N104SW

Part: SPACER — WORN (NR 1 ENGINE) · airframe 61,016 hrs · 65,925 cycles

NR 1 ENGINE THROTTLE BINDING AT ABOUT HALF-WAY. REMOVED AND REPLACED SPACER BETWEEN TWO CONTROL CABLES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,494 hrs · 65,252 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 18R. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,438 hrs · 65,179 cycles

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

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 59,673 hrs · 64,210 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS SECTION INOP IN AFT CABIN. RELAMPED EEPLS PER MM.

Part: CABLE — MISROUTED (AFT ECAPE SLIDE) · airframe 59,673 hrs · 64,210 cycles

DURING SCHEDULED C 2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — OUT OF POSITION (AFT SVC DOOR) · airframe 59,535 hrs · 64,039 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,167 hrs · 63,591 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,932 hrs · 63,303 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 930 AND BS 933, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,924 hrs · 63,294 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21R. REPAIRED SKIN PER SRM.

Part: RETAINER — LOOSE (AFT ENTRY DOOR) · airframe 58,834 hrs · 63,184 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER LOOSE. SECURED RETAINER PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 58,834 hrs · 63,184 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CORRODED, BS 907 STRINGER 26L. REPAIRED STRINGER SECTION PER SRM

Part: AILERON — DELAMINATED (LT WING) · airframe 58,829 hrs · 63,177 cycles

DURING WALK AROUND INSPECTION, FOUND LT AILERON DELAMINATED AT OUTER EDGE ON BOTH UPPER AND LOWER SURFACE. REMOVED AND REPLACED LT AILERON PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,210 hrs · 62,389 cycles

DURING SCHEDULED C4 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED (12 EA) ON WEBS THAT CONVERGE AT THE CENTER OF THE PRESS DOME AND RADIATE OUT IN ALL DIRECTIONS. MX FERRY TO PAE. REPAIRED BULKHEAD PER BFG ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,210 hrs · 62,389 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 1016 PRESS BULKHEAD CRACKED (12 EA) ON WEBS THAT CONVERGE AT THE CENTER OF THE PRESS DOME. REPAIRED BULKHEAD PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,138 hrs · 62,300 cycles

DURING SCHEDULED SERVICE CHECK, FOUND SKIN AND TEAR STRAP CRACKED AT AIR STAIR AFT LOWER CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 57,998 hrs · 62,126 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 57,605 hrs · 61,637 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 57,486 hrs · 61,486 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,467 hrs · 61,461 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 57,450 hrs · 61,438 cycles

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

Part: AILERON — DELAMINATED (RT WING) · airframe 57,310 hrs · 61,271 cycles

DURING WALK AROUND INSPECTION, FOUND RT AILERON DELAMINATED ON BOTTOM CENTER. REMOVED AND REPLACED AILERON PER MM..

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 57,195 hrs · 61,122 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 56,815 hrs · 60,649 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,563 hrs · 60,335 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED (2 EA) AT STR 14R, BS'S 340 AND 360. REPAIRED SHEAR TIE PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,563 hrs · 60,335 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,553 hrs · 60,335 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 11L, BS 767 AND 787. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 56,563 hrs · 60,335 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL CHORD CRACKED AT BS 178, WL 184 AND RBL 5.7. REPAIRED CHORD PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 56,563 hrs · 60,335 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY FLASHLIGHTS INOP IN AFT CABIN. REMOVED AND REPLACED FLASHLIGHTS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,559 hrs · 60,334 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED BETWEEN BS BS 616 AND BS 639, STR 4L. REPAIRED SKIN PER SWA RA.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 56,442 hrs · 60,194 cycles

EMERGENCY FLASHLIGHT INOP AFT CABIN TOP UNIT. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: LIGHT — LOOSE (AFT ENTRY DOOR) · airframe 56,064 hrs · 59,732 cycles

AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,518 hrs · 59,114 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,501 hrs · 59,094 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 1 1/2 LONG AT BS 430, STR 10R. REPAIRED SKIN PER SWA RA .

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 55,488 hrs · 59,079 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 55,219 hrs · 58,757 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,170 hrs · 68,694 cycles

DURING RON FOUND FUSE SKIN CRACKED AT BS 500, STR 10R. REPAIRED SKIN PER SWA RA.

Part: CAP — MISSING (CABIN) · airframe 54,747 hrs · 58,200 cycles

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

Part: LIGHT — INOPERATIVE (ENTRY DOOR) · airframe 54,643 hrs · 58,082 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY LIGHT INOP. R&R EMERGENCY LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 54,592 hrs · 58,019 cycles

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

Part: FITTING — CORRODED (LT WING) · airframe 55,150 hrs · 58,468 cycles

DURING SCHEDULED D-CHECK, FOUND LT MLG AFT STABILIZER BEAM FITTING CORRODED. REMOVED AND REPLACED BEAM FITTING PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 54,207 hrs · 57,624 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 53,914 hrs · 57,305 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 53,357 hrs · 56,726 cycles

FWD EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 53,340 hrs · 56,706 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 53,268 hrs · 56,626 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT BATTERY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 53,136 hrs · 56,483 cycles

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

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 52,633 hrs · 55,914 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 52,557 hrs · 55,828 cycles

OVERHEAD CENTER EMERGENCY EXIT LIGHT ASSY LOOSE. REINSTALLED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (EXTERNAL EEL) · airframe 52,288 hrs · 55,515 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EXTERNAL EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: FITTING — CORRODED (LT MLG) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D CHECK, FOUND LT MLG FITTING CORRODED AT TWO FASTENER HOLES, BS 706 STRINGER 18A L. REPAIRED FITTING PER ER NR 00-0667.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D CHECK, FOUND BS 663 FRAME CRACKED AT STRINGERS 1, 2L, 2R, 3L AND 3R. REPAIRED FRAME PER SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE INTERNAL DOUBLER CORRODED, BS 986, BETWEEN STRINGERS 27L - 27R. REPAIRED DOUBLER PER ER NR 00-0602.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB HINGE HOUSING LOWER INBD AND OUTBD LUGS CORRODED. REPAIRED LUGS PER ER 00-0590.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER 8 RT CRACKED AT BS 334. REPAIRED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 727B, LBL 6 TO RBL 6. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED, BS 986.5, STRINGER 26R TO STRINGER 27R. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION AT STRINGER 26R, BS 1016 TO BS 1006. REPAIRED STRINGER SECTION PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO BIN DOOR CUTOUT AFT FUSELAGE FRAME CORRODED, STRINGER 25R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED, BS 990, RBL 55, WL 210. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE FRAME CORRODED, BS 278, STRINGER 26R-28R. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 28R CRACKED, BS 460. REPAIRED STRINGER PER SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND BULKHEAD STIFFENER CORRODED BS 1016, WL 191. REPAIRED STIFFENER SECTION PER SRM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND COCKPIT WINDOW POST CRACKED BETWEEN NR 1 AND NR 2 WINDOWS. REPAIRED WINDOW POST PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED, BS 907, STRINGER 4L. REMOVED AND REPLACED SPLICE SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED BS 747, STR 5L, 5R, 6L, 7L, 7R, BS 787, STR 4R, 5R, 10L, BS 827, STR 10R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED, BS 360, STR 11L, BS 380, STR 5R, BS 400, STR 9L, AND BS 420, STR 7R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND BS 188 LT AND RT SIDE CHORDS CRACKED AT WL 208. REMOVED AND REPLACED SIDE CHORDS PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 5L CRACKED, BS 1138 - 1142. REPAIRED STRINGER SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 14L CRACKED, BS 360. REPAIRED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 27L CORRODED, BS 376. REPAIRED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED, BS 947 BETWEEN STRINGERS 26L-27L. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED, BS 380 STRINGER 26L. REMOVED AND REPLACED STRINGER CLIP PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 24R CORRODED, BS 494. REPAIRED STRINGER SECTION PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 STIFFENER CRACKED WL 178, RBL 24. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND BS 360 FLOORBEAM UPPER SURFACE CORRODED, LBL 33 TO RBL 33. REPAIRED BEAM PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 52,112 hrs · 55,310 cycles

DURING SCHEDULED D-CHECK, FOUND AFT ENTRY DOOR EXTERNAL EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUSTMENT. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: CAP — MISSING (LIGHT)

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

Part: LINE — LEAKING (NR 2 ENGINE)

INFLIGHT ENGINE SHUTDOWN, NR 2 ENG FLAMED OUT DURING DESCENT. FOUND P/D FUEL LINE LEAKING. ENGINE WOULD NOT RESTART. REMOVED AND REPLACED NR 2 ENG P/D TO OIL COOLER FUEL LINE..

Part: FLASHLIGHT — INOP (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

EEPLS ILLUMINATED WITH SWITCH IN ARMED POSITION. REMOVED AND REPLACED FWD OVERHEAD BATTERY PACK PER MM.

Part: SKIN — CRACKED (NR 4 LE SLAT)

DURING SCHEDULED C4 CHECK, FOUND NR 4 LE SLAT HAS A .25 INCH LONG CRACK AT INBD AUX TRACK CUT OUT. REPAIRED SLAT PER SWA RA NR 1-257-0703.

Part: SKIN — CRACKED (SERVICE DOOR)

DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR SKIN HAS 1 INCH LONG CRACK AT LOWER HINGE ARM CUT OUT. REPAIRED SKIN PER SRM.

Part: COVER — MISSING (EMERGENCY EXIT)

EMERGENCY EXIT LENS COVERS, RIGHT HAND AND LEFT HAND OVERWING EXITS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WEB — CRACKED (BS 180)

DURING SCHEDULED 1/4D CHECK, FOUND HORIZONTAL WEB CRACKED AT BS 180, RBL 26. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND FUSE SKIN CRACKED AT AFT ENTRY DOOR UPPER CUTOUT, 2 PLACES. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (CARGO DOOR)

DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR T CHORD CRACKED AT FWD STOP CASTING AND 2ND FROM BOTTOM. REMOVED AND REPLACED DOOR PER BOEING M/M.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD SKIN CRACKED AT LBL AND RBL 12. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 310)

DURING SCHEDULED C2 CHECK, FOUND A 1 INCH FUSELAGE SKIN CRACK AT BS 310 FWD OF FWD ENTRY DOOR GUIDE ARM. REPAIRED PER BOEING SRM.

Part: SLIDE — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND AFT ENTRY ESCAPE SLIDE GAUGE UNABLE TO READ. REMOVED AND REPLACED SLIDE PACK PER BOEING MM. PRESS READ NORMAL.

Part: SKIN — CRACKED (BS 767)

DURING SCHEDULED SERVICE CHECK, FOUND SKIN CRACKED AT BS 767 RT SIDE 5 INCHES BELOW WHITE STRIPE. REMOVED AND REPLACED PER BOEING MM.

Part: ENGINE — OIL LEAK (NR 1)

AFTER GEAR RETRACTION, EXPERIENCED NR 1 ENGINE OIL AND PRESSURE LOSS. RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. FOUND OIL FILTER HOUSING CAP STUDS PULLED. REMOVED AND REPLACED ENGINE PER BOEING M/M.

Part: BOLT — FRACTURED (NR 2 ENGINE)

DURING A NR 2 ENGINE CHANGE ON 05SEP97, IT WAS DISCOVERED THAT THE FWD I/B MOUNT ATTACH BOLT WAS FRACTURED. THE FRACTURE OCCURED IN THE THREADED AREA. FRACTURE PIECES AND NUT WERE FORWARDED TO BOEING SERVICE ENGINEERING. THE LAST ENGINE CHANGE OCCURED IN DEC 1994. IT APPEARS THE BOLT AND NUT WERE ORIGINAL INSTALLATION SINCE INSPECTION PUTTY WAS PRESENT. IN NOV 1996, DUE TO FINDINGS ON OTHER A/C, NUT TORQUE WAS CHECKED AND CONFIRMED TO BE OVER 900 IN-LBS. THE TORQUE ON THE NR 1 ENGINE WAS FOUND BELOW 200 IN-LBS AND WAS THEREFORE REPLACED.

Part: WHEEL — BROKEN (NR 1)

ON LANDING, A SECTION OF NUMBER 1 MAIN WHEEL HUB SEPARATED FROM MAIN ASSEMBLY, CAUSING MINOR DAMAGE TO NUMBER 1 MAIN BRAKE PRESSURE LINE. INSPECTED AREA, REMOVED AND REPLACED NUMBER 1 AND 2 MAIN WHEEL/TIRE ASSEMBLIES, AND PRESSURE LINE PER BOEING M/M.

Part: SLIDE — LOW PRESS (AFT ENTRY DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY SLIDE INSPECTION DUE. REPLACED SLIDE ASSEMBLY PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C1 CHECK, FOUND A FUSELAGE SKIN CRACK AT AFT LRRA ANTENNA AREA, FWD RIVET. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 947)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 947, S20L. REPAIRED PER BOEING SRM.

Part: DOOR FRAME — CRACKED (BS 440)

DURING SCHEDULED D-CHECK, FOUND DOOR FRAME CRACKED AT BS 440, RBL 36.5, WL 162. REPAIRED PER BOEING SRM.

Part: FRAMES — CRACKED (BS 294/616/639)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 616, WL 202, LBL 65, AT BS 294, RBL 54, WL 274, AND AT BS 639, WL 202, LBL 65. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 960)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 960, S21L. REPAIRED PER TRAMCO EWO 96-0406.

Part: SKIN — DENTED (BS 398)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 398, S24-25R. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 947)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 947, RBL 46 TO 43, WL 208. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM UPPER T-CHORD CORRODED AT BS 294.5, BBL ZERO TO LBL 8. REPAIRED PER BOEING SRM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD CHORD CRACK AT BS 178, WL 208.5, TO WL 207, LBL 29. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — CORRODED (BS 967)

DURING SCHEDULED D-CHECK, FOUND FRAME SHEAR TIE CORRODED AT BS 967, S25L. REPAIRED PER BOEING SRM.

Part: SUPPORTS — CORRODED (BS 400-520)

DURING SCHEDULED D-CHECK, FOUND FLOOR TO SIDEWALL SUPPORTS CORRODED AT BS 400A TO BS 520, RBL 23, WL 156, AT BS 492, RBL 32, WL 160, AND AT BS 420 TO BS 440, RBL 23, WL 156. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — GOUGED (BS 178)

DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD WEB GOUGED AT BS 178, RBL 12, WL 239. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 947-1012)

DURING SCHEDULED D-CHECK, FOUND STRINGER 27L CORRODED FROM BS 947 TO BS 1012. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 225)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED AT BS 225, S25R. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CRACKED (BS 710/712)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM WEB CRACKED TWO PLACES, BS 710 AND BS 712, RBL 25, WL 203. REPAIRED PER BOEING SRM.

Part: BULKHEAD ANGLE — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND T-ANGLE CRACK ON AFT SIDE OF BS 178 BULKHEAD, LBL 5.5, WL 183.5. REPAIRED PER BOEING SRM.

Part: FAN — FAILED (AC BAY)

FLIGHT ATTENDANT NOTED AND REPORTED TO CAPT AN ODOR IN THE CABIN. A UPS PILOT ONBOARD SUGGESTED THAT IT WAS SIMILAR TO THAT OF AN ELECTRICAL SMELL. CREW TURNED GASPER FAN OFF AND SMELL DISSIPATED. THEN SMELL RETURNED, CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED AT BWI WITHOUT INCIDENT. INSPECTED AND FOUND GASPER FAN TO BE THE FAULT, DEFERRED GASPER FAN OPERATION AND CONTINUED PER MEL 21-26. REPLACED GASPER FAN BER BOEING M/M.

Part: DOOR STOP — CRACKED (AIRSTAIR DOOR)

DURING SCHEDULED B/C CHECK, FOUND FWD UPPER AIRSTAIR DOOR STOP AFT T-CAP SECTION CRACKED 1.5 LONG. REPLACED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND AFT SECTION OF CABIN FLOOR TRACK LIGHTING INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: BULKHEAD — CRACKED (CONTROL CABIN)

DURING SCHEDULED C3 CHECK, FOUND BULKHEAD SKIN CRACKED AT CONTROL CABIN LEFT SIDE, 6 INCHES UP FROM FLOOR AND 6 INCHES FROM O/B EDGE. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND AFT CABIN FLOOR LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.