N80SW
Registered owner: KOLPAKCHI IGOR, NY (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.
39 reports on file, 1995-01-19 – 2000-03-09.
Part: INDICATOR — DISLODGED (ESCAPE SLIDE)
DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.
Earlier reports · 1995–1999 · 38 reports
1999
Part: SLIDE — DISCHARGED (PAX DOOR)
DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.
Part: STRINGER — CORRODED (BS 973-998)
DURING SCHEDULED D CHECK, FOUND STRINGER 27L CORRODED BETWEEN BS 973-998. REPAIRED STRINGER PER SRM.
Part: SPLICE — CRACKED (BS 360)
DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED, BS 360, STRINGER 11L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.
Part: DOUBLER — CRACKED (BS 1138)
DURING SCHEDULED D CHECK, FOUND DOUBLER STRAP CRACKED, BS 1138, STRINGER 12L AND STRINGER 5R. REPAIRED DOUBLER PER SRM.
Part: STRINGER — CORRODED (BS 1138)
DURING SCHEDULED D CHECK, FOUND STRINGER 5R CRACKED, BS 1138. REPAIRED STRINGER PER SRM.
Part: FLOORBEAM — CORRODED (BS 344)
DURING SCHEDULED D CHECK, FOUND BS 344 FLOORBEAM UPPER FACE CORRODED, RBL 11-RBL 56. REPAIRED BEAM PER SRM.
Part: STRINGER — CORRODED (BS 727)
DURING SCHEDULED D CHECK, FOUND STRINGER 4L CRACKED, BS 727. REPAIRED STRINGER PER SRM.
Part: FLOORBEAM — CORRODED (BS 312)
DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED, BS 312, RBL 6. REPAIRED BEAM PER SRM.
Part: BRACKET — CRACKED (SERVICE DR SLIDE)
DURING SCHEDULED D CHECK, FOUND FWD SERVICE SLIDE EVACUATION SLIDE FWD GIRT BAR MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER OHM.
Part: STRINGER — CRACKED (BS 900-933)
DURING SCHEDULED D CHECK, FOUND STRINGER 26L CRACKED AND CORRODED, BS 900-933. REPAIRED STRINGER PER SRM.
Part: CHORD — CRACKED (HORIZ STAB)
DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB AFT UPPER TEE CHORD CRACKED AT ELEV STA 94.07. REPAIRED CHORD PER SRM AND BOEING DRAWING.
Part: SKIN — CRACKED (SERVICE DOORWAY)
DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACK AT AFT SERV DOOR AT LOWER HINGE ARM CUTOUT. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (FUSELAGE)
DURING SCHEDULED CHECK, FOUND 4 INCH FUSELAGE SKIN CRACK ON RT SIDE ABOVE NR 24 PAX WINDOW. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (FUSELAGE)
DURING SCHEDULED CHECK, FOUND 4 INCH FUSELAGE SKIN CRACK ON RT SIDE ABOVE NR 24 PAX WINDOW. REPAIRED PER BOEING SRM.
1998
Part: STRINGER — CORRODED (BS 965)
DURING SCHEDULED 1/4D CHECK, FOUND CORRODED BS 965, STRINGER 26R. REPAIRED PER BOEING SRM.
Part: INTERCOSTAL — CRACKED (BS 291.5)
DURING SCHEDULED 1/4 D-CHECK, FOUND INTERCOSTAL ATTACH ANGLE CRACKED BELOW S15R AT BS 291.5. REPLACED PER BOEING SRM.
Part: INTERCOSTAL — CRACKED (BS 295)
DURING SCHEDULED 1/4 D-CHECK, FOUND INTERCOSTAL ATTACH ANGLE CRACKED ABOVE S12R AT BS 295. REPLACED PER BOEING SRM.
Part: SKIN — CRACKED (BS 943)
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 24L. REPAIRED PER BOEING SRM.
1997
Part: SKIN — CRACKED (FUSELAGE)
DURING SCHEDULED SERVICE CHECK, FOUND A 3 INCH FUSELAGE SKIN CRACK AT RIGHT SIDE ABOVE T/E FLAPS. REPAIRED PER BOEING SRM.
Part: LIGHT — INOPERATIVE (CABIN)
DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.
Part: BATTERY — DISCHARGED (CABIN)
DURING WALKAROUND CHECK, FOUND FWD CABIN EMERGENCY LIGHTS INOP \N\NREPLACED BATTERY PACK PER BOEING M/M
Part: WIRE — SHORTED (NR 1 START SW)
SMOKE AND ELECTRICAL SMELL IN COCKPIT NEAR NR 1 ENGINE START SWITCH. INSPECTED AND FOUND NR 1 START SWITCH SHORTED AGAINST STANDBY COMPASS. REPAIRED 5 WIRES PER BOEING M/M.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED TERMINAL CHECK, FOUND CABIN CENTER ISLE OVERWING EXIT LIGHTS INOP. REPLACED LIGHT BATTERY PER BOEING M/M.
1996
Part: SKIN — CRACKED (SERVICE DOORWAY)
DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR OUTER SKIN CRACKED THROUGH RIVET EXTENDING FWD .25 AND AFT .125. RIVET LOCATED UPPER FWD ABOVE LOWER HINGE CUTOUT. REPAIRED PER BOEING SRM.
Part: ACTUATOR — FAILED (NR 5 LE SLAT)
RETURNED TO PHX DUE TO NR 5 L/E SLAT NOT FULLY RETRACTING. INSPECTED, REPLACED NR 5 SLAT ACTUATOR AND OP CHECKED PER BOEING M/M.
Part: ACTUATOR — MALFUNCTIONED (NR 3 LE SLAT)
ON CLIMBOUT, NR 3 SLAT WOULD NOT FULLY RETRACT. AIRCRAFT RETURNED TO MAF AND MADE AN UNEVENTFUL LANDING. INSPECTED AND LUBED SLAT TRACKS, OPERATION CHECKED SLATS. MX FERRIED TO DAL. REMOVED AND REPLACED NR 3 SLAT ACTUATOR AND OP CHECKED PER BOEING M/M.
Part: FUEL LINE — LEAKING (APU)
FUEL FUMES NOTED IN CABIN AREA WHILE APU BLEED ON. INSPECTED AND FOUND PRESSURE LINE AT ATOMIZER LEAKING. CONTINUED WITH APU INOP PER MEL 49-1.
Part: DOUBLER — ELONGATED HOLES (VHF ANTENNA)
DURING SCHEDULED CHECK, FOUND EGG SHAPED HOLES ON NR 2 VHF ANTENNA DOUBLER. REPAIRED PER SWA ACO 6470-53.
Part: SKIN — DAMAGE (BS 420-440)
DURING SCHEDULED CHECK, FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BETWEEN BS 420 AND 440, BETWEEN S14 AND 15L. REPAIRED PER BOEING SRM.
Part: SUPPORT — CRACKED (BS 540)
DURING SCHEDULED CHECK, FOUND FLOORBEAM SUPPORT AT BS 540, BL 0 TO LBL 25, WL 208 CRACKED. REPLACED PER SWA ACO 6470-53.
1995
Part: SKIN — CRACKED (BS 713)
DURING SCHEDULED MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AT BS 713, LBL 24.5, WL 204. REPAIRED PER BOEING SRM.
Part: FLOOR BEAM — CORRODED (BS 294)
DURING SCHEDULED MAINTENANCE, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 294, RBL 14 TO LBL 14, WL 208. REPAIRED PER SWA TR 1-353-009.
Part: SKIN — DENTED (BS 907)
DURING SCHEDULED MAINTENANCE, FOUND FUSELAGE SKIN DENTED AT BS 907, BETWEEN STRINGERS 22 AND 23L AND AT BS 940 AT S18 AND 19L. REPAIRED PER BOEING SRM.
Part: WEB — CRACKED (BS 178)
DURING SCHEDULED MAINTENANCE, FOUND PRESSURE WEB CRACKED AT BS 178, WL 217, RBL 9.5 TO 13. REPAIRED PER BOEING SRM.
Part: STRINGER — CORRODED (BS 1006)
DURING SCHEDULED MAINTENANCE, FOUND STRINGER 27L CORRODED AT BS 1006. REPAIRED PER BOEING SRM.
Part: KEEL BEAM — CORRODED (BS 947)
DURING SCHEDULED MAINTENANCE, FOUND TOP OF FLOOR BEAM CHORD CORRODED AT BS 947, WL 208, RBL 55 TO LBL 55. REPAIRED PER BOEING SRM.
Part: FLOOR BEAM — CORRODED (BS 928)
DURING SCHEDULED MAINTENANCE, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 928, RBL 14-55, WL 208. REPAIRED PER SWA RA 1-253-423.
Part: ACTUATOR — INOP (NR 6 SLAT)
DURING CLIMB, NUMBER 6 L/E SLAT TRANSIT LIGHT REMAINED ILLUMINATED. RECYCLED SLATS WITH NO HELP. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 6 SLAT ACTUATOR AND OPERATION CHECK PER BOEING MM.