N060SW
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.
47 reports on file, 1998-06-19 – 2001-11-15.
Part: TIRE — BLEW OUT (RH NLG) · airframe 70,747 hrs · 78,981 cycles
( AIR TURNBACK, DECLARED EMERGENCY )â¦â¦â¦â¦â¦â¦â¦â¦â¦â¦..DURING T/O RH NOSE TIRE BLEW DAMAGING TCAS ANTENNA AND FUSELAGE SKIN FWD OF TCAS ANTENNA. R&R BOTH NLG TIRE/WHEEL ASSY'S. R&R LWR TCAS ANTENNA & REPAIRED SKIN PER SWA RA.
Part: LIGHT — INOPERATIVE (ENTRY DOOR) · airframe 70,742 hrs · 78,976 cycles
DURING SCHEDULED RON, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: LIGHT — LOOSE (SERVICE DOOR) · airframe 70,725 hrs · 78,954 cycles
FWD SVC DOOR EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED EXIT LIGHT PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,418 hrs · 78,580 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 831, STR 18L. REPAIRED SKIN PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,145 hrs · 78,268 cycles
DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT PER MM.
Part: CAP — MISSING (CABIN) · airframe 69,352 hrs · 77,339 cycles
DURING SCHEDULED SERVICE CHECK, FOUND EEPLS FLOOR TRACK MISSING END CAP. INSTALLED END CAP PER MM.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 68,805 hrs · 76,747 cycles
FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: CONNECTOR — LOOSE (NR 1 ENGINE) · airframe 68,791 hrs · 76,729 cycles
ABORTED TAKEOFF, EPR INDICATORS FAILED ON NR 1 & 2 ENGINES DURING ROLLOUT. FOUND NR 1 ENG EPR TRANSMITTER CONNECTOR LOOSE. SECURED CONNECTOR PER MM.
Part: DIODE — WEAK (EMERGENCY LIGHT) · airframe 68,583 hrs · 76,500 cycles
DURING SCHEDULED C4 CHECK, FOUND EEPLS LIGHTS DIM BETWEEN ROWS 5 & 10. REMOVED AND REPLACED BLOCKING DIODE AT MID CABIN PER MM.
Part: COVER — MISSING (CABIN) · airframe 68,583 hrs · 76,500 cycles
DURING SCHEDULED C4 CHECK, FOUND EEPLS FLOOR TRACK COVERS MISSING AT FWD SECTION. INSTALLED TRACK COVERS PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,583 hrs · 76,500 cycles
DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BRACKET — LOOSE (FWD SVC DOOR) · airframe 68,583 hrs · 76,500 cycles
DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE FWD GIRT BRACKET LOOSE. SECURED BRACKET PER MM.
Earlier reports · 1998–2000 · 35 reports
2000
Part: SKIN — CRACKED (FUSELAGE) · airframe 68,115 hrs · 75,971 cycles
DURING SCHEDULED RON CHECK, FOUND 3 INCH EXTERNAL FUSELAGE SKIN CRACK AT STR 16L, APPROX BS 500. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 68,096 hrs · 75,950 cycles
DURING SCHEDULED RON CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT STR 16L, APPROX. BETWEEN BS 500 & BS 520.
Part: BRACKET — LOOSE (SLIDE GIRT BAR) · airframe 67,847 hrs · 75,666 cycles
DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY BRACKETS LOOSE ON FLOOR. SECURED BRACKETS PER MM.
Part: SLIDE — DISLODGED (PAX DOOR) · airframe 67,566 hrs · 75,372 cycles
FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CASE WHILE PARKED AT GATE. REINSTALLED SLIDE ASSY PER MM.
Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 67,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND HORIZONTAL STAB CENTER SECTION REAR SPAR WEB CRACKED, RBL 12.5 ADJACENT TO REAR SPAR CHORD. REPAIRED WEB PER DALFORT XEA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND AFT CARGO DOOR FUSELAGE SKIN CUTOUT CRACKED AT FWD LOWER CORNER. REPAIRED SKIN PER DALFORT XEA.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,155 hrs · 74,919 cycles
DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIES CRACKED, BS 767, BETWEEN STRINGERS 27L - 28L, AND BS 847, STRINGER 27R. REPAIRED SHEAR TIE SECTIONS PER SRM.
Part: FRAME — CRACKED (CABIN) · airframe 67,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 767, STRINGER 13L. REPAIRED FRAME PER SRM.
Part: FLOORBEAM — CORRODED (CABIN) · airframe 67,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 967 FLOORBEAM CORRODED. REPAIRED FLOORBEAM PER SRM.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 67,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND RT WING I/B TRAILING EDGE FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.
Part: STRINGER — CRACKED (CABIN) · airframe 67,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 359, STRINGER 14L CRACKED. REPAIRED STRINGER SECTION PER SRM.
Part: STRINGER — CRACKED (CABIN) · airframe 67,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 903, STRINGER 14L SPLICE CRACKED. REMOVED AND REPLACED SPLICE SECTION PER SRM.
Part: SHEAR TIE — CRACKED (CABIN) · airframe 670,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 400 SHEAR TIE CRACKED, STRINGER 13R - 14R. REPAIRED SHEAR TIE PER SRM.
Part: STRINGER — CRACKED (CABIN) · airframe 670,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 4R CRACKED, BS 908. REPAIRED STRINGER SECTION PER SRM.
Part: FITTING — CRACKED (CARGO BAY) · airframe 670,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 727 BULKHEAD VERTICAL BEAM UPPER FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 67,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 5.7, WL 218. REPAIRED BULKHEAD PER SRM.
Part: SHEAR TIE — CRACKED (CABIN) · airframe 67,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 360 SHEAR TIE CRACKED, STR 15L TO STR 16L. REPAIRED SHEAR TIE SECTION PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 359, STRINGER 14L CRACKED. REPAIRED STRINGER SECTION PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BS 277 FRAME CRACKED, STRINGER 16L. REPAIRED FRAME PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED, BS 327, STR 16R AND BS 380, STR 15R. REMOVED AND REPLACED CLIPS PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 4L CRACKED BS 908. REPAIRED STRINGER SECTION PER SRM.
Part: SHEAR TIE — CRACKED (CABIN) · airframe 67,150 hrs · 74,912 cycles
DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED, BS 400, BETWEEN STRINGERS 15R - 16R. REPAIRED SHEAR TIE PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 66,113 hrs · 73,766 cycles
DURING SCHEDULED A1 CHECK, FOUND FUSLAGE EXTERNAL SKIN CRACKED 1.5 INCHES LONG, BS 867, STRINGER 24 LT. REPAIRED SKIN PER SRM.
Part: SKIN — DELAMINATED (TE FLAP)
DURING SCHEDULED SERVICE CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED AT T/E. REPAIRED FLAP PER SRM.
1999
Part: BRACKET — LOOSE (SERVICE DOORWAY)
DURING SCHEDULED C3 CHECK, FOUND FWD AND AFT SERVICE DOOR GIRT BAR FLOOR ATTACH BRACKETS LOOSE. TIGHTENED BRACKETS PER MM.
Part: LIGHT — MISSING (ROW 18)
DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK MISSING AT ROW 18. INSTALLED TRACK COVER PER MM.
Part: EPR TRANSMITTER — ERRATIC (RT ENGINE)
ABORTED TAKEOFF AT APPROX 40 KNTS DUE TO NR 1 ENG SURGING RAPIDLY FROM 1.7 TO 2.00 EPR. REMOVED AND REPLACED EPR TRANSMITTER PER MM.
Part: BATTERY CHARGER — INOPERATIVE (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY ESCAPE FLOOR TRACK LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.
1998
Part: BATTERY PACK — MISSING (SERVICE DOOR)
DURING WALKAROUND CHECK, FOUND FWD SERVICE DOOR EMERGENCY LIGHTS BATTERY PACK ROBBED FOR A/C 103 COCKPIT POSITION. INSTALLED SERVICEABLE EMERGENCY LIGHT BATTERY PACK A ASSY PER BOEING MM.
Part: SKIN — CRACKED (BS 927)
DURING SCHEDULED A1 CHECK, FOUND CRACKED FUSELAGE SKIN JUST FWD AND OUTBOARD OF AFT WATER SERVICE PANEL AT BS 927 STR 20L. REPAIRED PER BOEING SRM.
Part: SHEAR TIE — CRACKED (BS 360)
DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SHEAR TIE AT BS 360 BETWEEN STR 14 AND 13 RT. REPAIRED PER SRM.
Part: DOUBLER — CRACKED (BS 950)
DURING SCHEDULED SERVICE CHECK, FOUND CRACKED AT BS 950, STR 10 DOOR FRAME. REPAIRED PER SRM.
Part: FRAME — CRACKED (BS 663.75)
DURING SCHEDULED SERVICE CHECK, FOUND FRAME UPPER FLANGE CRACKED AT BS 663.75, STR 3R. REPAIRED PER SRM.
Part: LIGHT — INOPERATIVE (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT SEAT ROW NR 3. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: TRANSDUCER — MALFUNCTIONED (ANTI-SKID)
AIRCRAFT DIVERTED, OUTBOARD ANTI-SKID LIGHT CAME ON AFTER T/O. LIGHT STAYED ON FOR 1 HR. RECYCLED GEAR, NO HELP. LIGHT WENT OUT IN PATTERN AT STL. OK CONT MEL. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED TRANSDUCER PER BOEING MM.