N673AA

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 70,001 hrs · 60,866 cycles

RIGHT WING NR 5 L/E SLAT INBOARD END DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 69,426 hrs · 60,424 cycles

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

Part: SLAT — DELAMINATED (LT WING) · airframe 69,404 hrs · 60,407 cycles

DURING SCHEDULED C2 CHECK, FOUND LEFT WING NR 3 L/E SLAT DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 69,329 hrs · 60,344 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 69,354 hrs · 60,364 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAPS) · airframe 69,119 hrs · 60,161 cycles

DURING SCHEDULED A1 CHECK, FOUND LEFT WING OUTBOARD FORE FLAP T/E DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FRAME — CRACKED (BS 380 S15R) · airframe 69,119 hrs · 60,161 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 15R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 385 S15R) · airframe 69,119 hrs · 60,161 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 385, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 784 S20L) · airframe 69,119 hrs · 60,161 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 784, STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 534D S16L) · airframe 69,119 hrs · 60,161 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 534D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 485 S16L) · airframe 68,932 hrs · 60,011 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 506A S16L) · airframe 68,932 hrs · 60,011 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506A, STR 16L. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,923 hrs · 60,002 cycles

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

Part: SKIN — CRACKED (BS 267 S16R) · airframe 68,561 hrs · 59,724 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 267, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 68,561 hrs · 59,724 cycles

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

Part: GLOWSTRIP — WORN (CABIN) · airframe 68,495 hrs · 59,681 cycles

DURING SCHEDULED SPV CHECK, FOUND EEPLS PHOTO LUMINESCENT STRIP WORN AT ROW 23 ABC. R&R STRIP PER MM.

Part: SKIN — CRACKED (BS 759 S18R) · airframe 68,290 hrs · 59,518 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 759, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 793 S19L) · airframe 67,831 hrs · 59,148 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,609 hrs · 58,968 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 734D) · airframe 67,081 hrs · 58,555 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 734D, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 729D S19L) · airframe 67,081 hrs · 58,555 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729D, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 581 S10L) · airframe 67,081 hrs · 58,555 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 581, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 734D S20L) · airframe 66,748 hrs · 60,000 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 734D, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 728D S19L) · airframe 66,748 hrs · 60,000 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 728D, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 725 S19R) · airframe 66,617 hrs · 58,214 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 752, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,502 hrs · 58,119 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513D, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,502 hrs · 58,119 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 932 S24R) · airframe 66,437 hrs · 58,062 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 924 S24R) · airframe 66,437 hrs · 58,062 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 924, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 931 S23R) · airframe 66,437 hrs · 58,062 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 942 S23R) · airframe 66,437 hrs · 58,062 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,054 hrs · 57,761 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 496, STR 16L. REPAIRED SKIN PER SWA EA.

Part: CASTING — BROKEN (L1 DOOR ROD END) · airframe 65,974 hrs · 57,698 cycles

FWD ENTRY DOOR UPPER GATE CENTER ROD END CASTING BROKEN. REMOVED AND REPLACED UPPER GATE CASTING PER MM.

Part: GASPER FAN — FAULTY (E/E BAY) · airframe 65,962 hrs · 57,688 cycles

FAINT ELECTRICAL SMELL IN MID CABIN, TURNED OFF BOTH RECIRC AND GASPER FANS, PULLED C/B'S. SMELL DISSIPATED, PRIOR TO THIS OCCURRANCE THERE WAS LITTLE AIRFLOW THROUGH VENTS. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,623 hrs · 57,402 cycles

FUSELAGE SKIN CRACKED AT BS 845, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,437 hrs · 57,249 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 392, STR 25L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 500B) · airframe 64,272 hrs · 56,372 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SWA EA.

Part: CHANNEL — CRACKED (BS 348-360) · airframe 64,272 hrs · 56,372 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER SPLICE CHANNEL CRACKED BETWEEN BS 348 TO BS 360, STR 14L. REMOVED AND REPLACED SPLICE CHANNEL PER SRM.

Part: TAB — CRACKED (LT ELEVATOR) · airframe 64,272 hrs · 56,372 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT ELEVATOR TAB CRACKED AT NR 3 HINGE CUTOUT. REMOVED AND REPLACED TAB PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,272 hrs · 56,372 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD WEB CRACKED AT DOME CAP, 12 O'CLOCK POSITION. REPAIRED WEB PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 727A) · airframe 64,272 hrs · 56,372 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 727A, RBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (BS 578) · airframe 64,272 hrs · 56,372 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 578, STR 10R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,881 hrs · 56,071 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,631 hrs · 55,870 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 315) · airframe 63,631 hrs · 55,870 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRAKCED AT BS 315, STR 17R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 480) · airframe 63,631 hrs · 55,870 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRAKCED AT BS 480, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 452) · airframe 63,427 hrs · 55,692 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 452, STR 16L. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 62,929 hrs · 55,280 cycles

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

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 60,962 hrs · 53,749 cycles

DURING SCHEDULED C1 CHECK, FOUND 3 EACH CRACKS AT NLG W/W FWD UPPER WEB AT BS 233, BS 234, BS 238, UPPER RIVET ROW. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,962 hrs · 53,749 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 290, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,962 hrs · 53,749 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 500D + 3, ABOVE STRINGER 12R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,038 hrs · 53,000 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,879 hrs · 52,876 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 59,541 hrs · 52,582 cycles

FWD OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,451 hrs · 52,571 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 517, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 59,158 hrs · 52,272 cycles

L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,101 hrs · 52,222 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 807, STRINGER 19L, BS 957, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM AND EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 59,092 hrs · 52,214 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 59,092 hrs · 52,214 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR FRAME UPPER HINGE CUTOUT LOWER RADIUS, CRACKED. REPAIRED FRAME HINGE CUTOUT PER EA.

Part: LENS — BROKEN (CABIN) · airframe 58,383 hrs · 51,631 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,207 hrs · 51,485 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN AT BS 767, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOOR) · airframe 58,071 hrs · 51,378 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,827 hrs · 51,192 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT NLG WHEEL WELL BS 245.5, BELOW LT PRESSURE PANEL. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,667 hrs · 51,062 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACK AT BS 807. REPAIRED SKIN PER SRM.

Part: RETAINER — BROKEN (CABIN) · airframe 56,809 hrs · 50,374 cycles

FWD EMERGENCY FLASHLIGHT BASE ASSY BROKEN. REMOVED AND REPLACED BASE ASSY PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, BETWEEN STR 22R AND STR 23R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8L AND STR 9L, BS'S 827, 867, 887 AND 907. REPAIRED FRAMES PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CRACKED AT BS 947.5, WL 208 AND LBL 53. REPAIRED FLOORBEAM PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND LT KEEL BEAM CORRODED AT BS 500C, WL146 AND LBL 6. REPAIRED KEEL BEAM PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 1003, STR 21L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKRD (2 EA) AT BS 500, WL 148 AT RBL 8 AND BS 827, WL 148 AT RBL 3. REPAIRED FRAMES PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 767, WL 148 AND RBL 8. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, WL 148 AND LBL 3. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND RT HORIZ STAB HINGE FITTING LOWER AND UPPER LUGS CORRODED. REPAIRED LUGS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND KEELBEAM CORRODED BETWEEN BS 500D + 2 AND BS 500D + 6, WL 147 AND RBL 7. REPAIRED KEEL BEAM PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIES CRACKED (2 EA) AT BS 360 BETWEEN STR 14R AND STR 15R, BS 400 BETWEEN STR 13L AND STR 14L. REPAIRED SHEAR TIES PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 827, WL 148 AT LBL 17. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L AND STR 14L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, WL 208 AND LBL 17 TO RBL 12. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 787, WL 148 AND RBL 9. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM CORRODED AT BS 638, BS 907 AND BS 946. REPAIRED CREASE BEAM PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 1011, STR 7L. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND RT BS 188 CHORD CRACKED AT WL 207. REMOVED AND REPLACED CHORD PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 907, STR 4R AND STR 4L. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,162 hrs · 49,823 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,159 hrs · 49,822 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 495, ABOVE STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,159 hrs · 49,822 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, ABOVE STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,209 hrs · 49,083 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT BS 518 @ STR 19R, BS 800 @ STR 21L & BS 942 @ STR 25R. REPAIRED SKIN PER SRM.

Part: CASTING — CRACKED (SPOILER) · airframe 54,990 hrs · 48,910 cycles

FLT ATTENDANT REPORTS LOUD HUM AND VIBRATION LT SIDE OF CABIN FROM ROWS NR 6 THROUGH ROW NR 17. REMOVED AND REPLACED NR 4 GROUND SPOILER PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 54,486 hrs · 48,521 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN OPENING DOOR. REMOVED AND REPLACED SLIDE PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,313 hrs · 48,384 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 222 AND LBL 2 TO LBL 3. REPAIRED BULKHEAD WEB PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,276 hrs · 48,351 cycles

DURING SCHEDULED C2 CHECK, FOUND A 3.5 FUSELAGE SKIN CRACK, BS 807, STRINGER 19L. REPAIRED SKIN PER SRM.

Part: CABLE — MISROUTED (L2 DOOR) · airframe 54,276 hrs · 48,351 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE CABLE MISROUTED. REROUTED SLIDE CABLE PER MM.

Part: BUSHING — WORN (LT ELEV) · airframe 54,276 hrs · 48,351 cycles

DURING SCHEDULED C2 CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR CONTROL ROD END BUSHING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,417 hrs · 47,641 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 487, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,417 hrs · 47,641 cycles

DURING SCHEDULED SERVICE CHECK, FOUND SKIN CRACKED ON BOTH CAPTAIN'S AND FIRST OFFICER'S WINDOW POSTS. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,417 hrs · 47,641 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 12L, BS 500D + 2 AND BS 500D + 18. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,417 hrs · 47,641 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) ABOVE STR 10L, BS 500D + 16, BS 500A + 12, BS 500C + 5 AND BS 500A + 2. REPAIRED SKIN PER SWA EA AND SRM.

Part: STUD — LOOSE (LAVATORY) · airframe 53,410 hrs · 47,635 cycles

AFTER DEPARTURE AN ELECTRICAL FUME WAS NOTICED, CABIN CREW CONFIRMED FUME. NO CB'S TRIPPED, AC AND DC LOADS ALL NORMAL. FUMES DIMMISHED BUT NOT ELIMINATED. FOUND BLUE FLUID FROM FWD LAV LEAKING AT PRESS FILL. FOUND LOWER ENTRY LIGHT SHORTED OUT DUE TO LAV SPRAY. REMOVED AND REPLACED BULB PER MM. FOUND FWD LAV PRESS FILL ATTACHMENT STUDS ON TANK LOOSE. REMOVED AND REPLACED FWD LAV PRESS FILL ATTACHMENT SEAL AND TIGHTENED STUDS PER MM

Part: BUSHING — WORN (LT ELEVATOR) · airframe 52,627 hrs · 47,008 cycles

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

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 52,561 hrs · 46,949 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,503 hrs · 46,894 cycles

DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,356 hrs · 46,774 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 5, ABOVE STR 15R. REPAIRED SKIN PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 51,041 hrs · 45,668 cycles

AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: LENS — OBSTRUCTED (FWD CABIN) · airframe 50,536 hrs · 45,272 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS OBSTRUCTED AFT OF L1 DOOR. CLEANED LENS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 50,409 hrs · 45,175 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 50,400 hrs · 45,167 cycles

FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: STIFFENER — CRACKED (MAIN WHEEL WELL) · airframe 49,632 hrs · 44,498 cycles

DURING SCHEDULED 1/4D CHECK, FOUND MLG WHEEL WELL BULKHEAD VERTICAL STIFFENER CRACKED AT BS 663, RBL 6.5. REPAIRED STIFFENER PER SWA RA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,632 hrs · 44,498 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178, LBL 5.7 & WL 184. REPAIRED CHORD PER SRM.

Part: WIRE ROPE — FRAYED (EVAC SLIDE) · airframe 49,632 hrs · 44,498 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE FRAYED AND MISROUTED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 49,632 hrs · 44,498 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERWING EMERGENCY EXIT SIGN LOOSE AT LT CABIN INTERIOR. SECURED EXIT SIGN PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,632 hrs · 44,498 cycles

DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED AT BS 178, LBL 11.0, WL 218. REPAIRED WEB PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 49,632 hrs · 44,498 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED AT BS 520, STR 28L. REPAIRED KEEL BEAM PER SWA RA.

Part: WEB — CRACKED (RH MLG W/W) · airframe 49,632 hrs · 44,498 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 665, RBL 38. REPAIRED WEB PER SWA TI.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,632 hrs · 44,498 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1, WL 180. REPAIRED WEB PER SWA RA.

Part: UPLOCK SENSOR — OUT OF ADJ (RT MLG) · airframe 49,019 hrs · 43,979 cycles

AIR TURNBACK, RT GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR HANDLE IN THE OFF POSITION. ADJUSTED RT GEAR UPLOCK SENSOR PER MM.

Part: SENSOR — MALFUNCTIONED (RT WING PYLON) · airframe 48,054 hrs · 43,195 cycles

DIVERSION, AT FL370, LOST PNEU BLEED PRESS DURING DESCENT, BLEED TRIP OFF LIGHT ILLUMINATED. BOTH DUCT PRESS INDICATORS SHOWED APPROX 65 - 75 PSI. COULD NOT DUPLICATE PROBLEM. PERFORMED PRESS DECAY CHECK, PRESS CONTROL CHECK AND BLEED AIR OPS CHECK OK PER MM. FOR MX CONVENIENCE, REMOVED AND REPLACED NR 2 POS 390 SENSOR (P/N 12966-2) & 450 SENSOR.

Part: SLIDE — UNSECURE (AFT PAX DOOR) · airframe 47,501 hrs · 47,270 cycles

AFT ENTRY DOOR SLIDE GIRT BAR STRAP NOT SECURE. SECURED PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 46,895 hrs · 42,212 cycles

DURING SCHEDULED RON, FOUND EEPLS BROKEN/LOOSE AT MID CABIN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 46,868 hrs · 42,189 cycles

EEPLS LOOSE AT OVERWING EXIT. SECURED LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,595 hrs · 41,960 cycles

THREE EEPLS INOP. RELAMPED AND REMOVED AND REPLACED TRACK COVER PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 46,294 hrs · 41,699 cycles

FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUSTMENT. REINSTALLED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,838 hrs · 41,305 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN HAS A 3 INCH LONG CRACK, BS 942, STRINGER 25R. REPAIRED SKIN PER SRM.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 45,566 hrs · 41,058 cycles

ABORTED TAKEOFF, NR 2 ENG N1 INDICATOR INOP DURING TAKEOFF AT 25 KNTS. REMOVED AND REPLACED NR 2 ENG N1 INDICATOR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,414 hrs · 40,933 cycles

EEPLS LIGHT INOP AT OVERWING EXIT. R&R LIGHT ASSY PER MM.

Part: BATTERY — INOPERATIVE (ROW 18)

DURING SCHEDULED C4 CHECK, FOUND OVERHEAD EMERGENCY LIGHT INOP AT ROW 18. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP ON AFT END. REMOVED AND REPLACED LIGHT BULB AND COVER ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS INOP BY OVERWING EXIT. RELAMPED PER MM..

Part: LENS — MISSING (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EEPLS LENS MISSING AT MID CABIN. REPLACED LENS ASSY PER MM.

Part: SLIDE — LOW PRESS (SERVICE DOOR)

FWD SERVICE DOOR EVACUATION SLIDE PRESS OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LENS — BROKEN (LT&RT EMER EXIT)

DURING SCHEDULED C2 CHECK, FOUND LT AND RT OVERWING EMERGENCIY EXIT SIGN LENSES BROKEN. REMOVED AND REPLACED BOTH LENSES PER MM.

Part: FAN — FAILED (AC BAY)

DURING SCHEDULED 1/2D CHECK, NOTED A SMOKE SMELL WITH RECIRCULATING FAN RUNNING. REMOVED AND REPLACED FAN PER BOEING MM.

Part: FLOORBEAM — CORRODED (BS 727)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED UNDER STRAP AT BS 727D + 6, LBL 17. REPAIRED PER SWA RA 1-353-1979.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND A 1.5 INCH CRACK AT AFT LOWER CORNER OF FWD SERVICE DOOR. REPAIRED PER SWA RA 1-353-1970.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND A CRACK IN WEB AT BS 178, RBL 1.0. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 802)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 802, RBL 14. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 4.5. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 360)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CRACKED AT BS 360, AT S11L. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: STRINGER — CRACKED (BS 360)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CRACKED AT BS 360, AT S15L. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND LT CHORD CRACKED AT BS 178, LBL 29. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 940-947)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 940 TO 947, LBL 17. CUT OUT AND SPLICED IN REPAIR PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 727D+6, LBL 3 AND 8. REPAIRED PER SWA RA 1-353-1972.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACK AT LBL 10 AND RBL 10, WL 234. REPAIRED PER BOEING SRM.

Part: FRAME — GOUGED (BS 700)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME GOUGED AT BS 700, AT LBL 60. REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 7.0. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CORRODED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND NUMEROUS CRACK LOCATIONS IN WEB AT BS 178. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 1016)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT FWD FLANGE LOWER SURFACE, BS 1016. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5. REPLACED T-CHORD PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT FASTENER HOLE AND UPPER CHORD, BS 312. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 663)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 663, AT S10L AND R. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED NEAR Z ANGLE AT AFT ENTRY DOOR. REPLACED T CHORD PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED UNDER STRAP AT BS 727D PLUS 6 RBL 8 AND LBL 13. REPAIRED PER SWA RA 1-353-1972.

Part: STRINGER — CORRODED (FUSELAGE)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 26R AT AFT GALLEY CORRODED. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: PIN — UNSECURED (PAX DOOR)

LOUD NOISE FROM FWD ENTRY DOOR AFTER TAKEOFF. AIRCRAFT RETURNED TO BWI, FOUND HINGE PIN OUT AT UPPER HINGE COVER. RESECURED COVER.

Part: WIRE — FAILED (ROW 1-8)

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY TRACK LIGHTS INOP FROM ROWS 1 TO 8. REPLACED TRACK WIRE AND OP CHECKED PER BOEING M/M.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED C3 CHECK, FOUND SEVERAL LIGHTS INOPERATIVE ON AFT END OF EMERGENCY LIGHTS STRIP. RELAMPED LIGHTS AT END OF STRAP PER BOEING MM.

Part: ACTUATOR — FAILED (LT MLG)

ON CLIMB-OUT AFTER GEAR RETRACTION, LEFT MAIN GEAR EXTENDED WITH HANDLE IN UP POSITION. REPLACED LEFT MAIN GEAR UPLOCK ACTUATOR PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND 1 SECTION OF EMERGENCY TRACK LIGHTING INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: STRAP — CRACKED (AFT ENTRY)

DURING SCHEDULED C3 CHECK, FOUND STRAP BY AFT ENTRY DOOR CRACKED 1.25 INCH THROUGH LOCK. REPAIRED PER BOEING SRM.

Part: SLIDE — LOW PRESS (FWD SERV DOOR)

DURING SERVICE CHECK, FOUND R2 DOOR SLIDE PRESSURE LOW. REPLACED PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING C2 CHECK, FOUND ONE RED FLOOR TRACK LIGHT INOP. REPLACED PER BOEING M/M.

Part: LIGHT — LOOSE (CABIN)

DURING RON CHECK, FOUND FLOOR TRACK LIGHT LOOSE FROM FLOOR AT ROW 1. REINSTALLED PER BOEING SRM.

Part: RELAY — FAILED (E/E COMPT)

RETURNED TO MCI DUE TO NUMBER 1 TRANSFER C/B TRIPPING IN FLIGHT. REPLACED R3 RELAY AND OP CHECKED PER BOEING M/M.

Part: SKIN — DENTED (BS 194)

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN DENTED 6 INCHES ABOVE STRINGER 24 AT FRAME, BS 194. REPAIRED PER BOEING SRM.

Part: SKIN — BIRD STRIKE (NOSE)

AFTER TAKEOFF, LARGE BIRD OR BIRDS HIT NEAR LEFT NOSE WHEEL WELL. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND SLIGHT EVIDENCE OF STRIKE TO NOSE LEFT SIDE, WITHIN BOEING SRM AND NUMBER 1 ENGINE. BORESCOPED AND PERFORMED ENGINE RUN-UP, WITH NO DAMAGE NOTED.

Part: TRANSMITTER — FAILED (RT TE FLAPS)

ON CLIMBOUT, FLAPS WOULD NOT RETRACT PAST 2 UNITS, SPILT INDICATION. AIRCRAFT DIVERTED TO OAK AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED RT FLAP POSITION TRANSMITTER AND OP CHECKED PER BOEING M/M.

Part: SHEAR TIE — CORRODED (BS 927)

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN S27R AND S27L. REPAIRED PER BOEING SRM.

Part: DOOR WARNING — MALFUNCTIONED (FWD ENTRY)

ABORTED TAKEOFF DUE TO MASTER CAUTION INDICATING FWD ENTRY DOOR OPEN. RETURNED TO GATE. INSPECTED AND FOUND DOOR SECURED AND LOCKED. PLACED DOOR WARNING ON MEL 52-2. INSPECTED TIRES/BRAKES AND CONTINUED PER BOEING M/M.