N056SW
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.
23 reports on file, 1998-04-20 – 1999-11-22.
Part: SKIN — DELAMINATED (AILERON)
DURING WALK ARROUND INSP, FOUND RT AILERON DELAMINATED. REMOVED AND REPLACED AILERON PER MM.
Part: DETECTOR — INOP (#1 ENG)
RIGHT AFTER LANDING, NR 1 ENG FIRE WARNING LIGHT AND BELL SOUNDED, SHUT ENG DOWN, AND FIRED BOTH FIRE EXTINGUISHER BOTTLE. WARNING STOPPED. REMOVED AND REPLACED UPPER FIRE LOOP ELEMENT PER MM.
Part: BATTERY — DISCHARGED (RT EMER EXIT)
DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AND CHARGER PER MM.
Part: LIGHT — INOP (EMER EXIT)
DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AFT OF OVERWING DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: SLIDE — OUT OF POSITION (PAX DOORWAY)
DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.
Part: BATTERY PACK — DISCHARGED (CARGO COMPT)
DURING SCHEDULED SERVICE CHECK, FOUND LT OUTER OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY CHARGER — INOP (CABIN)
DURING SCHEDULED A1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.
Earlier reports · 1998 · 16 reports
1998
Part: BRAKE — WORN (MLG)
MUCH HIGHER BRAKE PEDAL PRESSURE IS REQUIRED TO GET NORMAL BRAKING. ON BOTH LT/RT PEDALS AND BOTH PILOT SIDES, NO ANTI-SKID LIGHTS ILLUMINATED, BRAKE AND ACCUMULATOR PRESSURES NORMAL. VERY HIGH PEDAL PRESSURE FOR BRAKES TO GRAB. PERFORMED TAXI CHECK WITH ANTI SKID SYSTEM ON AND OFF. BRAKES OPERATED NORMALLY WITH ANTI SKID OFF. BRAKES REQUIRED EXCESSIVE PRESSURE AND PULSED AND GRABBED WITH ANTI SKID ON. BRAKE ASSYS VISUALLY CHECKED OK PER MM. REMOVED AND REPLACED NR 1 AND NR 2 MAIN GEAR BRAKES AND BRAKE SHUTTLE VALVES. OPS AND LK CKD GOOD PER M/M. PERFORMED SYSTEM CHECK OF ANTI SKID SYSTEM. CKD GOOD PER MM.
Part: MOTOR — INOPERATIVE (RADAR ANTENNA)
AIRCRAFT DIVERTED TO DAL DUE TO WX RADAR WOULD NOT PAINT WX OR GROUND RETURNS. WX RADAR INOPERATIVE. RED HALF MOON BAND AT 5 MILE ARC. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED RADAR ANT MOTOR, OPS CHECK OK PER BOEING MM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTS AT FWD ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER BOEING MM.
Part: SKIN — CRACKED (BS 758.8-761.5)
DURING SCHEDULED RON CHECK, FOUND 2.65 INCH CRACK AT BS 758.8 TO BS 761.5 STR 24L. REPAIRED PER BOEING SRM.
Part: CSD — FAILED (NR 1 ENGINE)
AIR RETURN DUE TO NR 1 GEN LOW OIL PRESSURE LIGHT ILLUMINATED DURING TAKEOFF. DISCONNECTED NR 1 CSD. APU FIRE DETECTION SYSTEM INOP. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NR 1 CSD ASSYS PER BOEING MM. RAN ENGINE OPS CK'D OK AND CHANGE IN LINE FILTER LEAK CK'D OK.
Part: INTERCOSTAL — CORRODED (BS 328-344)
DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED INTERCOSTAL AT CLIP NUT HOLES AT BS 328 TO 344, LBL 10. REMOVED AND REPLACED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 294)
DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED FLOORBEAM HOLE AT BS 294, LBL 47. REMOVED AND REPLACED PER BOEING SRM.
Part: SKIN — CRACKED (BS 1136)
DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED FUSELAGE SKIN AT 2 ADJACENT FASTENERS AT BS 1136, STR 10R. REPAIRED PER BOEING SRM.
Part: ANGLE — CRACKED (LT WING)
DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED I/B FLAP WELL LWR SURFACE SUPPORT ANGLE AND WORN JUST ABOVE CANOE. REPAIRED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 504/505)
DURING SCHEDULED 1/4 D-CHECK, FOUND CORROSION UNDER FLOORBEAM NUT PLATE AT BS 504 LBL 13.5, BS 505 LBL 8.5 AND BS 504 RBL 2.5. REMOVED AND REPLACED PER BOEING SRM.
Part: CROSS MEMBER — CORRODED (FUSELAGE)
DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED FLOOR CROSS MEMBER AT BS 1011 LBL 7.5, BS 1013 LBL 6, BS 998 LBL 13.5, BS 999 LBL 11.5 AND 1001 LBL 12. REMOVED AND REPLACED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 429)
DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED FLOORBEAM NUT PLATE AT BS 429, RBL 8.5. REPAIRED PER BOEING SRM.
Part: STRINGER — CORRODED (BS 1006)
DURING SCHEDULED 1/4 D-CHECK, FOUND HEAVY CORROSION AT BS 1006, STR 27L AND BS 1006, STR 26L. REPAIRED PER BOEING SRM.
Part: CROSS MEMBER — CORRODED (FUSELAGE)
DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED FLOOR CROSS MEMBER AT BS 1003.5 LBL 10.5, BS 1004 LBL 11.5, BS 1008.5 LBL 7.5, BS 1010 LBL 8.5 AND BS 1011 LBL 6.5. REMOVED AND REPLACED PER BOEING SRM.
Part: SPLICE — CORRODED (BS 987 - 1006)
DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED SPLICE PLATE BETWEEN BS 987 AND 1006 AT O/B GALLEY TRACK. REMOVED AND REPLACED PER BOEING SRM.
Part: SKIN — CRACKED (BS 927)
DURING SCHEDULED RON CHECK, FOUND CRACKED FUSELAGE SKIN 1.25 AT BS 927, RT SIDE AFT OF AFT CARGO DOOR. REPAIRED PER BOEING SRM.