N105SW

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 58,594 hrs · 62,840 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 58,568 hrs · 62,804 cycles

R2 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,520 hrs · 62,742 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 884, STR 24R. REPAIRED SKIN PER SRM AND SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 58,520 hrs · 62,742 cycles

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

Part: DOOR FRAME — CRACKED (L2 DOOR) · airframe 58,333 hrs · 62,494 cycles

L2 DOOR FRAME CRACKED AT FWD LOWER END. REMOVED AND REPLACED L2 DOOR PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 58,305 hrs · 62,458 cycles

DURING SCHEDULED PM CHECK, FOUND EEPLS LOOSE AT FWD END. SECURED EEPLS PER MM

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,228 hrs · 62,364 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS RED LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: GEARBOX — LEAKING (NR 1 ENGINE) · airframe 58,122 hrs · 62,229 cycles

IN FLT SHUT DOWN, DECLARED EMERGENCY NR 1 ENG OIL PRESS IND BELOW LIMITS AND OIL TEMP IND INCREASE. REMOVED AND REPLACED NR 1 ENG GEAR BOX PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 57,754 hrs · 61,760 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: INDICATOR — OUT OF POSITION (SLIDE BOTTLE) · airframe 57,704 hrs · 61,692 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 57,615 hrs · 61,578 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,585 hrs · 61,536 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR UPPER FWD CORNER. REPAIRED SKIN PER SWA EA.

Part: LIGHT — WILL NOT TEST (FWD CABIN) · airframe 57,543 hrs · 61,483 cycles

DURING SCHEDULED PM CHECK, FOUND FWD CABIN OVERHEAD EMERGENCY LIGHT BASE WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BASE PER MM.

Part: INDICATOR — OUT OF POSITION (SERVICE DOOR) · airframe 57,504 hrs · 61,436 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 60,494 hrs · 65,252 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 57,376 hrs · 61,272 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,210 hrs · 61,057 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 811, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 57,141 hrs · 60,967 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,997 hrs · 60,784 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE STRINGERS CORRODED (2 EA) BS 967 AT STR 26L AND BS 967 TO BS 977 AT STR 25L. REPAIRED STRINGERS PER SRM.

Part: SKIN — CRACKED (TAIL) · airframe 56,993 hrs · 60,779 cycles

DURING SCHEDULED C4 CHECK, FOUND 4 EA CRACKS AT LT HORIZONTAL STAB LOWER SKIN EMANATING FROM FASTENERS HOLES, BETWEEN STA 124 AND STA 173. REPAIRED SKIN PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 56,993 hrs · 60,779 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,993 hrs · 60,779 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT PAX WINDOW CUTOUT, BS 357, STRINGER 13R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (TAIL) · airframe 56,993 hrs · 60,779 cycles

DURING SCHEDULED C4 CHECK, FOUND 14 EA CRACKS AT RT HORIZONTAL STAB LOWER SKIN EMANATING FROM FASTENERS HOLES, BETWEEN STA 107 AND STA 173. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 56,595 hrs · 60,277 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 56,385 hrs · 60,008 cycles

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

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 56,368 hrs · 59,990 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,141 hrs · 59,716 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 315, STR 18R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 55,983 hrs · 59,522 cycles

AFT SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,594 hrs · 59,042 cycles

DURING SCHEDULED C2 CHECK, FOUND BS 1016 BULKHEAD CRACKED (2 EA) AT 11: 00 O'CLOCK POSITION RADIATING FROM RIVETS AT THE PERIPHERY OF THE PRESS PLUG. REPAIRED BULKHEAD PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 55,363 hrs · 58,748 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 54,942 hrs · 58,213 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,929 hrs · 58,199 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 18L. REPAIRED SKIN PER SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 54,929 hrs · 58,199 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SEVERAL SKIN CRACKS AT FWD AIRSTAIR LOWER CUTOUT BEAR STRAP. REPAIRED DOUBLER PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,929 hrs · 58,199 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SKIN CRACKED AT FWD CARGO DOOR OPENING LOWER STOP FITTING. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,929 hrs · 58,199 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 915, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,929 hrs · 58,199 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 372, STR 16L. REPAIRED SKIN PER SRM.

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 54,929 hrs · 58,199 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 54,875 hrs · 58,132 cycles

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

Part: BATTERY — DISCHARGED (CARGO BAY) · airframe 54,850 hrs · 58,098 cycles

DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY IN AFT CARGO INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,743 hrs · 57,964 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,729 hrs · 57,948 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 790, BETWEEN STR'S 18L AND 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 54,390 hrs · 57,533 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,274 hrs · 57,385 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 23L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 54,274 hrs · 57,385 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 54,040 hrs · 57,096 cycles

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

Part: BUSHING — WORN (RT ELEVATOR) · airframe 54,023 hrs · 57,075 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, FOUND RT ELEVATOR TAB BUSHINGS WORN ON ALL 4 HINGES. REMOVED AND REPLACED RT TAB BUSHINGS AT ALL HINGES PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 54,023 hrs · 57,075 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, FOUND LT ELEVATOR TAB LOCKOUT MECHANISM HAS PLAY. REMOVED AND REPLACED LOCKOUT MECH BUSHING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,644 hrs · 56,594 cycles

DURING SKIN REPAIR, FOUND BELL FRAME CRACKED AT BS 907, STR 21R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,644 hrs · 56,594 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 22R. REPAIRED SKIN PER SRM.

Part: CAP — MISSING (CABIN) · airframe 53,555 hrs · 56,482 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,488 hrs · 56,403 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED 2.50 INCHES LONG AT BS 905, STR 25R. REPAIRED SKIN PER SWA RA.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 53,443 hrs · 56,344 cycles

DURING SCHEDULED RON, FOUND AFT SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 52,894 hrs · 55,679 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 52,676 hrs · 55,431 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: UPLOCK SENSOR — FAILED (NLG) · airframe 52,641 hrs · 55,391 cycles

AFTER GEAR RETRACTION RED NOSE GEAR LIGHT STAYED ON. CYCLED GEAR, LIGHT STAYED ON WITH GEAR UP. REMOVED AND REPLACED UPLOCK SENSOR ON NLG PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 52,481 hrs · 55,212 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 52,250 hrs · 54,948 cycles

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

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED ( 2 EA ) AT BS 767 & BS 807, BETWEEN STR 8L & 9L. REPAIRED FRAMES PER BFG ER 01-0788.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL BEAM WEBS CRACKED ( 2 EA ) AT BS 178, WL 175 & WL 177, RBL 17.1. R&R WEBS PER BFG ER 01-0781.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, BETWEEN STR 8R & 9R. REPAIRED FRAME PER BFG ER 01-0788

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR FWD LOWER CORNER CUTOUT. REPAIRED SKIN PER SRM & ER 01-0796.

Part: FITTING — CRACKED (LH W/W) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D-CHECK, FOUND Lt W/W SUPPORT FITTING CRACKED AT BS 716, LBL 68 & WL 192. REPAIRED FITTING PER SRM.

Part: WEB — CORRODED (AFT CARGO) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D-CHECK, FOUND WEB CORRODED AT BS 810-823, RBL 66 & WL 199.v Removed and replaced WEB PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CRACKED AT BS 189, STR 17L, WL 207. REPAIRED CREASE BEAM PER BFG ER.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,192 cycles

DURING SCHEDULED D CHECK, FOUND STR SPLICE CRACKED AT BS 365, STR 5L. R&R STR SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 986.5, BETWEEN STR 21R & 22R. R&R SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,512 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, BETWEEN STR 8R & 9R. REPAIRED FRAME PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 663, STRINGER 10R. R&R STRINGER CLIP PER SRM.

Part: WEDGE — DELAMINATED (# 2 SLAT) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND # 2 SLAT T/E WEDGE DELAMINATED. R&R SLAT ASSY PER MM.

Part: TIE — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, LBL 25. R&R SHEAR TIE PER SRM.

Part: WEDGE — DELAMINATED (# 3 SLAT) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND # 3 SLAT T/E WEDGE DELAMINATED. R&R SLAT ASSY PER MM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED ( 2 EA ) AT STR 16L, BS 767 & BS 787. R&R STR CLIPS PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND STR CRACKED AT BS 807, STR 16L. REPAIRED STR PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIP CRACKED AT BS 616, STR 7L. R&R STR CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND STR 5R LWR CHORD CRACKED BETWEEN BS 1138-1145, . R&R STR SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 616, STR 7L. REPAIRED FRAME PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND ( 2 EA ) STR CLIPS CRACKED AT BS 747, STR 6R, & 7R. R&R STR CLIPS PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D-CHECK, FOUND HORIZONTAL CHORD CORRODED AT LWR APU AIR INLET BETWEEN BS 1167-1177. REMOVED AND REPLACED CHORD PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED AT BS 787, STR 7R, BS 807, STR 10L, BS 847, STR 4L. R&R STR CLIPS PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIP CRACKED AT BS 1138, STR 13L. R&R STR CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, BETWEEN STR 28R & 28L. REPAIRED SKIN PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED ( 7 EA ) AT BS 727A, STR'S 7R & 7L, BS 727B, STR'S 7R, 7L, 6R, 6L, BS 887, STR 4L. R&R STR CLIPS PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND ( 4 EA ) STR CLIPS CRACKED AT BS 727, STR 5R, 4R, 7L, 5L. R&R STR CLIPS PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 52,215 hrs · 54,912 cycles

DURING SCHEDULED D CHECK, FOUND STR CLIPS CRACKED ( 3 EA ) AT BS 420, STR 10L, BS 747, STR 16L, BS 520, STR 19L. R&R STR CLIPS PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 52,134 hrs · 54,823 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 52,079 hrs · 54,758 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: BEARING — WORN (LH MLG) · airframe 51,852 hrs · 54,478 cycles

DECLARED EMERGENCY……………….DURING GEAR EXTENSION FOR LANDING, THE LEFT MAIN RED LIGHT REMAINED ON & NO GREEN LIGHT. NOSE & RIGHT MAIN WERE GREEN. AFTER MANUAL GEAR EXTENSION RED LIGHT REMAINED ON.. INSTALLED LEFT MAIN GEAR DOWNLOCK PIN FOR ONE TIME FERRY FLIGHT TO HOU. R&R LH MLG FWD TRUNION BEARING PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 51,835 hrs · 54,457 cycles

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

Part: CAP — MISSING (CABIN) · airframe 51,495 hrs · 54,068 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING AT FWD END. INSTALLED END CAP PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 51,470 hrs · 54,040 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,439 hrs · 54,001 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 870, BELOW STR 24R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 51,355 hrs · 53,895 cycles

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

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 51,336 hrs · 53,877 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY OUT OF ADJUST. READJUSTED EVAC SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 51,300 hrs · 53,834 cycles

AFT DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM.

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 51,227 hrs · 53,749 cycles

AIR TURNBACK, NR 4 L/E SLAT WOULD NOT RETRACT. VISUALLY VERIFIED SLAT NOT RETRACTED. R&R SLAT ACTUATOR PER MM. OPS & LEAK CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,153 hrs · 53,653 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 312, STR 20R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 50,725 hrs · 53,219 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS LOOSE AT FWD SECTION. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,725 hrs · 53,219 cycles

DURING SCHEDULED C3 CHECK, FOUND 2.75 EXTERNAL FUSELAGE SKIN CRACK BETWEEN BS 930 & BS 936, STR 10R. REPAIRED SKIN PER SRM.

Part: SLIDE — TORN (SERVICE DOOR) · airframe 50,725 hrs · 53,219 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY TORN AT FWD END. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 50,465 hrs · 52,949 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 50,008 hrs · 52,447 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 CRACKS IN NOSE GEAR W/W FWD WEB. REPAIRED WEB PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 49,985 hrs · 52,415 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS AFT SECTION INOP. REMOVED AND REPLACED CHARGER ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 49,960 hrs · 52,388 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH AFT DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED SLIDE ASSY''S PER MM.

Part: SHUTOFF VALVE — LEAKING (TAIL SECTION) · airframe 49,953 hrs · 52,380 cycles

AIR TURNBACK, ON CLIMBOUT B-SYSTEM HYD LOW QUANTITY LIGHT ILLUMINATED FOLLOWED BY BOTH LOW PRESSURE LIGHTS. REMOVED AND REPLACED B-SYSTEM HYD RUDDER MANUAL SHUT-OFF VALVE PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 49,584 hrs · 51,989 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD EGRESS LIGHTS INOP. REMOVED AND REPLACED FWD BATTERY CHARGER (P/N 61-282-1) AND BATTERY PACK.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 49,437 hrs · 51,833 cycles

AFT SERVICE DOOR EVACUATION SLIDE LOOSE AFTER LANDING. SECURED SLIDE ASSY PER MM.

Part: ENGINE — BIRD STRIKE (NR 1) · airframe 49,347 hrs · 51,733 cycles

ABORTED TAKEOFF, AT APPROX 90 KNOTS NR 1 ENG SUFFERED BIRD STRIKE. VISUALLY INSPECTED NR 1 ENG, PERFORMED ENG RUN UP AND HIGH ENERGY STOP CHECK. NO DEFECT NOTED.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 49,271 hrs · 51,654 cycles

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

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 48,693 hrs · 50,988 cycles

AFT ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — DISCHARGED (CABIN)

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED 1/4D CHECK, FOUND FWD AND AFT EMERGENCY FLASHLIGHTS INOP AND SAFETY STRAPS MISSING. REMOVED AND REPLACED FLASHLIGHTS AND STRAP ASSY'S PER MM.

Part: SKIN — CRACKED (BS 340)

DURING SCHEDULED 1/4D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 340, STRINGER 18L. REPAIRED SKIN PER XEA X2-53-275.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE EXTERNAL SKIN AFT ENTRY DOOR UPPER HINGE CUT OUT CRACKED. REPAIRED SKIN PER SWA RA NR 1-253-2211.

Part: FRAME — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD RT CHORD CRACKED, WL 207. REPAIRED BULKHEAD CHORD PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 12. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (CARGO DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD CARGO DOOR OUTER SKIN, FWD LOWER CORNER CRACKED. REPAIRED SKIN PER SRM.

Part: LIGHT — INOP (CABIN)

FWD LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY.

Part: SENSOR — DAMAGED (NR 3 SLAT)

AIR TURNBACK, NR 3 L/E SLAT EXTEND TRANSIT LIGHT ILLUMINATED WITH SLAT RETRACTED. REMOVED AND REPLACED NR 3 SLAT PROX SENSOR.

Part: SKIN — CRACKED (BS 767)

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED, BS 767, STRINGER 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 480-515)

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED IN 3 PLACES BETWEEN BS 480-515, STRINGER 4L. REPAIRED SKIN PER SRM.

Part: HOLDER — LOOSE (SERVICE DOOR)

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR GIRT BAR HOLDERS ON SLIDE PACK LOOSE. TIGHTENED HOLDERS PER MM.

Part: SKIN — CRACKED (BS 873)

DURING SCHEDULED C1 CHECK, FOUND THRU EDDY CURRENT INSP CRACKED FUSELAGE SKIN, BS 873, STRINGER 23R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (AFT GALLEY)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP ON AFT GALLEY OVERHEAD. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SKIN — CRACKED (BS 897)

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 897, STRINGER 18R. REPAIRED SKIN PER SRM.

Part: COALESCER BAG — DIRTY (AC BAY)

DURING DESCENT PASSING APPROX 1500 FT, A STRONG SMELL WAS EVIDENT IN THE COCKPIT OF TURBO OIL. SMELL CONTINUED UNTIL SHUTDOWN AT GATE. SERVICED AIR CYCLE MACHINE AND CHANGED WATER SEPARATOR BAG, LEAK CK AND OPS CK GOOD PER M/M.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE ON BULLNOSE AT 14 LEFT. RELAMPED PER BOEING MM, OPS CHECK OK.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN DOUBLER TOP CENTER AT 178 BULKHEAD BENT & CRACKED. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 962)

DURING SCHEDULED C2 CHECK, FOUND CRACKED FUSELAGE SKIN AT 962, STR 21L. REPAIRED PER BOEING SRM.

Part: CIRCUIT BREAKERS — TRIPPED (AC POWER)

ON GROUND LOSS OF ALL AC POWER, SMELL OF SMOKE MULTIPLE CB'S TRIPPED. APU POWERING BUSSES AT TIME. REMOVED AND REPLACED C803 BREAKER AND APU GCU. RAN APU ENGINES ALL CHECK NORMAL PER BOEING MM.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED C1 CHECK, FOUND BULLNOSE EMERGENCY LIGHT ASSY LOOSE AT SEAT 9ABC. REPAIRED PER BOEING MM.

Part: SKIN — CRACKED (BS 924)

DURING SCHEDULED C4 CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 924, STR 24R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 886/930)

DURING SCHEDULED A2 CHECK, FOUND CRACKED SKIN AT BS 930, STR 23R, BS 930 STR 21R AND BS 860 STR 23R. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 930/880)

DURING SCHEDULED A2 CHECK, FOUND CRACKED SKIN AT BS 930, STR 25R, BS 880 STR 24R AND BS 880 STR 25R. REMOVED AND REPLACED PER BOEING SRM.

Part: FIRE LOOP — MALFUNCTIONED (APU)

IN FLIGHT, APU FIRE WARNING SOUNDED. PERFORMED FIRE PROCEDURES AND ACTIVATED FIRE BOTTLES. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. CONTINUED PER MEL. REMOVED AND REPLACED APU TAILPIPE FIRE DETECTOR PER BOEING M/M.

Part: ENGINE — DAMAGED (NR 1)

DURING CLIMBOUT, EXPERIENCED NR 1 ENGINE FAILURE WITH ASSOCIATIED VIBRATION AND OIL SMELL IN CABIN. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. INSPECTED AND DISCOVERED DAMAGE FROM BIRD STRIKE. REPLACED ENGINE ASSEMBLY PER BOEING M/M.

Part: SKIN — CRACKED (BS 861)

DURING SCHEDULED RON CHECK, FOUND A 2.5 FUSELAGE SKIN CRACK AT LAP JOINT AT BS 861, S25R. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 976)

DURING B1/B2 CHECK, FOUND A FUSELAGE SKIN DENT AT BS 976, BETWEEN S21 AND 22L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 970)

DURING SCHEDULED 1/2 TERM CHECK, FOUND A 3 INCH FUSELAGE SKIN CRACK AT BS 970, AT S21L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 970)

DURING WALKAROUND INSPECTION, FOUND A 3 INCH CRACK ON FUSELAGE SKIN AT BS 970, AT S21L. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (AFT PAX DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR WEB CRACKED APPROX .5 INCH. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 767)

DURING SCHEDULED C4 CHECK, FOUND A 3 INCH FUSELAGE SKIN CRACK AT S9L, FWD OF BS 767. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C4 CHECK, FOUND A .25 INCH FUSELAGE SKIN CRACK AT POTABLE WATER SERVICE PANEL, AT AFT LATCH POSITION. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 847)

DURING WALK-AROUND, FOUND A FUSELAGE SKIN CRACK AT 7 O'CLOCK POSITION, BS 847. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 847)

DURING WALKAROUND CHECK, FOUND FUSELAGE SKIN CRACK AT BS 847, AT APPROX 7 O'CLOCK POSITION. REPAIRED PER BOEING SRM.

Part: OVERHEAT WARNING — ILLUMINATED (NR 2 ENGINE)

NR 2 ENGINE OVERHEAT WARNING ILLUMINATED IN FLIGHT, CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT LANDED AT MAF WITHOUT INCIDENT. INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. DEFERRED DETECTION SYSTEM AND CONTINUED PER MEL 26-2.

Part: WINDOW — SHATTERED (L1)

CAPTAIN'S NR 1 WINDOW OUTER PANE SHATTERED ACROSS ENTIRE LENGTH. DIVERTED TO TUL AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED WINDOW ASSEMBLY PER BOEING M/M.

Part: SKIN — CRACKED (SERVICE DOOR)

DURING SCHEDULED MAINT CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED AT PREVIOUS REPAIR. REPAIRED PER BOEING SRM.

Part: BYPASS SWITCH — MALFUNCTIONED (NR 1 ENGINE)

DURING DESCENT, NUMBER 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT MADE AN UNEVENTFUL LANDING AT DAL. INSPECTED, NO CONTAMINATION NOTED. REPLACED BYPASS SWITCH, LEAK CHECKED AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE FWD SERVICE DOOR INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRYWAY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY CHARGER AND BATTERY PACK PER BOEING M/M.