N93SW
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.
21 reports on file, 1995-04-09 – 1999-12-19.
Part: DUCT — CRACKED (NR 1 ENGINE)
AIR TURNBACK, NR 1 ENG OVERHEAT LIGHT ILLUMINATED. FOUND NR 1 ENG UPPER FUEL HEAT DUCT CRACKED. REMOVED AND REPLACED DUCT PER MM.
Part: SLIDE — SHIFTED (PAX DOOR)
AFT ENTRY DOOR EVACUATON SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.
Earlier reports · 1995–1997 · 19 reports
1997
Part: SEALS — JAMMED (NR 4 LE SLAT)
AFTER TAKEOFF, EXPERIENCED L/E FLAP AND NR 4 SLAT YELLOW TRANSIT LIGHTS REMAINING ILLUMINATED. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REMOVED JAMMED AUX TRACK SLAT SEALS. INSTALLED NEW PER BOEING M/M.
Part: SKIN — CRACKED (BS 930)
DURING RON CHECK, FOUND A 3 FUSELAGE SKIN CRACK AT BS 930, RIGHT SIDE. REPAIRED PER BOEING SRM.
Part: BEARING — FAILED (RT TE FLAP)
AFTER TAKEOFF, EXPERIENCED AIRFRAME VIBRATION, WITH FLAPS AT 2 DEG, RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. INSPECTED, REPLACED RT I/B FLAP DRIVE MECHANISM BEARING AND BOOM CABLES PER BOEING M/M. ALSO, PERFORMED OVERWEIGHT LANDING INSPECTION.
Part: BEARINGS — WORN (RT TE FLAP)
DURING CLIMBOUT, NOTED AIRFRAME VIBRATION AND A SLIGHT ROLL TO THE RIGHT WITH FLAPS AT 2 DEGREES. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REPLACED RT I/B AFT FLAP DRIVE BEARINGS AND BOOM CABLES PER BOEING M/M.
Part: FRAME — CRACKED (GALLEY DOOR)
DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR LOWER AFT FRAME INNER DOUBLER CRACKED. INSTALLED DOUBLER REPAIR PER BOEING SRM.
Part: ANGLE — CRACKED (BS 270)
DURING SCHEDULED D-CHECK, FOUND Z-ANGLE CORRODED AT BS 270, BL 0, WL 208 AND FROM RBL 7 TO LBL 5. REPAIRED PER BOEING SRM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD SIDE CHORD CRACKED LEFT SIDE. REPAIRED PER BOEING SRM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT WL 234, RBL 13. REPAIRED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 359)
DURING SCHEDULED D-CHECK, FOUND STRINGER 15L LOWER FLANGE TIE CRACKED AT BS 360 AND STRINGER 14L AT BS 359 CRACKED IN LOWER FLANGE. REPLACED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 344)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 56 TO RBL 1, WL 208. REPAIRED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 360)
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 360, RBL 1 TO 20, WL 208. REPAIRED PER BOEING SRM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND BULKHEAD BS 178 CRACKED AT LBL 6.7 TO 13.0, RBL 14.25 TO 15.0 AND RBL 10.25. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (GALLEY DOOR)
DURING SCHEDULED D-CHECK, FOUND FORWARD GALLEY DOOR OUTER SKIN FORWARD EDGE ABOVE HINGE CUTOUT CRACKED AT FASTENER HOLE. REPAIRED PER BOEING SRM.
Part: BULKHEAD ANGLE — CRACKED (BS 727)
DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 727 PLUS 4 SUPPORT ANGLE AT RBL 10, WL 160. REPAIRED PER BOEING SRM.
Part: BULKHEAD CHORD — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND BULKHEAD BS 178 AFT SIDE CHORD CRACKED AT LBL 5.7, WL 183. REPAIRED PER BOEING SRM.
1996
Part: COFFEEMAKER — INOPERATIVE (FWD GALLEY)
DURING DESCENT, NOTED A PLASTIC TYPE BURNING SMELL IN FWD GALLEY AREA. INSPECTED GALLEY COFFEEMAKERS, PULLED AND COLLARED C/B'S TO FWD GALLEY COFFEEMAKERS, NO OTHER DISCREPANCIES NOTED.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED A2 CHECK, FOUND FWD LT AND RT EXTERNAL EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK PER BOEING M/M.
1995
Part: FUEL CONTROL — MALFUNCTIONED (NR 2 ENGINE)
AFTER TAKEOFF, EXPERIENCED NR 2 ENGINE POWER FLUCTUATION AT ALL SETTINGS. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REPLACED NR 2 ENGINE FUEL CONTROL UNIT PER BOEING M/M.
Part: CONNECTOR — BROKEN (NR 1 ENGINE)
DURING CLIMBOUT, NUMBER 1 ENGINE OIL TEMP INDICATOR ENTERED YELLOW RANGE FOR 14 MINUTES. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND NR 1 ENGINE OIL TEMP SENSOR CANNON PLUG PIN B BROKEN. REPLACED PIN AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING MM.