N690SW

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,808 hrs · 57,925 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED CHARGER & BATTERY ASSY PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 312, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER AEM EO.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING I/B AFT FLAP LOWER SURFACED DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: GIRT BAR — DAMAGED (L1 DOOR) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BASE DAMAGED. REMOVED AND REPLACED BASE PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BASE CORRODED. REMOVED AND REPLACED BASE PER MM.

Part: LENS — DAMAGED (CABIN) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT LAV EEPLS LENS DAMAGED. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CORRODED AT BS 312, STR 28L. REPAIRED WEB PER AEM EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER AEM EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,330 hrs · 56,763 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.5. REPAIRED BEAM PER AEM EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,330 hrs · 56,783 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,330 hrs · 56,783 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,330 hrs · 56,783 cycles

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

Part: FITTING — CORRODED (GIRT BAR) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED. REPAIRED FITTING PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED. REPAIRED FITTING PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR CUTOUT WEB CRACKED AT BS 297.5, STR 17R. REMOVED AND REPLACED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 48. REPAIRED BEAM PER SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND SUPPORT BRACKET CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED BRACKET PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING FORE FLAP T/E DELAMINATED BETWEEN WBL 117 TO WBL 122. REPAIRED FORE FLAP PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 4 SLAT SKIN LOWER SURFACE CRACKED. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND WEB CRACKED AT BS 295.5, STR 8L. REMOVED AND REPLACED WEB PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND ZEE ANGLE CORRODED AT BS 297.5, STR 17R. REPAIRED ZEE ANGLE PER SRM.

Part: TAB — DELAMINATED (AILERON) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING AILERON TAB O/B CORNER DELAMINATED. REPAIRED TAB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 321, STR 20L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND FITTING CRACKED AT BS 294.5, STR 8R. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND SUPPORT ZEE ANGLE CORRODED BETWEEN BS 967 TO BS 986.5, LBL 50. REMOVED AND REPLACED SUPPORT ZEE ANGLE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,330 hrs · 56,783 cycles

DURING SCHEDULED 22Y CHECK, FOUND ANGLE CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,347 hrs · 56,040 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 864, STR 3L. REPAIRED SKIN PER EA.

Part: GASPER FAN — FAULTY (CABIN) · airframe 68,749 hrs · 55,595 cycles

FLIGHT ATTENDANT ADVISED MODERATE ACRID SMELL (HYD) IN CABIN. ODOR DISSIPATED AS FLIGHT CONTINUED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 68,587 hrs · 55,478 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,744 hrs · 54,874 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,744 hrs · 54,874 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LENS — CRAZED (EXTERIOR) · airframe 67,744 hrs · 54,874 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT LENS CRAZED. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 67,676 hrs · 54,829 cycles

FWD F/A FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: TERMINAL — LOOSE (WINDOW HEAT) · airframe 67,471 hrs · 54,687 cycles

L1 COCKPIT WINDOW ARCED. TIGHTENED L1 COCKPIT WINDOW HEAT HARNESS TERMNAL PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 66,292 hrs · 53,847 cycles

FOUND EMERGENCY EXIT FLOOR LIGHT STRIP LOOSE AT ROW 8 ABC. SECURED STRIP PER MM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 65,672 hrs · 53,379 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED FUSE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,626 hrs · 53,349 cycles

DURING SCHEDULED MV1 CHECK, AFT LT CABIN EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,928 hrs · 52,840 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,928 hrs · 52,840 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 64,895 hrs · 52,818 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LIGHT LENS PER MM.

Part: STIFFENER — CRACKED (LT WING) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING AFT SPAR UPPER CHORD INBOARD STIFFENER CRACKED. REPAIRED STIFFENER PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6R. REPAIRED WEB PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 7 TO RBL 15. REPAIRED CHORD PER ER.

Part: WEB — CORRODED (NLG W/W) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND NLG W/W CHORD CORRODED AT BS 247, RBL 16. REMOVED AND REPLACED CHORD PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 3 DOOR STOP. REMOVED AND REPLACED FRAME PER BOEING DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 400 AND BS 420, RBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: SUPPORT FITTING — CORRODED (LT WING) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT MLG WALKING BEAM SUPPORT FITTING LUG CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME UPPER CRACKED. REMOVED AND REPLACED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 360 AND BS 380, RBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 505D AND BS 525. REPAIRED BEAM PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 420 AND BS 440, LBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 19R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR OUTER SKIN CREASED. REMOVED AND REPLACED SKIN PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727A S25L) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,566 hrs · 52,563 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,523 hrs · 52,532 cycles

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

Part: GLOWSTRIP — WORN (CABIN) · airframe 64,036 hrs · 52,182 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED STRIP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,036 hrs · 52,182 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: RELAY — FAULTY (MLG) · airframe 63,836 hrs · 52,025 cycles

AIR TUNBACK, ON CLIMBOUT OF LAS NOSE GEAR UNSAFE LIGHT REMAINDED ON AFTER GEAR RETRACTION. GEAR LIGHT STAYED ON WITH HANDLE IN OFF POSITION. REMOVED AND REPLACED R374 RELAY PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 63,370 hrs · 51,671 cycles

FWD CABIN EMERGENCY EXIT SIGN MISSING LENS. INSTALLED LENS PER MM.

Part: LOGIC CARD — FAULTY (LANDING GEAR) · airframe 63,223 hrs · 51,559 cycles

RAISED LANDING GEAR LEVER ON CLIMBOUT AND HAD RED NLG INDICATION WITH NO OTHER LIGHTS ILLUMINATED. CYCLED GEAR, LIGHTS NORMAL. ADJUSTED NLG DOWNLOCK SENSOR, REMOVED AND REPLACED M983 LOGIC CARD PER MM.

Part: LENS — MISSING (CABIN) · airframe 62,986 hrs · 51,370 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 2 ABC. INSTALLED LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 62,986 hrs · 51,370 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 19L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 10L CRACKED AT BS 295. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 827, STR 17R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 500B, STR 21L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 420, STR 7L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 23L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 16L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 502D, STR 7R. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR CUTOUT FWD FRAME CRACKED AT BS 294.5. STR 10R. REPAIRED FRAME SECTION PER ER.

Part: STRINGER CLIP — CRACKED (BS 294 S11L) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SKIN — CRACKED (BS 430) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER SKIN CUTOUT BS 430, RBL 3. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 450) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER SKIN CUTOUT BS 450, BL 0. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 410) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER SKIN CUTOUT BS 410, RBL 5. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (BS 360 S9) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 9. REPAIRED FRAME SECTION PER ER.

Part: STRINGER SPLICE — CRACKED (BS 360 S16L) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 16L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT UPPER INBOARD CORNER. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 360 S15L) · airframe 60,756 hrs · 49,639 cycles

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

Part: STRINGER SPLICE — CRACKED (BS 360 S23L) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 23L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CORRODED (BS 827 S17R) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 827, STR 17R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER — CRACKED (BS 500B S21L) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 21L CRACKED AT BS 500B. REPAIRED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CRACKED (BS 360 S15R) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 360 S4L) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 807 S19L) · airframe 60,056 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 60,756 hrs · 49,639 cycles

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

Part: FRAME — CRACKED (BS 500A S9L) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 9L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 360 S13R) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8R) · airframe 60,756 hrs · 49,139 cycles

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

Part: FRAME — CRACKED (BS 500C S8R) · airframe 60,756 hrs · 49,139 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 847 S8R) · airframe 60,756 hrs · 49,139 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 373, RBL 70. REMOVED AND REPLACED CREASE BEAM CHORD SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 502D, STR 7R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 60,756 hrs · 49,639 cycles

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

Part: SHEAR TIE — CRACKED (BS 928 S21L) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 928, STR 21L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 908 S4R) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 639 S4L) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (BS 420 S7L) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 7L CRACKED AT BS 420. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 908 S4L) · airframe 60,756 hrs · 49,639 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S4L) · airframe 60,756 hrs · 49,639 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,937 hrs · 48,974 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 717, STR 10L. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 59,937 hrs · 48,974 cycles

BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 22 DEF. INSTALLED LIGHT LENS PER MM.

Part: SKIN — DELAMINATED (LT FOREFLAP) · airframe 59,351 hrs · 48,520 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING T/E INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED LT WING FOREFLAP PER MM.

Part: WEDGE — DELAMINATED (RT WING TE FLAP) · airframe 59,351 hrs · 48,520 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING T/E MID FLAP WEDGE PANEL DELAMINATED. REMOVED AND REPLACED RT WING T/E MID FLAP PER MM.

Part: SKIN — CRACKED (BS 930 S22L) · airframe 59,351 hrs · 48,520 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 22L. REPAIRED SKIN PER SRM.

Part: CABLE — MISROUTED (L1 DOOR SLIDE) · airframe 59,351 hrs · 48,520 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EMERGENCY EVAC SLIDE CABLE PER MM.

Part: SKIN — CRACKED (BS 500D S10L) · airframe 59,351 hrs · 48,520 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 13 INCHES, STR 10L. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 58,557 hrs · 47,931 cycles

DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,557 hrs · 47,931 cycles

DURING SCHEDULED A1 CHECK, FOUND CABIN EMERGENCY EXIT LIGHT INOP AT ROW 21 ABC. RELAMPED LIGHT PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 58,351 hrs · 47,778 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 58,290 hrs · 47,723 cycles

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

Part: MOTOR — INOPERATIVE (TE FLAPS) · airframe 58,176 hrs · 47,642 cycles

DECLARED EMERGENCY, T/E FLAPS WOULD NOT FULLY EXTEND. FOUND HYDRAULIC FLAP DRIVE MOTOR SEIZED. REMOVED AND REPLACED FLAP DRIVE MOTOR PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,008 hrs · 46,716 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20R. REPAIRED FRAME PER SWA EA.

Part: CABLE — BROKEN (R2 DOOR) · airframe 57,008 hrs · 46,716 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE BROKEN. REMOVED AND REPLACED CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,008 hrs · 46,716 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 4, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,008 hrs · 46,716 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 18, STR 12L. REPAIRED SKIN PER SWA EA.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 57,008 hrs · 46,716 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 7L. REPAIRED WEB PER SWA EA.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 57,008 hrs · 46,716 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT HORIZONTAL STAB ANGLE CRACKED AT STA 213, AFT SPAR UPPER CORNER. REMOVED AND REPLACED VERTICAL STIFFENER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,008 hrs · 46,716 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,008 hrs · 46,716 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727C + 5, STR 10L. REPAIRED SKIN PER SWA EA.

Part: TIRE — SEPARATED (RT MLG) · airframe 56,955 hrs · 46,659 cycles

NR 4 MAIN TIRE TREAD SEPARATED. FOUND RT MAIN FLYING AND FIXED DOORS, RT WING PANEL, RT WING INBD T/E FOREFLAP AND RT WING NR 5 GROUND SPOILER DAMAGED. REMOVED AND REPLACED NR 4 MAIN TIRE ASSY PER MM. MX FERRY TO DAL FOR REPAIRS. REMOVED AND REPLACED RT MLG WING PANEL AND FOREFLAP PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 56,569 hrs · 46,328 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 56,407 hrs · 46,188 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,164 hrs · 46,000 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 8 TO RBL 9, WL 234. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,799 hrs · 45,705 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727 D TO BS 727 E, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,799 hrs · 45,705 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 919 TO BS 922, STR 21R. REPAIRED SKIN PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 54,796 hrs · 44,918 cycles

LT OVERWING EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 & R2 DOORS) · airframe 54,440 hrs · 44,650 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 & R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 & R2 DOOR EVAC SLIDES PER MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 52,602 hrs · 43,150 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR LOWER HINGE STRAP FWD UPPER RADIUS CRACKED. REPAIRED L1 DOOR LOWER HINGE STRAP PER EA.

Part: SIGN — LOOSE (LT OVERWING) · airframe 52,602 hrs · 43,150 cycles

DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EXIT SIGN LOOSE. SECURED LT OVERWING EXIT SIGN PER MM.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 52,602 hrs · 43,150 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDES GIRT CABLES MISROUTED. REROUTED EVAC SLIDES GIRT CABLES PER MM.

Part: BOLT — BROKEN (FLAP ROLLER) · airframe 52,522 hrs · 43,079 cycles

LT WING T/E FLAPS DO NOT RETRACT TO FULL UP POSITION. REMOVED AND REPLACED LT WING T/E FT INBOARD MID FLAP ROLLER ASSY BOLT.

Part: INDICATOR — OUT OF LIMITS (SLIDE) · airframe 50,783 hrs · 41,730 cycles

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

Part: LINE — LEAKING (HYD SYSTEM) · airframe 49,228 hrs · 40,504 cycles

AIR TURNBACK, DECLARED EMERGENCY. LOST B-SYSTEM HYDRAULIC FLUID CAUSING FAILURE OF B-SYSTEM. FOUND, HYD LINE LEAKING FROM ACOUSTIC FILTER TO PRESS B-MODULE. REMOVED AND REPLACED HYD LINE FROM ACOUSTIC FILTER TO PRESS B-MODULE PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,222 hrs · 40,497 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 227 & LBL 17.1. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM.

Part: LIGHT — LOOSE (EXIT SIGN) · airframe 49,221 hrs · 40,496 cycles

DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHTS LOOSE AT ROW NR 2 DEF, ROW NR 9 DEF, ROW NR 11 ABC, ROW NR 14 ABC & ROW NR 18 ABC. SECURED OVERHEAD BIN BULLNOSE EMERGENCY EXITS LIGHTS PER MM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 49,221 hrs · 40,496 cycles

DURING SCHEDULED 1/2 D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 181, WL 230 AND RBL 17.1. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO BAY) · airframe 49,221 hrs · 40,496 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 767 PLUS 3, LBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: WEB — CRACKED (BULKHEAD) · airframe 49,221 hrs · 40,496 cycles

DURING SCHEDULED 1/2 D CHECK, FOUND VERTICAL BEAM WEBS CRACKED (2 EA) AT BS 179, WL 229 AT LBL 17.1 & WL 227 AT RBL 17.1. REMOVED AND REPLACED BOTH LT & RT WEBS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,221 hrs · 40,496 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED (3 EA) AT BS 747 AT STR 20L, BS 747 AT STR 22R, BS 867 AT STR 20R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FITTING — CORRODED (GIRT BAR ATTACH) · airframe 49,221 hrs · 40,496 cycles

DURING SCHEDULED 1/2 D CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING CORRODED. REMOVED AND REPLACED GIRT BAR ATTACH FITTING PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 48,947 hrs · 40,293 cycles

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,776 hrs · 40,168 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 953, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,049 hrs · 39,622 cycles

DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 308, STR 18R. REPAIRED SKIN PER SRM.

Part: ACTUATOR — LEAKING (LT WING) · airframe 48,000 hrs · 39,574 cycles

LEFT INBD GROUND SPOILER ACTUATOR LEAKING HYDRAULIC FLUID. REMOVED AND REPLACED LEFT INBD GROUND SPOILER ACTUATOR PER MM.

Part: BEARING — WORN (ELEVATOR) · airframe 47,862 hrs · 39,473 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR CONTROL PUSH ROD AFT BEARING PER MM.

Part: LIGHT — WORN (CABIN) · airframe 46,987 hrs · 38,737 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP WORN AT ROW NR 8. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 45,220 hrs · 27,274 cycles

AIR TURNBACK, R-1 WINDOW SHATTERED AFTER T/O. REMOVED AND REPLACED WINDOW AND HEAT CONTROL UNIT PER MM.

Part: SKIN — CRACKED (LH HORIZ STAB.) · airframe 44,299 hrs · 36,554 cycles

DURING SCHEDULED C4 CHECK, FOUND SKIN CRACKED 2 INCHES LONG ON LH HORIZONTAL STAB LOWER SURFACE, .062 INCH FROM SURFACE ROOT. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 43,450 hrs · 35,801 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 42,731 hrs · 35,154 cycles

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

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 42,665 hrs · 35,112 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRES IND OUT OF LIMITS. R&R EMERGENCY EVAC SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 42,518 hrs · 34,979 cycles

DURING SCHEDULED C2 CHECK, FOUND RT OVERWING EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 42,205 hrs · 34,720 cycles

ABORTED TAKEOFF AT 80 KTS, CAPT''S ASI INOP. REMOVED AND REPLACED MACH AIRSPEED INDICATOR PER MM, OPS CHECK GOOD.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 41,821 hrs · 34,383 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF HOLDER. REINSTALLED EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 41,733 hrs · 34,307 cycles

AFT CABIN LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: CHARGER — MALFUNCTIONED (FLASHLIGHT) · airframe 41,706 hrs · 34,283 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT CABIN LOWER EMERGENCY FLASHLIGHT WOULD NOT TURN OFF. REMOVED AND REPLACED FLASHLIGHT HOLDER PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 40,843 hrs · 33,588 cycles

DURING SCHEDULED 1/2D CHECK, FOUND KEEL BEAM CORRODED AT BS 539, RBL 8. REPAIRED KEEL BEAM PER ER 00-1198-6900U.

Part: SKIN — CRACKED (GALLEY DOOR) · airframe 40,843 hrs · 33,588 cycles

DURING SCHEDULED CHECK, FOUND FWD GALLEY DOOR SKIN CUTOUT CRACKED IN LOWER FORWARD CORNER. REPAIRED DOOR CUTOUT PER ER 00-1208.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,839 hrs · 33,587 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME CRACKED AT BS 188, WL 208, STR 17R. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CORRODED (CARGO BAY) · airframe 40,839 hrs · 33,587 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME CORRODED AT BS 867, BL 0, STR 27 R. REPAIRED FRAME PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 40,579 hrs · 33,369 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS LOOSE IN AFT GALLEY. SECURED LIGHTING PER MM.

Part: SKIN — DELAMINATED (TE FLAPS) · airframe 40,568 hrs · 33,363 cycles

DURING SCHEDULED C4 CHECK, FOUND LT AND RT WING OUTBOARD T/E FLAPS DELAMINATED AT INBOARD ENDS. REMOVED AND REPLACED CW BOTH T/E AFT FLAPS PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 40,568 hrs · 33,363 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED SLIDE ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 40,031 hrs · 32,912 cycles

FWD SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 39,638 hrs · 32,594 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH FWD ENRTY AND SERVICE DOOR EVACUATION SLIDE GIRT ASSY''S OUT OF ADJUST. REINSTALLED SLIDE ASSY''S PER MM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 39,594 hrs · 32,550 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT W/W PRESSURE WEB CRACKED, BS 663, LBL 33. REPAIRED WEB PER TI-353-046.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN CRACKED ON AFT SERVICE DOOR UPPER HINGE CUT OUT. REPAIRED SKIN PER RA NR 1-353-2234.

Part: MODULE — ERRATIC (E/E BAY)

DIVERSION, AFTER LANDING GEAR RETRACTION, NLG RED LIGHT ILLUMINATED. LANDING GEARS EXTENDED NORMAL. REMOVED AND REPLACED R374 RELAY AND LANDING GEAR LOGIC MODULE PER MM.

Part: SENSOR — INOPERATIVE (NLG)

NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. REMOVED AND REPLACED NOSE GEAR LOCK SENSOR S846 AND REMOVED AND REPLACED NOSE GEAR LOCK PROX CARDS M1215 AND M983.

Part: SEAL — LEAKING (PAX DOOR)

AIR TURNBACK, LOUD PRESSURIZATION AIR LEAK AROUND FWD ENTRY DOOR LOWER HINGE COVER PLATE AREA. REPOSITIONED FWD ENTRY DOOR LOWER HINGE SECTION OF DOOR FRAME SEAL PER MM. C/W PHASE 1 OVERWEIGHT LANDING INSPECTON. NO DEFECTS NOTED.

Part: SWITCH — OUT OF ADJUST (SPOILER HANDLE)

TAKEOFF WARNING SOUND WENT OFF PRIOR TO 80 KNOTS. RAN ENGS AND OPS CHECKED GOOD. SECOND TAKEOFF ATTEMPT, TAKEOFF WARNING SOUND WENT OFF AGAIN PRIOR TO 80 KNOTS. CLEANED AND ADJUSTED SPOILER HANDLE SWITCH ASSY, OPS CHECKED GOOD PER MM.

Part: WINDOW — CRACKED (LT COCKPIT)

DURING CRUISE 45 MIN INTO FLIGHT, L2 WINDOW HEAT BEGAN ARCING AND OUTER PANE CRACKED, INNER PANE REMAINED INTACT. AIRCRAFT RETURNED TO TPA AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED CAPT SLIDING WINDOW PER M/M.

Part: ENGINE — MALFUNCTIONED (NR 2)

ON CLIMBOUT PASSING 20,000 FT, A/C YAWED RIGHT AND GRINDING NOISE WAS FELT THROUGH CONTROLS. NR 2 N1 + N2 FLUCTUATED APPROX 5 PERCENT WITH GRINDING NOISE. POWER AT CLIMB (APPROX 90 PERCENT) EGT + FUEL FLOW NORMAL. AFT F/A REPORTED BANGING NOISE IN CABIN. NR 2 ENG PARAMETERS NORMAL ON APPROACH. FOUND EVIDENCE OF SHINGLED BLADES. INSP'D INLET, EXHAUST VBV, VSV, OIL FILTER AND CHIP DETECTORS; NO FAULTS NOTED. RAN ENG, PARAMETERS WITHIN M/M LIMITS. ENG OPS CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD RT RADIUS OF AC GROUND CONNECTION CUTOUT. REPAIRED PER BOEING SRM.

Part: SENSOR — FAILED (LT MLG)

WITH GEAR HANDLE UP, LEFT MAIN GEAR INDICATED UNSAFE (RED LIGHT). LEFT MAIN RED AND GREEN GEAR LIGHTS ILLUMINATED WITH GEAR HANDLE OFF. WITH GEAR EXTENDED ALL INDICATIONS SAFE AND OK HYD PRESS AND QTY NORMAL. REMOVED AND REPLACED LT MAIN GEAR UPLOCK SENSOR PER M/M, OPS AND ADJUSTED PER M/M.

Part: WIRE — FAILED (ROW 10-12)

DURING SCHEDULED A1 CHECK, FOUND FLOOR TRACK LIGHTS AR ROW 10-12 INOPERATIVE. REPAIRED WIRING AT ROW 10 FLOOR TRACK LIGHT PER BOEING MM.

Part: LIGHT — DETACHED (CABIN)

DURING SCHEDULED BC4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSY DETATCHED, 20 DEF. REPLACED BULLNOSE EMERGENCY EXIT LIGHT ASSY PER BOEING MM.

Part: WEB — CORRODED (BS 312-344)

DURING SCHEDULED D CHECK, FOUND CORRODED WEB AT BS 312-344, LBL 60, WL 208. RREMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (NR 5 LE SLAT)

DURING SCHEDULED D CHECK, FOUND CRACKED NR 5 SLAT LOWER SKIN AT FS 172, AFT ROW. REMOVED AND REPLACED PER DRAWING 65C30133 BOEING SRM.

Part: THRESHOLD — CORRODED (BS 303-344)

DURING SCHEDULED D CHECK, FOUND CORRODED FWD ENTRY THRESHOLD INBOARD SUPPORT ANGLE AT BS 303-344, WL 208, LBL 61. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (NR 5 LE SLAT)

DURING SCHEDULED D CHECK, FOUND CRACKED NR 5 SLAT LOWER SKIN AT WBL 167.5, AFT ROW. REMOVED AND REPLACED PER DRAWING 65C30133 BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED BS 178 BULKHEAD WEB AT WL 197 TO 201, RBL 4.7. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CHAFED (BS 867-886)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CHAFFED AT BS 867-886 BETWEEN STR 1 AND 2 LT. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 727)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 727D PLUS 6, LBL 17, WL 156. REMOVED AND REPLACED PER BOEING SRM.

Part: MOUNTING — CORRODED (BS 344)

DURING SCHEDULED D CHECK, FOUND CORRODED FWD ENTRY DOORWAY GIRT BAR MOUNTING PAD AT BS 344, WL 208, LBL 60. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR WEB — CRACKED (BS 927-947)

DURING SCHEDULED D CHECK, FOUND CRACKED SHEAR WEB UPPER ATTACH ANGLE AT BS 927 TO 947 BL0, WL 208. CRACK LOCATION AT BS 930. REMOVED AND REPLACED PER BOEING SRM.

Part: CREASE WEB — CORRODED (BS 877)

DURING SCHEDULED D-CHECK, FOUND CORRODED CREASE BEAM AT BS 877, LT 65, WL 208 AROUND FASTENER HOLE. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 727/767)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 727C LT BETWEEN STR 8 AND 9, BS 727D LT BETWEEN STR 8 AND 9 AND BS 767 LT BETWEEN 8 AND 9. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 787)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 787 LT BETWEEN STR 8 AND 9 AT A/C VENT ATTACH BRACKET FASTENER. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER CLIP — CRACKED (BS 400)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP FWD CARGO BAY AT BS 400 STR 28L. REPAIRED PER BOEING SRM.

Part: SKIN — BONDED (BS 727)

DURING SCHEDULED D-CHECK, FOUND SKIN BONDED DOUBLER DELAMINATED AT BS 727+18, STR 20 LT. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 787/807)

DURING SCHEDULED D-CHECK, FOUND WEB CRACKED BETWEEN BS 787 AND 807, STR 24L WL 161. REPAIRED PER BOEING SRM.

Part: FRAME — GOUGED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY DOOR CUTOUT AFT FRAME CLOSEOUT WEB IS GOUGED AND OIL CANNED AT BS 500, WL 156 TO 159, RBL 24 TO 28. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 358)

DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 358 RBL 63 WL 201. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 270)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND 178 BULKHEAD WEB CRACKED AT WL 196.5+0 200, LBL 4.7 AND WL 199 TO 200 LBL 6.7. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND 178 BULKHEAD WEB CRACKED AT WL 211 TO 212, RBL 6.7 AND WL 211 TO 212.5, LBL 6.7. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND 178 BULKHEAD WEB CRACKED AT WL 234 RBL 11.7 AND 12.7. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 1 LBL 1, WL 187. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED LOWER AFT CORNER OF R1 DOOR CUTOUT. REPAIRED PER BOEING SRM.

Part: STRAP — CRACKED (BS 328)

DURING SCHEDULED RON CHECK, FOUND FLOOR STABILIZING STRAP CRACKED FWD OF BS 328. REPAIRED PER BOEING SRM.

Part: SKIN — CREASE (BS 380)

DURING SCHEDULED BC3 CHECK, FOUND A FUSELAGE SKIN CREASE AT BS 380 BELOW S16. REPAIRED PER BOEING SRM.

Part: STRINGER WEB — CRACKED (FUSELAGE)

DURING SCHEDULED SERVICE CHECK, FOUND LT STRINGER 18A SHEAR BEAM WEB CRACKED, ORIGINATING FROM AFT END OF WEB TO THE MOST I/B AFT FASTENER HOLE. REPAIRED PER SWA ACO 6580-53.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND AFT UPPER EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY AND CENTER OVERHEAD EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: SENSOR — FAILED (LANDING GEAR)

AFTER TAKEOFF, LANDING GEAR POSITION LEVER WOULD NOT MOVE PAST OFF POSITION. GEAR POSITION INDICATED GEAR DOWN AND LOCKED. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. MAINTENANCE FERRIED AIRCRAFT TO PHX. REPLACED GROUND SHIFT SENSOR AND PC LOGIC CARD PER BOEING M/M.