N57SW
Registered owner: SCHIEFEN-GUNDERSON ANNICKA K, SD (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
82 reports on file, 1995-01-07 – 1999-10-26.
Part: SKIN — CRACKED (BS 727)
EXTERNAL FUSELAGE SKIN CRACKED, APPROX BS 727C, STRINGER 14L. REPAIRED SKIN PER SRM.
Part: WEB — CRACKED (BS 277)
DURING SCHEDULED SERVICE CHECK, FOUND NLG WHEEL WELL CEILING CRACKED, BS 277 RT SIDE. REPAIRED WEB PER SRM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR)
UNABLE TO READ SLIDE PRESSURE GAGE ON THE AFT SERVICE DOOR. REPOSITIONED SLIDE PACK ASSY PER MM.
Part: BATTERY — DISCHARGED (EXTERIOR)
DURING SCHEDULED SERVICE CHECK, FOUND LEFT AND RIGHT SIDE, OUTER EGRESS LIGHTS INOP. REMOVED AND REPLACED BATTERY SUPPLY PER MM.
Part: SKIN — CRACKED (BS 510)
DURING SCHEDULED SERVICE CHECK, FOUND A 3 INCH CRACK AT FUSELAGE SKIN BS 510, STR 18R. REPAIRED PER SRM.
Earlier reports · 1995–1998 · 77 reports
1998
Part: LIGHT — INOPERATIVE (PAX DOOR)
DURING SCHEDULED SERVICE CHECK, FOUND FWD PASSENGER DOOR EMERGENCY EXIT LIGHT CHARGING BASE BAD. REPLACED FWD PASSENGER DOOR EMERGENCY EXIT LIGHT PER PER BOEING MM.
Part: SKIN — CRACKED (PAX DOORWAY)
DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED PER BOEING MM.
Part: SKIN — DAMAGED (BS 360-540)
DURING SERVICE VISIT, REPAIRED SKIN LAP AT BS 360 TO 540, STR 14L, BS 360 TO 540 STR 10L, BS 360 TO 540 STR 4L, BS 360 TO 540 STR 4R AND BS 360 TO 540 STR 10R. REPAIRED PER SWA ACO 6717-53.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND CENTER EMERGENCY EXIT LIGHT BATTERY AND BASE CHECK BAD. REMOVED AND REPLACED BASE SYSTEM AND BATTERY PER BOEING MM.
Part: SKIN — DAMAGED (BS 727-908)
DURING SERVICE VISIT, REPAIRED SKIN LAP AT BS 727 TO 908 STR 4R AND BS 727 TO 908, STR 10R. REPAIRED PER SWA ACO 6717-53.
Part: STRINGER — CRACKED (BS 380)
DURING SCHEDULED SERVICE CHECK, FOUND CRACKED STRINGER 3L AT BS 380 UNDER STRINGER TIE CLIP. REPAIRED PER BOEING SRM.
Part: SKIN — DAMAGED (BS 360-540)
DURING SERVICE VISIT, REPAIRED SKIN LAP AT BS 360 TO 540 STR 14R, BS 540 TO 727 STR 4L, BS 540 TO 727 STR 4R, BS 727 TO 908 STR 10L AND BS 727 TO 908 STR 4L. REPAIRED PER SWA ACO 6717-53.
Part: STRINGER — CRACKED (BS 1010)
DURING SCHEDULED SERVICE CHECK, FOUND CRACKED STRINGER 4L AT BS 1010. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 938 STR 10R)
THE FUSELAGE SKIN FOUND CRACKED IN THE SKIN LAP LOWER ROW AT STA 938, STR 10R, AT SEVERAL FASTENER HOLES. THIS REPAIR IS ADJACENT TO THE AFT GALLEY DOOR UPPER HINGE CUT OUT. REPAIRED PER DALFORT AEROSPACE, L.P. XEA X2-53-213 DATED 3-17-98. REF: FAA FORM 8110-3 DATED MARCH 24, 1998.
1997
Part: LIGHT — INOPERATIVE (R2 DOOR)
DURING SCHEDULED TERMINAL CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.
Part: LIGHT — INOPERATIVE (CABIN)
DURING SCHEDULED TERMINAL CHECK, AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT MODULE AND OP CHECKED PER BOEING M/M.
1996
Part: SKIN — CRACKED (SERV DOOR CUTOUT)
DURING SCHEDULED B-CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED .3125 INCH. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (CARGO DOORWAY)
DURING SCHEDULED B-CHECK, FOUND A .75 INCH CRACK ON DOOR FRAME THROUGH 1ST FASTENER AFT OF LOWER FWD DOOR STOP MOUNT INSIDE DOOR. REPAIRED PER BOEING SRM.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED TERMINAL CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK PER BOEING M/M.
Part: ANGLE — CRACKED (FWD ENTRY)
DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY DOOR, INNER FRAME SKIN CRACKED BELOW LOWER HINGE. REPLACED FRAME ANGLE PER BOEING SRM.
Part: MOPSILL — CORRODED (BS 304-360)
DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR MOPSILL CORRODED AT BS 304 TO 360, WL 208, LBL 56. REPAIRED PER BOEING SRM.
Part: FLOOR BEAM — CORRODED (BS 344)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 50 TO RBL 8. REPAIRED PER BOEING SRM.
Part: SKIN — DENTED (BS 827)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 827, S27R, WL 155. REPAIRED PER BOEING SRM.
Part: SKIN — DENTED (BS 912-921)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED AT BS 912 TO 921, RBL 0 TO 19, FROM S24R TO S27R. REPAIRED PER BOEING SRM.
Part: SKIN — DENTED (BS 850-865)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED FROM BS 850 TO 865, S25 TO 27R. REPAIRED PER BOEING SRM.
Part: SHEAR TIE — CRACKED (BS 1138)
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1138, LBL 27, WL 261. REPAIRED PER BOEING SRM.
Part: SKIN — PUNCTURES (BS 1134)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN PUNCTURED AT BS 1134. REPAIRED PER BOEING SRM.
Part: SKIN — DAMAGE (BS 354)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN LIGHTNING STRIKE DAMAGE AT BS 354, S17 TO 18. REPAIRED PER TRAMCO EWO 96-0279.
Part: SKIN — CRACKED (SERV DR CUTOUT)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR LOWER HINGE CUTOUT. REPAIRED PER TRAMCO 96-0270.
Part: SPLICE — CORRODED (BS 907)
DURING SCHEDULED D-CHECK, FOUND I/B SIDE OF STRINGER SPLICE CORRODED AT BS 907, LBL 12, WL 166 AT S26L. REPLACED PER BOEING SRM.
Part: FRAME — CRACKED (BS 420)
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 420 AT S26L, ABOVE STRINGER CLIP. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (BS 597)
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 597, S17R, WL 208. REPLACED PER BOEING SRM.
Part: WEB — CRACKED (BS 135)
DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 135, LBL 8, WL 187. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (BS 492)
DURING SCHEDULED D-CHECK, FOUND UPPER FLANGE OF FUSE FRAME CRACKED AT BS 492, RBL 36, WL 162. REPAIRED PER TRAMCO EWO 96-0249.
Part: SKIN — DENTED (BS 921)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED AT BS 921, BETWEEN S22 AND 23R. REPAIRED PER BOEING SRM.
Part: SHEAR TIE — CRACKED (BS 1104)
DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1104, BELOW S5L. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND FUSE SKIN CRACKED AT BS 178, AT S17R. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (BS 328)
DURING SCHEDULED D-CHECK, FOUND FUSE FRAMES CRACKED AT BS 328, RBL 54, WL 183 AND AT BS 360, RBL 55, WL 184. REPLACED PER BOEING SRM.
Part: FRAME — CRACKED (BS 344)
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 344, LBL 45, WL 170. REPAIRED PER BOEING SRM.
Part: SKIN — DENTED (BS 1178)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1178, LBL 4. REPAIRED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 727)
DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 727B, S9R. REPLACED STRINGER SECTION PER BOEING SRM.
Part: SKIN — CRACKED (BS 727)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B PLUS 2, AT S18L. REPAIRED PER BOEING SRM.
Part: FRAME — DENTED (FWD CARGO)
DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY FRAME DENTED BEYOND LIMITS. REPLACED PER BOEING SRM.
Part: FRAME — CRACKED (BS 188)
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED IN RADIUS AT BS 188, S16R. REPAIRED PER BOEING SRM.
Part: CREASE BEAM — CRACKED (BS 639)
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM I/B CHORD CRACKED AT BS 639, RBL 65, WL 208. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND FUSE FRAMES CRACKED IN RADIUS AT BS 178, WL 207, RBL 29 AND LBL 29. REPLACED PER BOEING SRM.
Part: FRAME — CRACKED (BS 188)
DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 188, WL 207, LBL 28. REPAIRED PER BOEING SRM.
Part: SKIN — GOUGED (BS 380-400)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 380 TO 400, BELOW S19R. REPAIRED PER BOEING SRM.
Part: SPLICE — CORRODED (BS 907)
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, S26L. REPAIRED PER BOEING SRM.
Part: STRAP — CRACKED (BS 1138)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRAP CRACKED AT BS 1138, S12L. REPAIRED PER BOEING SRM AND BOEING DRAWING 65C35132.
Part: CHORD — CRACKED (BS 1154)
DURING SCHEDULED D-CHECK, FOUND LOWER CHORD CRACKED AT BS 1154, AT S5L. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (BS 440)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, AT S21L. REPAIRED PER BOEING SRM.
Part: SKIN — DAMAGED (BS 360-380)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AND GOUGED FROM BS 360 TO 380, S3L TO 6L. REPAIRED PER BOEING SRM.
Part: STRINGER — CORRODED (BS 907)
DURING SCHEDULED D-CHECK, FOUND O/B SIDE OF STRINGER CORRODED AT BS 907, RBL 15, WL 166, S26R. REPAIRED PER BOEING SRM.
Part: MOPSILL — CORRODED (BS 959-990)
DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR MOPSILL CORRODED AT BS 959 TO 990, RBL 53 TO 48, WL 209. REPAIRED PER BOEING SRM.
Part: FRAME — DENTED (BS 500)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 500A, RBL 44 AND RBL 52 TO 56, WL 168, 179 TO 177. REPLACED WITH NEW SECTION PER BOEING SRM.
Part: FRAME — DENTED (BS 500)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 500, RBL 33 AND RBL 26, WL 161 AND 169. REPLACED WITH NEW SECTION PER BOEING SRM.
Part: SPLICE — CRACKED (BS 907)
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, S4L. REPLACED PER BOEING SRM.
Part: SKIN — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AROUND FASTENER HEAD AT BS 178, WL 234, LBL 9. REPAIRED PER BOEING SRM.
Part: SKIN — DAMAGED (BS 382)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 382, S17L AND BS 381 BETWEEN S17L AND 16L. ALSO, DAMAGED CREASE BEAM WEB AND OUTER CREASE BEAM CHORD AT BS 383, WL 208, LBL 70. REPAIRED PER BOEING SRM.
Part: FRAME — DENTED (CARGO BAY)
DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY FRAME DENTED AT BS 500B S22 TO 25R, BS 400 S21 TO 25L, BS 420, S21 TO 25L, BS 480 S 21 TO 22L AND AT BS 500A 21 TO 25L. REPAIRED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 495)
DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 495, S22R. REPLACED WITH NEW SECTION PER BOEING SRM.
Part: STRINGER — CRACKED (BS 1010)
DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 1010, S6R. SPLICED IN NEW SECTION PER BOEING SRM.
Part: SPLICE — CRACKED (BS 907)
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, S4R. REPLACED PER BOEING SRM.
Part: SPLICE — CRACKED (BS 907)
DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, S4R. REPLACED SPLICE PER BOEING SRM.
Part: ANGLE — CRACKED (BS 540)
DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 540, LBL 41, WL 156. REPLACED PER BOEING SRM.
Part: STR CLIP — DAMAGED (BS 747)
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP DAMAGED AT BS 747, S20L. REPLACED PER BOEING SRM.
Part: LIGHT — INOP (AFT GALLEY)
DURING SCHEDULED C1 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT ABOVE SERVICE DOOR INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.
Part: SKIN — CRACKED (FUSELAGE)
DURING SCHEDULED CHECK, FOUND AFT SERVICE DOORWAY SKIN AT LOWER HINGE CUTOUT CRACKED UNDER REINFORCEMENT TAB. REPAIRED PER BOEING DRAWING 65C27269 AND SWA ACO 649-53.
Part: DOOR FRAME — CRACKED (CARGO COMPT)
DURING SCHEDULED MAINT CHECK, FOUND FWD CARGO DOOR FRAME CRACKED ABOVE FWD I/B DOOR STOP. REPAIRED PER SWA ACO 577-52.
Part: DOOR FRAME — CRACKED (AFT ENTRY DOOR)
DURING SCHEDULED MAINT CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUTOUT CRACKED AT BOTTOM RADIUS. REPAIRED PER BOEING SRM.
1995
Part: FRAME — CRACKED (BS 727)
DURING SCHEDULED MAINTENANCE, FOUND RT BS 727 O/B CHORD FRAME AT STRINGER 18A CRACKED FROM FWD EDGE OF FLANGE TO SECOND FASTENER. REPAIRED PER SWA ACO 651-53 REV 2.
Part: VALVE — LEAKING (A-HYD SYST)
DURING MAINT FERRY FLIGHT AFTER RUDDER CHANGE, AIRCRAFT LOST A-SYSTEM HYDRAULICS. AIRCRAFT RETURNED TO PAE AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND A-SYSTEM SHUTTLE VALVE LEAKING. REPLACED AND SERVICED SYSTEM PER BOEING M/M.
Part: WEB — CRACK (BS 178)
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, LBL 10.5 TO 12.7, WL 218. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: WEB — CRACK (BS 178)
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, RBL 5.7, WL 184 TO 207. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: WEB — CRACK (BS 178)
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, RBL 7.7 TO 14.7, WL 218. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: BEAM — CRACK (BS 178)
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND VERTICAL BEAM CRACKED AT BS 178, RBL 7, WL 203. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: WEB — CRACK (BS 178)
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, LBL 5.7, WL 201. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: PWR SUPPLY — INOP (LT O/W EEL)
DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT POWER SUPPLY PER BOEING M/M.
Part: EEL BATTERY — DISCHARGED (LT OVERWING)
DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED LEFT OVERWING LIGHT BATTERY PER BOEING M/M.
Part: EEL CHARGER — INOPERATIVE (CABIN)
DURING SCHEDULED A-CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY CHARGER PER BOEING MM.
Part: SKIN — CRACKED (BS 947)
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947 AT STRINGER 24R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.