N081SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,762 hrs · 72,044 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21R. REPAIRED SKIN PER SWA EA.

Part: PCU — FAULTY (TAIL) · airframe 65,755 hrs · 72,034 cycles

AIRCRAFT WOULD NOT TRIM. REMOVED AND REPLACED RUDDER PCU PER MM.

Part: TRANSMITTER — FAULTY (NR 2 ENGINE) · airframe 65,593 hrs · 71,837 cycles

IN-FLIGHT SHUTDOWN, AIR TURNBACK, SHUT DOWN NR 2 ENGINE DUE TO OIL FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPLACED OIL FILTER AND FILTER BYPASS TRANSMITTER PER MM.

Part: SWITCH — FAULTY (NR 2 ENGINE) · airframe 65,399 hrs · 71,592 cycles

INFLIGHT SHUTDOWN, DECLARED EMERGENCY, DURING DESCENT NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPLACED OIL PRESS SWITCH PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,263 hrs · 71,420 cycles

DURING SCHEDULED C4 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED (2 EA) AT THE 12 AND 6 O'CLOCK POSITIONS RADIATING FROM RIVETS AT THE PERIPHERY OF THE DOME. REPAIRED BULKHEAD PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,263 hrs · 71,420 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR CUTOUT FRAME CRACKED AT INBD FLANGE. REPAIRED FRAME PER SWA EA.

Part: CABLE — MISROUTED (FWD SVC DOOR) · airframe 65,261 hrs · 71,417 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,036 hrs · 71,125 cycles

DURING SCHEDULED A2 CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHT INOP AT BS 727D. RELAMPED EXIT LIGHT PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,676 hrs · 70,677 cycles

DURING SCHEDULED PM CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 64,573 hrs · 70,549 cycles

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

Part: GASPER FAN — OVERTEMP (A/C COMP) · airframe 64,461 hrs · 70,408 cycles

DURING CLIMB ELECTRICAL FUMES IN COCKPIT AND CABIN. WITH GASPER AIR FAN OFF FUMES WENT AWAY. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,387 hrs · 70,319 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT WINDOW BELT CUTOUT ON LT WINDOW'S NR 21, 25, 26, 27 AND 29. REPAIRED SKIN PER SWA SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,387 hrs · 70,319 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT WINDOW BELT CUTOUT ON RT WINDOW'S NR 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 26, 27, 28, 29, 30 AND 32. REPAIRED SKIN PER SWA SI.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 64,387 hrs · 70,319 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CORRODED FROM BS 992 TO BS 1014, STR 27L. REPAIRED STR PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,387 hrs · 70,319 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27L AND 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,387 hrs · 70,319 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT WINDOW BELT CUTOUT ON LT WINDOW'S NR 1, 2, 3, 4, 5, 6, 7, 8, 9, 10 AND 11. REPAIRED SKIN PER SWA SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,360 hrs · 70,285 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445, BL O. REPAIRED SKIN PER SWA EA.

Part: LINE — LEAKING (MLG W/W) · airframe 64,336 hrs · 70,253 cycles

DECLARED EMERGENCY, HYDRAULIC SYSTEM A FAILED DURING CLIMB-OUT. REMOVED AND REPLACED SYSTEM AILERON PCU LINE PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 64,124 hrs · 69,972 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 191 AT RBL 5.7. REPAIRED WEB PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 64,124 hrs · 69,972 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 4 L/E SLAT DELAMINATED AT UPPER INBD CORNER. REPAIRED L/E SLAT PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 64,124 hrs · 69,972 cycles

DURING SCHEDULED 1/4D CHECK, FOUND T-CHORD CRACKED AT BS 178, WL 188 AT RBL 5. REPAIRED T-CHORD PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 64,124 hrs · 69,972 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,124 hrs · 69,972 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (5 EA) AT STR 2R, BS'S 1020, 1065, 1097, 1099 AND 1117.5. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,124 hrs · 69,972 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1065, STR 3R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,124 hrs · 69,972 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (5 EA) AT STR 2R, BS'S 1099, 1111, 1113, 1115 AND 1116.5. REPAIRED SKIN PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 64,124 hrs · 69,972 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB ASSY CRACKED (2 EA) AT BS 178, LBL 6.0, WL 188 AND 191. REPAIRED WEB ASSY PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,981 hrs · 69,789 cycles

DURING SCHEDULED RON, ON WALK AROUND INSPECTION FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10L, BS 670 AND BS 680. REPAIRED SKIN PER SWA RA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,981 hrs · 69,789 cycles

DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CARGO BAY) · airframe 63,560 hrs · 69,270 cycles

DURING SCHEDULED A2 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHTS INOP AT BOTH FWD CABIN DOORS. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CARGO BAY) · airframe 63,560 hrs · 69,270 cycles

DURING SCHEDULED A2 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHTS INOP AT RT OVERWING AND AFT OF RT WING. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 63,264 hrs · 68,903 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE AT ROWS 14 AND 15. SECURED EEPLS PER MM.

Part: BATTERY — DISCHARGED (CARGO BAY) · airframe 63,184 hrs · 68,811 cycles

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

Part: COVER — MISSING (CABIN) · airframe 62,541 hrs · 68,037 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER MISSING AT ROW 14. INSTALLED COVER PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 62,389 hrs · 67,863 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 62,051 hrs · 67,455 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT WING INBOARD T/E FLAP DELAMINATED AT INBOARD EDGE. REPAIRED RT WING T/E AFT FLAP PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 61,811 hrs · 67,191 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,747 hrs · 67,112 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD DOOR EMERGENCY EVAC SLIDE EXTERIOR LIGHTS INOP. REMOVED AND REPLACED EXIT LIGHT BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,712 hrs · 67,071 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD FUSELAGE EXTERIOR. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,505 hrs · 66,830 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR and FWD SVC DOOR EMERGENCY EXIT LIGHTS INOP. Removed and replaced EMERGENCY LIGHT BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,335 hrs · 66,636 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 61,119 hrs · 66,405 cycles

EEPLS LOOSE & WIRES EXPOSED AT EMERGENCY EXIT ROW. REPAIRED & RELAMPED EEPLS PER MM.

Part: STIFFENER — CRACKED (MLG WW) · airframe 61,063 hrs · 66,341 cycles

DURING SCHEDULED C2 CHECK, FOUND BS 663.5 VERTICAL STIFFENER CRACKED AT LBL 6.15. REPAIRED VERTICAL STIFFENER PER SWA RA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,881 hrs · 66,140 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD ENTRY AND SVC DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 60,805 hrs · 66,045 cycles

EEPLS DAMAGED AT ROW 14. REPAIRED EEPLS PER MM.

Part: INDICATOR — ERRATIC (COCKPIT) · airframe 60,457 hrs · 65,664 cycles

AIR TURNBACK, FLAPS WOULD NOT RETRACT FROM POSITION 5. NO C/B TRIPPED AND NO ASYMETRIC CONDITION. ALT FLAPS USED TO LAND. REMOVED AND REPLACED FLAP POSITION IND. OPS CHECK GOOD PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,404 hrs · 65,608 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT BS 580, ABOVE STR 10L. REPAIRED SKIN PER RA.

Part: LAMP SOCKET — MISSING (CABIN FLOOR) · airframe 60,302 hrs · 65,491 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS SOCKET MISSING AT MID CABIN. INSTALLED LIGHT SOCKET PER MM.

Part: COVER — LOOSE (CABIN) · airframe 59,985 hrs · 65,171 cycles

EEPLS TRACK COVER LOOSE. SECURED TRACK COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,893 hrs · 65,071 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT BS 695, STR 10L. REPAIRED SKIN PER SRM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 59,678 hrs · 64,840 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND EEPLS MISSING PIECES NEAR ROW 14. INSTALLED TRACK COVER PER MM.

Part: BATTERY — INOPERATIVE (EXTERIOR) · airframe 59,646 hrs · 64,801 cycles

DURING SCHEDULED PM CHECK, FOUND FWD EXTERIOR EVACUATION SLIDE LIGHT INOP. REMOVED AND REPLACED FWD BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (ROW 14) · airframe 59,484 hrs · 64,630 cycles

EEPLS ROW 14 INOP. REPAIRED EEPLS WIRING PER MM.

Part: LIGHT — DAMAGED (ROW 11) · airframe 59,433 hrs · 64,573 cycles

EEPLS DAMAGED AT ROW 11. REPAIRED EEPLS PER MM.

Part: COVER — CRACKED (ROW 11) · airframe 59,423 hrs · 64,563 cycles

EEPLS TRACK COVER CRACKED AT ROW 11. REPAIRED TRACK COVER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,052 hrs · 64,152 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED LBL 12 TO RBL 12. REPAIRED BULKHEAD PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,052 hrs · 64,152 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD ANGLES CRACKED RBL 24, RBL 25 AND LBL 24.5. REPAIRED ANGLES PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 58,807 hrs · 63,889 cycles

EEPLS TRACK LOOSE. SECURED TRACKS PER MM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 58,456 hrs · 63,496 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BS 663 PRESS BULKHEAD WEB CRACKED, RBL 39. REPAIRED BULKHEAD PER TI-353-032.

Part: SWITCH — ERRATIC (NR 2 ENGINE) · airframe 58,389 hrs · 63,414 cycles

IN FLIGHT ENG SHUT DOWN. NR 2 ENG OIL FILTER BY-PASS LIGHT ILLUMINATED. NO ENG VIBRATION NOTED. REMOVED AND REPLACED NR 2 ENG OIL FILTER BY-PASS SWITCH PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED D CHECK, FOUND BOTH FWD EMERGENCY EVACUATION SLIDE LIGHTS INOP. REMOVED AND REPLACED LIGHT ASSY'S PER MM.

Part: FLOORBEAM — CORRODED (BS 259)

DURING SCHEDULED D CHECK, FOUND BS 259 FLOORBEAM UPPER SURFACE CORRODED, LBL 9 TO RBL 9. REPAIRED BEAM PER SRM.

Part: CLIP — CRACKED (BS 500B)

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 500B, STRINGER 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CORRODED (BS 480)

DURING SCHEDULED D CHECK, FOUND FUSELAGE EXTERNAL SKIN CORRODED, BS 480, STRINGER 4R. REMOVED AND REPLACED SKIN PANEL BS 360-BS 520 PER ACO 6717-53.

Part: STRINGER — CRACKED (BS 727)

DURING SCHEDULED D CHECK, FOUND THROUGH HFEC INSPECTION STRINGER CHORD 18A LT CRACKED, BS 727. REPAIRED PER ACO 651-53.

Part: SKIN — CORRODED (BS 468)

DURING SCHEDULED D CHECK, FOUND FUSELAGE EXTERNAL SKIN CORRODED, BS 468, WL 148. REPAIRED SKIN PER SRM.

Part: CLIP — CRACKED (BS 663 & BS 534)

DURING SCHEDULED D CHECK, FOUND THROUGH HFEC INSPECTION 2 EACH STRINGER TIE CLIPS CRACKED, BS 663, STR 7R, AND BS 534, STR 4R. REMOVED AND REPLACED TIE CLIPS PER SRM.

Part: FRAME — CRACKED (BS 490)

DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR CUT OUT FRAME CRACKED, BS 490, WL 183-189. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (BS 360)

DURING SCHEDULED D CHECK, FOUND CRACKED SHEAR TIE, BS 360, STRINGER 14R. REPAIRED SHEAR TIE PER SRM.

Part: TRACK — CORRODED (RT TE FLAP)

DURING SCHEDULED D CHECK, FOUND RT OUTBOARD AFT FLAP INBOARD CENTER AND OUTBOARD TRACKS CORRODED. REMOVED AND REPLACED TRACKS PER OHM.

Part: SKIN — CREASED (BS 869-876)

DURING SCHEDULED D CHECK, FOUND EXTERNAL FUSELAGE SKIN CREASED FROM BS 869 TO BS 876, BETWEEN STRINGERS 24R-25R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 440)

DURING SCHEDULED D CHECK, FOUND CRACKED FUSELAGE FRAME, BS 440, WL 166 AND WL 170. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (LT TE FLAP)

DURING SCHEDULED D CHECK, FOUND LT OUTBOARD AFT FLAP DELAMINATED IN SEVERAL AREAS. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SKIN — CRACKED (CARGO DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND AFT CARGO DOOR HANDLE CUTOUT SKIN CRACKED. REPAIRED SKIN PER SWA RA NR 1-252-0336.

Part: FRAME — CRACKED (BS 500)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE FRAME CRACKED, BS 500, BETWEEN STRINGERS 20L-21L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: LIGHT — LOOSE (ROW 8)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LIGHT LOOSE AT ROW 8. RESECURED EEPLS LIGHT PER MM.

Part: COUPLING — LEAKING (RT ACM)

ABORTED TAKEOFF, RT WING BODY OVERHEAT LIGHT ILLUMINATED DURING TAKEOFF AT 78 KNOTS. FOUND COUPLING LEAKING AT COMPRESSOR SIDE OF RT AIR CYCLE MACHINE. REMOVED AND REPLACED COUPLING PER MM.

Part: SLIDE — DETACHED (SERVICE DOOR)

AFT SERVICE DOOR EVACUATION SLIDE ASSY NOT SECURED TO DOOR. REPOSITIONED SLIDE ASSY PER MM.

Part: RETRACT MECH — MALFUNCTIONED (NR 4 SLAT)

AIR TURNBACK DUE TO NR 4 SLAT WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NR 4 SLAT ACTUATOR, OPS CK AND LEAK CHECK GOOD PER BOEING MM.

Part: BRACKET — CRACKED (CARGO DOORWAY)

DURING SCHEDULED C1 CHECK, FOUND CARGO DOOR UPLATCH BRACKET INTERCOSTAL CRACKED. REMOVED AND REPLACED PER BOEING SRM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED RON CHECK, FOUND EGRESS LIGHT INOP AT LEFT WING TRAILING EDGE. CLEANED SOCKET AND RELAMPED PER BOEING MM, OPS CHECK OK.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND AFT GALLEY DOOR SKIN CRACKED AT LOWER HINGE CUTOUT LWR CORNER.

Part: BULKHEAD — DAMAGED (CABIN)

DURING SCHEDULED C4 CHECK, FOUND RT BULKHEAD (CENTER) TORN UNDER MAGAZINE POUCH. REPAIRED PER BOEING MM.

Part: SKIN — CORRODED (BS 727)

DURING SCHEDULED 1/4D CHECK, FOUND BULGING CORROSION ON FUSELAGE SKIN AT BS 727, STR 27R, 6 AFT; AND STR 27L. REPAIRED PER BOEING SRM

Part: ANGLE — BENT (FUSELAGE)

DURING SCHEDULED 1/4D CHECK, FOUND E3-4 FWD RACK ANGLE BENT. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — HOLE (BS 380)

DURING SCHEDULED 1/4 D-CHECK, FOUND WEB ABOVE BELT FRAME AT BS 380, STR 26L HAS HOLE .5 INCH CENTER. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED FWD SERVICE DOOR ANGLE BELOW FWD LOWER ATTACH FOR TORQUE BOX. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 179)

DURING SCHEDULED 1/4D CHECK, FOUND ULTRA SONIC INSP REVEALS 100 PERCENT CRACK INDICATION RBL 5.4, WL 199 UNDER STRAP. REPAIRED CRACKED WEB PER BOEING SRM.