N519SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,913 hrs · 59,494 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 62,253 hrs · 59,038 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,747 hrs · 58,694 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,439 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 927+7, STR 22L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 947+4, STR 21L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 971, STR 21L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 947+5, STR 22L. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 673.75, RBL 24.5. REPAIRED BEAM PER EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND STUB BEAM CRACKED AT BS 616, LBL 70.53. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER AFT CORNER OF UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 707, LBL 24.5. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER FWD CORNER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 360, BETWEEN STR 5R TO STR 6R. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 671, LBL 24.5. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT UPPER CORNER. REPAIRED SKIN PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND LOWER STRAP CRACKED BETWEEN BS 947 TO BS 967, BETWEEN STR 22L TO STR 27L. REMOVED AND REPLACED STRAP PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727B+5, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, FRAME CORRODED AT BS 827, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, FRAME CORRODED AT BS 482A, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, FRAME CORRODED AT BS 482A, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, FRAME CORRODED AT BS 482A, BETWEEN STR 27R TO STR 28R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, FRAME CORRODED AT BS 482A, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER SPLICE CRACKED AT BS 360, STR 6R. REMOVED AND REPLACED SPLICE PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 64,100 hrs · 58,444 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, FRAME CORRODED AT BS 482, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, LBL 3. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, RBL 3. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727A, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 947.5, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: LENS — BROKEN (CABIN) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, FWD LAV WALL EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, FWD LAVATORY WALL EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,413 hrs · 58,451 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 767, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,884 hrs · 58,093 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT CORRODED BETWEEN BS 799 TO BS 801, BETWEEN STR 22R TO STR 21R. REPAIRED SKIN PER EA.

Part: LENS — LOOSE (CABIN) · airframe 59,772 hrs · 57,289 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,638 hrs · 57,193 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 516, STR 16L. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 59,227 hrs · 56,904 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MID CABIN EMERGENCY EXIT LIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT) · airframe 59,174 hrs · 56,863 cycles

AIR TURNBACK/DECLARED EMERGENCY. SMELL OF SMOKE IN MID CABIN AND IN COCKPIT CLIMBING THROUGH FL280. SMOKE DISSIPATED AFTER GASPER AND RECIRC FAN TURNED OFF. REMOVED AND REPLACED RT FRONT WINDOW HEAT CONTROLLER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,036 hrs · 56,760 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 810, STR 20L. REPAIRED SKIN PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 58,835 hrs · 56,617 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 58,819 hrs · 56,607 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND PRESSURE DECK WEB CRACKED AT BS 664.75, RBL 43. REPAIRED WEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,716 hrs · 56,539 cycles

DURING SCHEDULED MV3 CHECK, FOUND STRINGER CRACKED AT BS 370, STR 15R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,716 hrs · 56,539 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 780, STR 19L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,716 hrs · 56,539 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 761, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,716 hrs · 56,539 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 376, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,716 hrs · 56,539 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 754, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,716 hrs · 56,539 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 770.5, STR 18L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,515 hrs · 56,400 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,515 hrs · 56,400 cycles

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

Part: LENS — MISSING (CABIN) · airframe 57,622 hrs · 55,813 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,531 hrs · 55,750 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 3. RELAMPED PER MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 57,148 hrs · 55,511 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR LOWER WEB FRAME CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 57,062 hrs · 55,458 cycles

LT FWD GALLEY EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 56,459 hrs · 55,070 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING NR 6 SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 56,460 hrs · 55,071 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER MM.

Part: STRIP — CRACKED (CABIN) · airframe 56,460 hrs · 55,071 cycles

DURING SCHEDULED 18Y CHECK, FOUND EEPLS STRIP CRACKED AT ROW 6. REPAIRED EEPLS PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 56,460 hrs · 55,071 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING NR 6 SLAT DELAMINATED. REPAIRED SLAT PER MM.

Part: SPACER — CORRODED (GIRT BAR) · airframe 56,459 hrs · 55,070 cycles

DURING SCHEDULED 18Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING SPACERS CORRODED. REMOVED AND REPLACED SPACER PER MM.

Part: SPACER — CORRODED (GIRT BAR) · airframe 56,459 hrs · 55,070 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING SPACERS CORRODED. REMOVED AND REPLACED SPACER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,459 hrs · 55,070 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,459 hrs · 55,070 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,459 hrs · 55,070 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 706, RBL 24.5. REPAIRED WEB PER AAR EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 56,459 hrs · 55,070 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING O/B FORE FLAP I/B END DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 56,459 hrs · 55,070 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 56,459 hrs · 55,070 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 56,459 hrs · 55,070 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REMOVED AND REPLACED SKIN PER SWA WA.

Part: FITTING — LOOSE (GIRT BAR) · airframe 56,459 hrs · 55,070 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT FLOOR GIRT BAR LATCH FITTING LOOSE. SECURED FITTING PER SRM.

Part: LANDING GEAR — OBSTRUCTED (LT MLG) · airframe 55,316 hrs · 54,328 cycles

AIR TURNBACK, LT MLG FAILED TO FULLY RETRACT AFTER TAKEOFF. CYCLED GEAR SEVERAL TIMES, NO HELP. GEAR GOES DOWN AND LOCKED NORMALLY. FOUND GEAR IMPACTED WITH ICE. REMOVED ICE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,778 hrs · 53,937 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EEPLS SIDEWALL LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,361 hrs · 53,565 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 259.5, BETWEEN WL 195 TO WL 160. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,361 hrs · 53,565 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 259.5, BETWEEN STR 19L TO STR 23L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,033 hrs · 53,276 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 762, STR 18L. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 53,863 hrs · 53,137 cycles

FOUND AFT EMERGENCY EXIT LENS COVER LOOSE. SECURED COVER PER MM.

Part: WIRE — CHAFED (COCKPIT) · airframe 52,601 hrs · 52,176 cycles

AIR TURNBACK/DECLARED EMERGENCY, AFTER ROTATION SMELLED SMOKE IN COCKPIT. INSPECTED AIRCRAFT FOUND WIRE BUNDLE AT P5 PANEL CHAFFED. REPAIRED WIRE CONNECTOR AT PANEL PER WDM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,193 hrs · 51,863 cycles

DURING SCHEDULED 16Y CHECK, FOUND ZEE CHORD CORRODED AT BS 270, LBL 11 TO RBL 11, WL 208. REMOVED AND REPLACED ZEE CHORD PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. FOUND BROKEN WIRE AT D2992. REPAIRED WIRE PER WDM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED FLOORBEAM PER ER AND BOEING SB.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 701, BL 0. REPAIRED FLOORBEAM PER ER AND BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 387 AND BS 454, RBL 1 AND LBL 3. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, LBL 18 TO RBL 50. REPAIRED CHORD PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,188 hrs · 51,827 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 440 TO BS 460, LBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,188 hrs · 51,827 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 15R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 460, STR 18L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 278, RBL 60. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND RIGHT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 7L CRACKED AT BS 360. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 15R CRACKED AT BS 380. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,188 hrs · 51,859 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 50,805 hrs · 50,595 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 4 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (BS 930 S25R) · airframe 49,977 hrs · 49,777 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 25R. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 49,591 hrs · 49,402 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROW 10 DEF AND ROW 12 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 6L CRACKED AT BS 727B. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 8R CRACKED AT BS 482A. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,467 hrs · 49,278 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 2L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10R. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 8R. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 5L. R&R STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S4R) · airframe 49,467 hrs · 49,278 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727B S5R) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S3L) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S1) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 520 S5R) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 482A S5L) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 520 S8R) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 616) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT RT BS 616, WL 199. REPAIRED CHORD PER SRM.

Part: FRAME — CRACKED (BS 616) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT LH BS 616, WL 199. REPAIRED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (BS 827 S10R) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S8R) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 482 S8R) · airframe 49,467 hrs · 49,278 cycles

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

Part: STRINGER CLIP — CRACKED (BS 482A S9R) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 867 S8R) · airframe 49,467 hrs · 49,278 cycles

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

Part: FRAME — CRACKED (BS 520 S8R) · airframe 49,467 hrs · 49,278 cycles

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

Part: FRAME — CRACKED (BS 440 S8R) · airframe 49,467 hrs · 49,278 cycles

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

Part: STRINGER CLIP — CRACKED (BS 520 S7L) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 520 S8L) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 482A S8R) · airframe 49,467 hrs · 49,278 cycles

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

Part: SKIN — CRACKED (BS 777 S18L) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 749 S18L) · airframe 49,467 hrs · 49,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 526 S27R) · airframe 49,446 hrs · 49,258 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT GROUND AIR CONDITIONING DOOR CUTOUT BS 526, STR 27R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 526 S27L) · airframe 49,446 hrs · 49,258 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT GROUND AIR CONDITIONING DOOR CUTOUT BS 526, STR 27L. REPAIRED SKIN PER SWA EA.

Part: ACTUATOR — LEAKING (SPOILERS) · airframe 48,500 hrs · 48,266 cycles

ON LANDING -A- HYDRAULIC SYSTEM FAILURE, ZERO PRESSURE, ZERO QUANTITY. BOTH LIGHTS ILLUMINATED. REMOVED AND REPLACED NR 8 GROUND SPOILER ACTUATOR PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,425 hrs · 48,190 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 12 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,656 hrs · 47,409 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 20L. REPAIRED FRAME SECTION PER ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 47,656 hrs · 47,409 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 47,656 hrs · 47,409 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 47,656 hrs · 47,409 cycles

DURING SCHEDULED 14Y CHECK, FOUND MID CABIN EEPLS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 47,656 hrs · 47,409 cycles

DURING SCHEDULED 14Y CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663.75, RBL 6.15, WL 172.4. REPAIRED STIFFENER PER ACO.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 47,656 hrs · 47,409 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER BOEING DRAWING AND SRM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 47,656 hrs · 47,409 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT AND LT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED FITTING PER SRM.

Part: FITTING — BROKEN (L1 DOOR GIRT BAR) · airframe 48,728 hrs · 48,534 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING BROKEN. REMOVED AND REPLACED EVAC SLIDE FITTING PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,586 hrs · 47,334 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494B, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 46,952 hrs · 46,621 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 46,944 hrs · 46,612 cycles

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

Part: SKIN — CRACKED (BS 941 S25R) · airframe 46,891 hrs · 46,550 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 25R. REPAIRED SKIN PER SWA EA AND SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 46,891 hrs · 46,550 cycles

DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 25R CRACKED AT BS 885. REPAIRED STRINGER PER SWA EA.

Part: GLOWSTRIP — WORN (CABIN) · airframe 46,659 hrs · 46,308 cycles

DURING SCHEDULED A1 CHECK, FOUND CABIN EEPLS PHOTOLUMINESCENT STRIP WORN. R&R STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,449 hrs · 45,060 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 24L. REPAIRED SKIN PER SWA EA & SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,077 hrs · 44,698 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,675 hrs · 44,268 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 924, STR 24L. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,663 hrs · 44,251 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 43,110 hrs · 42,595 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E FLAP PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 43,000 hrs · 42,491 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,694 hrs · 41,160 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 11 ABC, INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 40,523 hrs · 40,014 cycles

L1 DOOR EVAC SLIDE INADVERTENTLY PULLED FROM CASE. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 40,523 hrs · 40,014 cycles

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

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 40,512 hrs · 40,005 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 3 L/E SLAT LOWER SKIN SURFACE CRACKED 30 INCHES FROM INBD END. REPAIRED SLAT SKIN PER SRM.

Part: FRAME — CRACKED (R1 DOOR) · airframe 40,512 hrs · 40,005 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT STOP FITTINGS. REMOVED AND REPLACED R1 DOOR PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 38,683 hrs · 38,296 cycles

EEPLS LOOSE AT ROW NR 7. SECURED EEPLS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 37,076 hrs · 36,809 cycles

LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: LENS — LOOSE (MID CABIN) · airframe 37,035 hrs · 36,767 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 36,676 hrs · 36,426 cycles

DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: ACTUATOR — CRACKED (LT WING) · airframe 36,165 hrs · 35,959 cycles

AFTER LANDING DURING, TAXIING, HYD A-SYS PRESS AND QTY IND WENT TO ZERO. REMOVED AND REPLACED NR 2 SPOILER ACTUATOR PER MM.

Part: TAB — WORN (LT ELEVATOR) · airframe 34,614 hrs · 34,482 cycles

DURING SCHEDULED A1 CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: CONTROL ARM — WORN (ELEVATOR TAB) · airframe 34,614 hrs · 34,482 cycles

DURING SCHEDULED RON, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TRIM TAB CONTROL CRANK PER MM.

Part: FITTING — BROKEN (R1 DOOR) · airframe 34,074 hrs · 33,965 cycles

FWD SERVICE DOOR UPPER ATTACH CONTROL ARM FITTING BROKEN. REMOVED AND REPLACED CONTROL ARM FITTING PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,096 hrs · 33,053 cycles

DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: PROBE — LEAKING (PITOT/STATIC SYS) · airframe 32,453 hrs · 32,421 cycles

(AIR TURNBACK) FEEL DIFF PRESSURE LIGHT ILLUMINATED AFTER TAKEOFF. FOUND LT AND RT PITOT PROBES LEAKING. REMOVED AND REPLACED BOTH PITOT PROBES PER MM.

Part: FITTING — CRACKED (LH WING) · airframe 32,453 hrs · 32,421 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND LH AILERON INBD ATTACH FITTING CRACKED. R&R AILERON FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,453 hrs · 32,421 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND FUSELAGE Z-FRAME CRACKED, BS 787, STRINGER 8R. R&R Z- FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,453 hrs · 32,421 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND FUSELAGE FRAME SHEAR TIE CRACKED, BS 360, BETWEEEN STRINGERS 14R-15R. REPAIRED SHEAR TIE PER SRM.

Part: RIB — CRACKED (LH HORIZ STAB) · airframe 32,453 hrs · 32,421 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND LH HORIZ STAB L/E PANEL RIBS CRACKED ( 2 EA ) AT STA 258.3 & STA 249.1. R&R RIBS PER SRM.

Part: RIB — CRACKED (RH HORIZ STAB) · airframe 32,453 hrs · 32,421 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND RH HORIZ STAB L/E PANEL RIB CRACKED AT STA 203.1. R&R RIB PER SRM.

Part: FITTING — CORRODED (LH WING) · airframe 32,453 hrs · 32,421 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND LH MLG BEAM STABILIZER FITTING CORRODED. R&R FITTING PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 32,453 hrs · 32,421 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND STR SPLICE CRACKED AT BS 907, STR 4L. R&R STR SPLICE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 42,453 hrs · 32,421 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND STR CRACKED AT BS 907, STR 4R. REPAIRED STR PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,453 hrs · 32,421 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND MAIN FRAME 'Z' ANGLE CRACKED AT BS 380, STR 8R. REPAIRED 'Z' ANGLE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,453 hrs · 32,421 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND 'Z' FRAME ANGLES CRACKED AT STR 8L, BS 400, BS 787 & BS 907. REPAIRED ANGLES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,453 hrs · 32,424 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND FUSELAGE FRAME CRACKED ( 2 EA ) AT BS 420, BETWEEN STR 15R & STR 17R. REPAIRED FRAME PER SRM.

Part: TIE — CRACKED (FUSELAGE) · airframe 32,453 hrs · 32,421 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,453 hrs · 32,421 cycles

DURING SCHEDULED D-CHECK, FOUND STR TIE CLIP CRACKED AT BS 380, STR 10L. REMOVED AND REPLACED STR TIE CLIP PER SRM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 32,130 hrs · 32,088 cycles

EEPLS COVERS LOOSE. SECURED EEPLS COVERS PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 31,573 hrs · 31,554 cycles

EEPLS TRACK WIRES EXPOSED AT MID CABIN. RESECURED EEPLS WIRES PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 31,552 hrs · 31,535 cycles

EEPLS TRACK WIRING EXPOSED. RESECURED EEPLS WIRING PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 31,562 hrs · 31,544 cycles

EEPLS TRACK WIRING EXPOSED AT MID CABIN. SECURED EEPLS WIRING PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 31,513 hrs · 31,496 cycles

EEPLS TRACK WIRES EXPOSED. RESECURED EEPLS WIRES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,492 hrs · 31,478 cycles

DURING SCHEDULED A2 CHECK, FOUND EEPLS INOP AT FWD SECTION. RELAMPED EEPLS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 31,320 hrs · 31,317 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 30,832 hrs · 30,854 cycles

EEPLS TRACK COVER BROKEN. REMOVED AND REPLACED TRACK COVER PER MM.

Part: STIFFENER — CRACKED (AFT CARGO DOOR) · airframe 30,432 hrs · 30,458 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR LOWER FWD CORNER INTERNAL STIFFENER CRACKED. REMOVED AND REPLACED AFT CARGO DOOR (P/N 65-47952-358) (S/N 001954) PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,175 hrs · 30,192 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB .5 CRACK AT WL 190, RBL 5.7. REPAIRED BULKHEAD WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,175 hrs · 30,192 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED AT WL 207, RBL 28. R&R SIDE CHORD PER ACO 7342-53.

Part: TEE CHORD — CRACKED (FUSELAGE) · airframe 30,175 hrs · 30,192 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED AT VERTICAL T-CHORD, WL 184, LBL 5.7. REPAIRED BULKHEAD SUPPORT TEE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,673 hrs · 31,863 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA CRACKS AT BS 178 BULKHEAD BETWEEN RBL 5.0 & LBL 5.0, WL 190 - WL 201. REPAIRED BULKHEAD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,175 hrs · 30,192 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKS AT WL 210.5 RBL 6.7, WL 213 LBL 6.7 & WL 190 LBL 5.7.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 29,579 hrs · 29,588 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR RETAINER BRACKETS LOOSE ON FLOOR. SECURED GIRT BAR RETAINING BRACKETS PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 28,948 hrs · 28,955 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY. (GIRT BAR STILL HOOKED TO FLOOR). REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DISCHARGED (SERVICE DOOR) · airframe 28,831 hrs · 28,836 cycles

FWD SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR READS LOW. R & R SLIDE ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 28,762 hrs · 28,767 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 12. INSTALLED TRACK COVER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 28,762 hrs · 28,767 cycles

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

Part: INDICATOR — DISLODGED (ESCAPE SLIDE)

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT)

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

Part: SLIDE — DISLODGED (CABIN)

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REPOSITIONED SLIDE ASSY PER MM.

Part: LIGHT — DISCONNECTED (CABIN)

DURING SCHEDULED C3 CHECK, FOUND 2 MOST FWD EMERGENCY ESCAPE FLOOR TRACK LIGHTS INOP. RECONNECTED LEADS TO UNIT PER MM.

Part: LIGHT — INOPERATIVE (RT EMER EXIT)

DURING SCHEDULED C3 CHECK, FOUND RT OVERWING DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF POSITION (PASSENGER DOOR)

FWD SERVICE DOOR EVACUATION SLIDE DROPPED OUT OF HOLDER. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND 2 DOOR SKIN CRACKS COMING OUT OF THE SAME RIVET HOLE. FIRST CRACK IS .375 INCH LONG, SECOND IS .75 INCH LONG, AT LOWER AFT CORNER JUST ABOVE LOWER GATE HINGE. REPAIRED CRACK PER SRM.

Part: INTERCOSTAL — CRACKED (CARGO DOOR)

DURING SCHEDULED BC4 CHECK, FOUND AFT CARGO DOOR UP LATCH INTERCOSTAL CRACKED. REPAIRED PER BOEING SRM.

Part: SLIDE — DISLODGED (EMERGENCY EXIT)

DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT SLIDE FELL OUT OF CONTAINER WHEN OPENING FORWARD EXIT DOOR. INSTALLED SLIDE, OK PER BOEING MM.

Part: SLIDE — LOW PRESS (FWD ENTRY DOOR)

DURING WALKAROUNBD CHECK, FOUND FWD ENTRY DOOR SLIDE PRESS LOW. REPLACED PER BOEING M/M.

Part: SLIDE — LOW PRESS (ENTRY DOOR)

DURING WALKAROUND CHECK, FOUND FWD ENTRY DOOR SLIDE PRESSURE LOW. MX FERRIED TO OAK. REPLACE PER BOEING M/M.

Part: SKIN — GOUGED (CARGO DOOR)

DURING SCHEDULED B/C3 CHECK, FOUND FWD CARGO DOOR SKIN GOUGED 13 AFT OF HANDLE. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

FOUND AFT LOWER EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY PER BOEING M/M.

Part: ENGINE — BIRD STRIKE (NR 1)

DURING CLIMBOUT, EXPERIENCED BIRDSTRIKE TO NR 1 ENGINE. AIRCRAFT RETURNED TO BWI AND MADE AN UNEVENTFUL LANDING. INSPECTED AND PERFORMED BIRDSTRIKE INSPECTION, CONFIRMED BIRD ENTRY INTO ENGINE CORE. ENGINE PLACED ON 10-CYCLE FLYBACK. HOU RON BORESCOPED, NO DEFECTS NOTED.

Part: EEL BATTERY — DISCHARGED (L1 DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FORWARD ENTRY DOOR EMERGENCY EXIT SIGN LIGHT INOP. REPLACED BATTERY PACK PER BOEING MM.