hrs · 54,368 cycles

FRAME CORRODED AT BS 993, RBL 45. REPAIRED FRAME IAW ER & EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 77,304 hrs · 54,368 cycles

AFT ENTRY DOOR LOWER SILL WEB CORRODED BETWEEN BS 980 - 986, LBL 45. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 77,304 hrs · 54,368 cycles

RIGHT CREASE BEAM WEB UPPER SURFACE CORRODED, BETWEEN BS 616 - 638, WL 208. R & R WEB IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,304 hrs · 54,368 cycles

FUSELAGE SKIN CRACKED AT BS 960, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,304 hrs · 54,368 cycles

FLOORBEAM CORRODED AT BS 328, LBL 28. R & R FLOORBEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,304 hrs · 54,368 cycles

FLOORBEAM CORRODED AT BS 312, RBL 8. REPAIRED FLOORBEAM IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,304 hrs · 54,368 cycles

STRINGER CLIP CRACKED, BS 276.5, STRINGER 15R. R & R CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,304 hrs · 54,368 cycles

FITTING CRACKED AT BS 295.5, RBL 46 IN FWD CABIN. REPLACED FITTING IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,304 hrs · 54,368 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STRINGER 28L - 28R. REPAIRED SHEAR TIE IAW ER & EA.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 77,304 hrs · 54,368 cycles

FORWARD CARGO BAY RT CARGO TRACK CRACKED, BETWEEN BS 410 - 500A+10. R & R TRACK IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 77,304 hrs · 54,368 cycles

GIRT BAR FITTING SUPPORT ANGLE CORRODED AT BS 344, LBL 59. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 77,304 hrs · 54,368 cycles

GIRT BAR FITTING SUPPORT ANGLE, CORRODED AT BS 312, LBL 53. R & R ANGLE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 77,304 hrs · 54,368 cycles

AFT BULKHEAD SUPPORT CORRODED AT BS 500D, BETWEEN STRINGER 26L - 28R. R & R SUPPORT IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 77,242 hrs · 54,306 cycles

DOME WEB CRACKED AT BS 1016, STRINGER 17R. REPAIRED WEB IAW EA.

Part: FLASHLIGHT — LOOSE (CABIN) · airframe 77,148 hrs · 54,238 cycles

FORWARD FLASHLIGHT LOOSE. SECURED FLASHLIGHT IAW MT.

Part: WINDOW — CRACKED (COCKPIT) · airframe 76,990 hrs · 5,125 cycles

L1 WINDOW DELAMINATED, ARCED & CRACKED. R & R NR 1 WINDOW IAW MM.

Part: LENS — MISSING (CABIN) · airframe 76,926 hrs · 54,085 cycles

AFT EMER EXIT LIGHT LENS MISSING AT ROW 23. INSTALLED LENS IAW SIP.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 75,430 hrs · 52,928 cycles

RIGHT ELEVATOR INBD TAB CONTROL DELAMINATED. R & R TAB IAW AMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 74,001 hrs · 51,877 cycles

R2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: LIGHT — DIRTY (CABIN) · airframe 74,001 hrs · 51,877 cycles

RIGHT EEPLS DIRTY. CLEANED EEPLS IAW AMM.

Part: LIGHT — DIRTY (CABIN) · airframe 74,001 hrs · 51,877 cycles

LEFT EEPLS DIRTY. CLEANED EEPLS IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 73,629 hrs · 51,632 cycles

AFT PRESS BULKHEAD WEB Y CHORD CRACKED BS 1016, STRINGER 6R. REPAIRED Y CHORD IAW SRM.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

PRESSURE DECK WEB CRACKED AT BS 665 BETWEEN BL 0.07 TO RBL 2. REPAIRED WEB IAW EO & EA.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

PRESSURE DECK WEB CRACKED AT BS 665 BETWEEN BL 0.07 TO LBL 10. REPAIRED WEB IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

FRAME CRACKED AT BS 312 BETWEEN STRINGER 18R TO STRINGER 19R. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

SKIN CRACKED AT BS 727 LT SIDE AT 3 O'CLOCK POSITION. REPAIRED SKIN IAW EO & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

WEB CRACKED AT BS 1016 STRINGER 7L. REPAIRED WEB IAW EO.

Part: SKIN — CRACKED (LT WING) · airframe 71,941 hrs · 50,459 cycles

LT WING FIXED LE SKIN AT KRUEGER FLAP SEAL DOOR CUT OUT CRACKED AT LE SIDE 208 LT SIDE. REPAIRED CUTOUT IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 71,941 hrs · 50,459 cycles

RT WING SIDE FIXED LE SKIN AT KRUEGER FLAP SEAL DOOR CUT OUT CRACKED AT LE S 208. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

SKIN CRACKED AT BS 294.5+4 STRINGER 18R. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED BETWEEN BS 887 TO BS 907. R&R ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (NLG WW) · airframe 71,941 hrs · 50,459 cycles

LT NLG WW WEB CRACKED AT BS 243.7+2.5, WL 169. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 71,941 hrs · 50,459 cycles

RT NLG WW CRACKED AT BS 243.7+4.5, WL 169. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

LT NLG WW WEB CRACKED AT BS 251.6, WL 178. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 71,941 hrs · 50,459 cycles

RT NLG WW WEB CRACKED AT BS 243.7+3.5," WL 169. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 71,941 hrs · 50,459 cycles

LT SIDE OF NLG WW WEB CRACKED AT BS 243.7+3.5, WL 169. REPAIRED WEB IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

UNDER GALLEY AFT CARGO COMPARTMENT ANGLE CORRODED AT BS 1022, BL 0. R&R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

CLIP ANGLE CRACKED AT BS 348.2 STRINGER 16L. R & R CLIP ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

WEB CRACKED BETWEEN BS 294.5 TO BS 303.9, STRINGER 8L. R&R WEB IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

TIE CLIP CRACKED AT STATION 294.5, STRINGER 12L. R&R TIE CLIP IAW SRM & DRAWING.

Part: PANEL — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

CURVED CORRUGATED PANEL CRACKED LOCATED BETWEEN BS 720 TO BS 727 RBL 6.10 KEEL BEAM. R & R PANEL IAW SRM & DRAWING.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 71,941 hrs · 50,459 cycles

LT WING FIXED LE LOWER SKIN PANEL CRACKED. REPAIRED PANEL IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

AFT CARGO COMPARTMENT STRAP CRACKED BETWEEN BS 727 TO BS 767, STRINGER 25R. R&R STRAP IAW SRM & DRAWING.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

CHORD CRACKED AT BS 665, BL 0.07. REPAIRED CHORD IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

SKIN CRACKED AT BS 328+13, STRINGER 17L. REPAIRED SKIN IAW EO & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 665, RBL 24.8. REPAIRED CHORD IAW EO & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

LONGITUDINAL FLOOR BEAM CRACKED AT BS 661 BBL 0.07. REPAIRED WEB IAW EO & EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

CHORD CRACKED AT BS 727 UPPER AFT LOWER FWD & LOWER AFT FASTENER HOLES LT SIDE 3 O'CLOC. REPAIRED CHORD IAW EO &EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

CHORD AT AFT LOWER FASTENER HOLE CRACKED AT BS 727 INSPECTION AREA RT SIDE 5 O'CLOCK POSITION. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

LONGITUDINAL FLOOR BEAM CRACKED AT BS 661 BBL 0.07. REPAIRED CHORD IAW EO & EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

STRINGER CRACKED AT BS 727 STRINGER 18A AT AFT LOWER FASTENER HOLE RT SIDE. REPAIRED STRINGER IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 71,941 hrs · 50,459 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED BETWEEN BS 705 TO BS 715, LBL 24.8. REPAIRED WEB IAW EA.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 71,567 hrs · 50,183 cycles

BURNING RUBBER SMELL FORWARD GALLEY AREA & FIRST 5 ROWS, GASPER WAS ON, TURNED OFF. SMELL SUBSIDED. R&R GASPER FAN & RECIRC FAN FILTER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,965 hrs · 48,318 cycles

LEFT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 10. REMOVED & REPLACED BULB PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,965 hrs · 48,318 cycles

LEFT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 10. REMOVED & REPLACED BULB PER AMM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 68,866 hrs · 48,240 cycles

RIGHT WING NR 5 SLAT DELAMINATED ON UPPER INBOARD SKIN EDGE. REMOVED AND REPLACED SKIN IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 68,698 hrs · 48,106 cycles

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

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 68,457 hrs · 47,918 cycles

LEFT MLG NO GREEN LIGHT AND NO RED LIGHT WITH GEAR SELECTED DOWN. GEAR SELECTED UP, SYSTEM TEST GREEN LIGHT WILL NOT ILLUMINATE. RELAMP AND TEST GOOD PER MM.

Part: PIN — INOPERATIVE (CABIN) · airframe 68,006 hrs · 47,569 cycles

EMERGENCY LIGHTS FOUND GROUND WIRE PIN INOP. REMOVED AND REPLACED PIN PER WDM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,006 hrs · 47,569 cycles

RIGHT FWD EMERGENCY LIGHT BATTERY PACK HOUSING FAILED. REPLACED BATTERY PACK HOUSING PER M/M.

Part: HOUSING — DEFECTIVE (CABIN) · airframe 67,420 hrs · 47,134 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY HOUSING PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 67,262 hrs · 47,017 cycles

R1 WINDOW ARCED DURNG DESCENT THEN IT CRACKED. REMOVED AND REPLACED R1 WINDOW PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,185 hrs · 46,955 cycles

FWD GALLEY EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER M/M.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,056 hrs · 46,856 cycles

RT FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME INNER CHORD WEB CRACKED AT BS 360, STR 20R. REPAIRED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND PRESSURE DECK UPPER WEB CRACKED AT BS 664, LBL 31.0. REPAIRED WEB IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK FOUND, STRINGER SPLICE CRACKED AT BS 359, STR 7L. REMOVED AND REPLACED SPLICE PER SRM.

Part: LENS — CRAZED (CABIN) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRAZED. REMOVED AND REPLACED LENS ASSY PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT KEEL BEAM ANGLE CORRODED AT BS 540, RBL 12. REPAIRED ANGLE IAW SRM AND DWG.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND BEADED HORIZONTAL PRESSURE WEB CRACKED AT BS 664, LBL 39.5. REPAIRED WEB PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 540, STR 27R. REPAIRED FRAME PER EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLIGHT DECK FLOOR WEB CRACKED AT BS 246.6, RBL 15. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLIGHT DECK FLOOR WEB OPC COMPUTER CRADLE BRACKED, FWD O/B MOUNT HOLE CRACKED AT BS 246.6, RBL 22. REPAIRED WEB IAW EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT KEEL BEAM CORRODED AT STA 540. REMOVED AND REPLACED KEEL BEAM SECTION PER SRM.

Part: LENS — DIRTY (CABIN) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS DISCOLORED. CLEANED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT FRAME I/B LOWER FASTENER INNER CHORD CRACKED AT BS 616. REPAIRED CHORD PER SWA EA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND CUSP WEB CORRODED AT BS 597, STR 17L. REPAIRED WEB IAW SRM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GAUGE PRESSURE LOW. R&R SLIDE PER MM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP DAMAGED AT BS 907, STR 19L. R&R CLIP IAW SRM.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD CREASED AT BS 1016, ON AFT SIDE AT STIFFENER 10 AND 8 INCHES DOWN FROM CENTER OF PRESSURE WEB. REPAIRED BULKHEAD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016 AT APPROX 2 O'CLOCK POSITION AT CENTER OF DOME CAP CENTER. REPAIRED BULKHEAD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016 AT APPROX 5 O'CLOCK POSITION AT CENTER OF DOME CAP CENTER. REPAIRED BULKHEAD PER SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND CUSP WEB CRACKED AT BS 639, STR 17L. REPAIRED WEB PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016 AT APPROX 7 O'CLOCK POSITION AT CENTER OF DOME CAP CENTER. REPAIRED BULKHEAD PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 67,008 hrs · 46,818 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 480 TO BS 500, STR 17L. REPAIRED BEAM IAW EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 66,788 hrs · 46,660 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 66,127 hrs · 46,141 cycles

CABIN ALT WARNING HORN AT FL 340, CABIN ALTITUDE 10,500. REMOVED AND REPLACED MAIN OUTFLOW VALVE PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 65,773 hrs · 45,856 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE LOW PRESSURE. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,551 hrs · 45,684 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS INOP AT ROW 6. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — BROKEN (EXIT SIGN) · airframe 62,933 hrs · 43,644 cycles

AFT RT EMERGENCY EXIT SIGN LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,194 hrs · 42,346 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 321.5, WL 211.8. REPAIRED SKIN PER EO.

Part: SKIN — DELAMINATED (SPOILER) · airframe 61,194 hrs · 42,346 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SPOILER SKIN DELAMINATED. REPAIRED SPOILER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,194 hrs · 42,346 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR AT BS 308.5, WL 230. REPAIRED SKIN PER EO.

Part: LIGHT — BROKEN (CABIN) · airframe 61,194 hrs · 42,346 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD GALLEY LOWER EMERGENCY EXIT LIGHT BASE BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 61,194 hrs · 42,346 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING O/B END UPPER SURFACE NR 3 SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,194 hrs · 42,346 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED CHORD PER EO.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,194 hrs · 42,346 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,194 hrs · 42,346 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT LOWER BULB INOP. REMOVED AND REPLACED BULB PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,194 hrs · 42,346 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT CREASE BEAM CHORD CORRODED BETWEEN BS 259.5 TO BS 360. REMOVED AND REPLACED CHORD PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 61,194 hrs · 42,346 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,194 hrs · 42,346 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER ACO.

Part: COVER — BROKEN (CABIN) · airframe 61,194 hrs · 42,346 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: MODULE — FAULTY (E&E BAY) · airframe 60,770 hrs · 42,023 cycles

DIVERSION, GEAR LEVER WOULD NOT PAST OFF AFTER RAISING FLAPS "NO" TAKEOFF WARNING SO CONTINUED PER QRH "LEVER LOCK SOLENOID FAILURE". REMOVED AND REPLACED M991 MODULE AND R276 RELAY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,486 hrs · 41,808 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — DEBONDED (CABIN) · airframe 59,741 hrs · 41,230 cycles

EEPLS DISBONDED AT FWD RT SIDE. SECURED EEPLS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 58,579 hrs · 40,403 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING O/B TRAILING EDGE AFT FLAP DELAMINATED AT I/B EDGE. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP BETWEEN ROW 15 TO ROW 16. REPAIRED WIRE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP AT ROW 10. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,461 hrs · 40,322 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 291, WL 233. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 727E, STR 13R. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 304, WL 238. REPAIRED SKIN PER ER.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 304, WL 259. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED SHEAR TIE PER PAE DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP DAMAGED AT BS 500A, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 300, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 19R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 727D, STR 13R. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867, STR 23R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 291, WL 230, R1 DOOR HINGE CUTOUT. REPAIRED SKIN PER SRM & ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500, STR 14R. REPAIRED FRAME PER ER.

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 500A, STR 13L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 540, STR 26L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 2 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 500, BETWEEN STR 13L TO 14L. REPAIRED FRAME PER ER.

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 727C, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER ER.

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 500C, STR 13L. REPAIRED FRAME PER ER.

Part: STRINGER CLIP — CRACKED (BS 727E S16L) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 693, STR 4L. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 859, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 996, STR 25L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,456 hrs · 40,318 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (BS 736E S18R) · airframe 57,682 hrs · 39,751 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 736E, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 730D S23R) · airframe 57,682 hrs · 39,751 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730D, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,484 hrs · 38,858 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,898 hrs · 38,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 748D, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,898 hrs · 38,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730, STR 23L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,898 hrs · 38,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,898 hrs · 38,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 410 AND BS 448, STR 28R. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,898 hrs · 38,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 887, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,898 hrs · 38,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 55,898 hrs · 38,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT KEEL BEAM CORRODED AT BS 523. REPAIRED KEEL BEAM PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 55,898 hrs · 38,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND BELTFRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8R) · airframe 55,898 hrs · 38,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: BEARING — WORN (LT ELEVATOR) · airframe 55,898 hrs · 38,410 cycles

DURING SCHEDULED BRDG CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING PER MM.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 55,898 hrs · 38,410 cycles

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

Part: FRAME — CRACKED (BS 400 S8R) · airframe 55,898 hrs · 38,410 cycles

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

Part: FLAP TRACK — CORRODED (NR 2 FLAP) · airframe 55,898 hrs · 38,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 OUTBOARD FLAP INBOARD TRACK FITTING CORRODED. REPAIRED FLAP TRACK PER SWA EA.

Part: BEARING — WORN (RT ELEVATOR) · airframe 55,898 hrs · 38,410 cycles

DURING SCHEDULED BRDG CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING PER MM.

Part: FLAP TRACK — CORRODED (NR 7 FLAP) · airframe 55,898 hrs · 38,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 7 OUTBOARD FLAP INBOARD TRACK FITTING CORRODED. REPAIRED FLAP TRACK PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8L) · airframe 55,898 hrs · 38,410 cycles

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

Part: FRAME — CRACKED (BS 294 S17R) · airframe 55,898 hrs · 38,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND STUB FRAME CRACKED AT BS 294.5, STR 17R. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 55,446 hrs · 38,060 cycles

DURING SCHEDULED C1 CHECK, FOUND RIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 55,446 hrs · 38,060 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 55,446 hrs · 38,060 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 55,431 hrs · 38,045 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 20 ABC. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,256 hrs · 37,911 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 745D AND BS 730E, STR 24L AND STR 23L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (CABIN) · airframe 55,201 hrs · 37,865 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,990 hrs · 37,696 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,990 hrs · 37,696 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: MODULE — FAULTY (HYD SYSTEM) · airframe 54,670 hrs · 37,444 cycles

DIVERSION / DECLARED EMERGENCY. HYD A-SYS OVERHEAT LIGHT ILLUMINATED, DIM -TEST C/B TRIPPED AND MASTER CAUTION SYS LOSS. REMOVED AND REPLACED HYD A-SYS PUMP & OVERHEAD HYD CONTROL MODULE PER MM.

Part: FAN — FAULTY (E&E BAY) · airframe 54,303 hrs · 37,147 cycles

AIR TURNBACK, DURING CLIMB F/A REPORTED STRONG ELECTRICAL/CHEMICAL ODOR IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: DOOR FRAME — CRACKED (BS 348 S16L) · airframe 53,162 hrs · 36,262 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR FRAME WEB CRACKED AT BS 348, STR 16L. REPAIRED FRAME WEB PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,808 hrs · 35,997 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 745D, STR 22L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 51,685 hrs · 35,123 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 51,012 hrs · 34,585 cycles

AIR TURNBACK. ON DEPARTURE NR 2 ENGINE WOULD NOT ACCELERATE ABOVE 60 PERCENT N1, TURNING PMCS ON AND OFF MADE NO DIFFERENCE. REMOVED AND REPLACED ENGINE MEC PER MM.

Part: SKIN — CRACKED (BS 520) · airframe 50,879 hrs · 34,476 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28L. REPAIRED SKIN PER SWA EA.

Part: DOOR FRAME — CRACKED (BS 440) · airframe 62,542 hrs · 58,334 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT CRACKED AT BS 440, NR 5 STOP PAD. REPAIRED FRAME SECTION PER ER AND SB.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 49,004 hrs · 32,994 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT LOWER SKIN CRACKED. REPAIRED SLAT PER SRM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 49,004 hrs · 32,994 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 48,571 hrs · 32,628 cycles

R2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: SHAFT — CORRODED (RT WING TE FLAP) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING INBOARD T/E MIDFLAP OUTBOARD GIMBLE SHAFT CORRODED. REMOVED AND REPLACED GIMBLE SHAFT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER BFG ER.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER BFG ER.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: FRAME — CRACKED (FWD CARGO) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, LT SIDE, WL 208. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (AFT CARGO) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, RBL 21. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 986, RBL 45. REPAIRED FLOORBEAM PER BFG ER.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED BETWEEN BS 727D TO BS 867, LBL 8. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 807, BS 827, BS 847, BS 867, BS 887 & BS 907, STR 8R TO STR 9R. REPAIRED FRAMES PER SRM.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FLOOR BRACKET CORRODED. REMOVED AND REPLACED AFT BRACKET PER SRM.

Part: FRAME — CRACKED (CABIN FLOOR) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 294, RBL 55, WL 209. REPAIRED STUB FRAME PER BFG ER & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 747, BS 807, BS 827, BS 847 & BS 867, STR 8L TO STR 9L. REPAIRED FRAMES PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 420, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CORRODED (CABIN FLOOR) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 480 & BETWEEN BS 887 TO BS 907. REMOVED AND REPLACED CREASE BEAM WEB SECTIONS PER SRM.

Part: WEB — CORRODED (CABIN FLOOR) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420 & BETWEEN BS 847 TO BS 867. REMOVED AND REPLACED CREASE BEAM WEB SECTIONS PER SRM.

Part: FLOORBEAM — CORRODED (COCKPIT FLOOR) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT FLOORBEAM CORRODED AT BS 270, LBL 10 TO RBL 10, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 48,342 hrs · 32,440 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 500D, STR 12R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 48,183 hrs · 32,314 cycles

LT OVERWING EMERGENCY EXIT DOOR LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 47,329 hrs · 31,654 cycles

L2 COCKPIT WINDOW ARCING & CRACKED DURING FLIGHT. REMOVED AND REPLACED L2 COCKPIT WINDOW PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 47,245 hrs · 31,588 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 47,245 hrs · 31,588 cycles

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

Part: FRAME — CRACKED (AFT CARGO DOOR) · airframe 47,242 hrs · 31,585 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR MID FRAME CRACKED. REMOVED AND REPLACED CARGO DOOR PER MM.

Part: SKIN — WORN (FUSELAGE) · airframe 47,096 hrs · 31,484 cycles

DURING SPV, FOUND UPPER RT AND LT FUSELAGE SKIN FROM BS 860 TO BS 887, UNDER DORSAL FIN, WORN. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 47,093 hrs · 31,482 cycles

DURING SPV, FOUND STRINGER CLIP AT BS 360, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CABLE — MISROUTED (L2 DOOR GIRT BAR) · airframe 46,307 hrs · 30,872 cycles

DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED SLIDE CABLE PER MM.

Part: FITTING — DIRTY (R2 DOOR SLIDE) · airframe 46,045 hrs · 30,635 cycles

F/A HAD DIFFICULTY DISARMING R2 DOOR EVAC SLIDE. CLEANED R2 DOOR EVAC SLIDE GIRT BAR FLOOR ATTACH FITTING PER MM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 45,615 hrs · 30,297 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR SKIN AT UPPER AFT CORNER, CRACKED. REPAIRED DOOR SKIN PER SRM.

Part: UPLOCK SENSOR — MALFUNCTIONED (LT MLG) · airframe 44,420 hrs · 29,315 cycles

AIR TURNBACK, DURING POSITION FERRY FROM PAE TO PHX, AFTER LAP INSPECTION, DUE TO LT MLG UNSAFE LIGHT ILLUMINATED. CYCLED GEAR 4 TIMES, LIGHT REMAINED ON IN THE UP POSITION. REMOVED AND REPLACED LT, MLG UPLOCK SENSOR PER MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 44,415 hrs · 29,311 cycles

DURING SPV, FOUND FWD GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 44,228 hrs · 29,165 cycles

LT AFT GALLEY AREA EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 44,211 hrs · 29,147 cycles

DURING SCHEDULED SP CHECK, FOUND STRINGER 16 L CRACKED AT BS 500. REPAIRED PER SB.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,211 hrs · 29,147 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CREASE BEAM CORRODED, BS 500 TO BS 500A, LT SIDE. REPAIRED CREASE BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 44,211 hrs · 29,147 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 663, STR 10L AND 10R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SENSOR — FAULTY (NLG) · airframe 43,661 hrs · 28,706 cycles

DURING GEAR RETRACTION, NLG UNSAFE WARN LIGHT ILLUMINATED, RECYCLED GEAR AND LIGHT DID NOT EXTINGUISHED. REMOVED AND REPLACED NLG UPLOCK AND DOWLOCK SENSORS S845 AND S846. OPS CK GOOD PER MM.

Part: INDICATOR — OUT OF LIMITS (SLIDE BOTTLE) · airframe 42,838 hrs · 28,056 cycles

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

Part: RELAY — FAULTY (NLG LATCH) · airframe 42,733 hrs · 27,988 cycles

GEAR HANDLE RAISED, NLG RED UNSAFE LIGHT DID NOT EXTINGUISH. CYCLED GEAR ALL GREEN LIGHTS ILLUMINATED, RED LIGHT EXTINGUISHED. REMOVED AND REPLACED S845 SWITCH AND R375 NLG LATCHING RELAY PER MM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,661 hrs · 27,930 cycles

DURING SCHEDULED RON, FOUND NLG ACTUATOR UPPER SUPPORT GUSSET FITTING CRACKED. REMOVED AND REPLACED NLG ACTUATOR UPPER SUPPORT FITTING PER BAC DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,459 hrs · 27,775 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: GIRT BAR — LOOSE (AFT SVC DOOR) · airframe 42,459 hrs · 27,775 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING LOOSE. SECURED ATTACH FITTING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,459 hrs · 27,775 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 42,459 hrs · 27,775 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING NR 3 L/E SLAT CRACKED ON LOWER SKIN AROUND ACTUATOR CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,576 hrs · 56,295 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 490, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 42,459 hrs · 27,775 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 4 L/E SLAT CRACKED ON LOWER SKIN JUST BELOW RETRACT ACTUATOR. REPAIRED NR 4 L/E SLAT PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 42,459 hrs · 27,775 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT OUTBOARD AFT T/E FLAP DELAMINATED. REPAIRED LT OUTBOARD AFT T/E FLAP PER SRM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 40,168 hrs · 25,966 cycles

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

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 40,168 hrs · 25,966 cycles

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

Part: SLIDE — MISROUTED (AFT SVC DOOR) · airframe 40,168 hrs · 25,966 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW AND SLIDE GIRT CABLE MISROUTED. REPOSITIONED SLIDE AND REROUTED CABLE PER MM.

Part: TAB — WORN (RT ELEVATOR) · airframe 40,015 hrs · 25,843 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK, (NR 1 HINGE WORN ). REMOVED AND REPLACED RT ELEVATOR TAB PER MM.

Part: BATTERY — ERRATIC (CABIN) · airframe 38,634 hrs · 24,689 cycles

DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT WILL NOT STAY ILLUMINATED. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 38,340 hrs · 24,449 cycles

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

Part: SLIDE — OUT OF ADJ (L1 DOOR) · airframe 37,722 hrs · 23,925 cycles

FWD ENTRY DOOR EVACUATION SLIDE OUT OF ADJUST. READJUSTED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 37,601 hrs · 23,825 cycles

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

Part: SLIDE — DEPLOYED (FWD ENTRY DOOR) · airframe 37,580 hrs · 23,806 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED AT THE GATE. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 36,478 hrs · 22,906 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 35,504 hrs · 22,077 cycles

DURING SCHEDULED C3 CHECK, FOUND LT & RT OVERWING EMERGENCY EXIT LIGHT LENSES LOOSE. SECURED LENSES PER MM.

Part: FLAP — BROKEN (LT WING) · airframe 34,893 hrs · 21,570 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING L/E NR 1 KRUEGER FLAP OUTBD END BROKEN AT SPRING LOADED FLAP DOOR. REMOVED AND REPLACED KRUEGER FLAP PER MM.

Part: LENS — MISSING (CABIN) · airframe 24,592 hrs · 21,321 cycles

EMERGENCY EXIT LIGHT LENS COVER MISSING AT BULLNOSE, ROW 12 DEF. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 34,504 hrs · 21,247 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING AT BULLNOSE, ROW 13 DEF. INSTALLED LENS PER MM.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 34,266 hrs · 21,048 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT AFT LOWER CORNER BEHIND DOOR STOP FITTING. REPAIRED DOOR FRAME PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,266 hrs · 21,048 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE ANGLE CRACKED AT FWD ENTRY DOOR, BS 301, STR 10L. REPAIRED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,266 hrs · 21,048 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT, FWD UPPER CORNER. REPAIRED SKIN PER RA 1-353-1253 & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,266 hrs · 21,048 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 770 FLOOR BEAM CORRODED AT RBL 13. REPAIRED FLOOR BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 34,266 hrs · 21,048 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CRACKED AT BS 520, RBL 45.5 & LBL 45.5, UPPER T RADIUS. REPAIRED FLOOR BEAM PER RA 1-353-2416.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,266 hrs · 21,048 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STR CLIP CRACKED AT BS 1121, STR 2L, UPPER RADIUS. R&R STR CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,266 hrs · 21,048 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 200, LBL 5. REPAIRED BULKHEAD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,266 hrs · 21,048 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STR CLIP CRACKED AT BS 1104, STR 3R. R&R STR CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 34,266 hrs · 21,048 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CRACKED AT BS 787, RBL 14. REPAIRED FLOOR BEAM PER SRM.

Part: BRACKET — CORRODED (ENTRY DOOR) · airframe 34,266 hrs · 21,048 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR GIRT ASSY BRACKET CORRODED AT BS 312, LBL 60. R&R BRACKET PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,266 hrs · 21,048 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM CORRODED AT BS 947.5, LBL 5 TO RBL 5. REPAIRED FLOOR BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,266 hrs · 21,048 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 312 FLOOR BEAM CORRODED, LBL 8.0 TO RBL 7.0. REPAIRED FLOOR BEAM PER T1-353-007.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 34,266 hrs · 21,048 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB CRACKED AT STR 17L, BS 560 TO BS BS 580.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,266 hrs · 21,048 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 EA. BS 178 BULKHEAD WEB CRACKS AT WL 202, RBL 7 & RBL 5. REPAIRED BULKHEAD PER SRM.

Part: WIRE — CHAFED (COCKPIT) · airframe 34,165 hrs · 20,950 cycles

DIVERTED DURING CRUISE AT FL 330, ALL IND LIGHTS ON FWD INST PANEL ILLUMINATED, ADDITIONALLY, EQUIP COOLING OFF & L/E DEVICES LIGHT - COULD NOT CLEAR. FOUND CHAFFED WIRE AT DIMMING MODULE AND REPAIRED PER MM.

Part: SKIN — DELAMINATED (AILERON TAB) · airframe 33,009 hrs · 19,929 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT AILERON TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: LENS — MISSING (CABIN) · airframe 32,913 hrs · 19,844 cycles

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

Part: SKIN — DEBONDED (LE FLAP)

DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT DISBONDED ON OUTBOARD END. REPAIRED SLAT PER SWA RA NR 1-357-0779.

Part: LENS — BROKEN (SERVICE DOORWAY)

DURING SCHEDULED TRANSITION CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED TRANSITION CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM, BS 986.5, RBL 5-BL 0. REPAIRED BEAM PER EO 99-5383.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED TRANSITION CHECK, FOUND CRACKS AT BULKHEAD WEB, BS 178, RBL 1-LBL 1, WL 188. REPAIRED BULKHEAD PER SRM.

Part: STOPS — WORN (LT, RT EMER EXIT)

DURING SCHEDULED TRANSITION CHECK, FOUND WORN STOP PADS AT LT AND RT OVERWING EMERGENCY EXIT DOORS. REMOVED AND REPLACED STOPS PER MM.