N193SW
Registered owner: WISE MATTHEW A, PA (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.
26 reports on file, 1995-02-17 – 2000-07-29.
Part: UPLOCK SWITCH — FAILED (LT MLG) · airframe 30,446 hrs · 36,841 cycles
ON DEPARTURE, LANDING GEAR WOULD NOT RETRACT. ALL GREEN LIGHTS STAYED ON AND ALL RED LIGHTS WERE ON. IT FELT LIKE THE GEAR REMAINED IN THE DOWN POSITION WITH NO MOVEMENT. RETURNED TO RNO. REPLACED LEFT GEAR UPLOCK A SYSTEM PROX SWITCH IAW 32-61-01. OPS CHECKS GOOD.
Part: HARNESS — DAMAGED (WOW SWITCH) · airframe 30,427 hrs · 36,812 cycles
ON TAKEOFF GEAR WOULD NOT COME UP, ALL GREEN LIGHTS STAYED ON. NOSE AND RIGHT MAIN RED ''A'' CAME ON WITH HANDLE IN UP POSITION. IN DOWN POSITION ALL REDS OUT AND ALL GREENS ON, NORMAL DOWN INDICATION. FOUND DAMAGED WOW HARNESS ON LEFT MLG. REMOVED AND REPLACED HARNESS IAW EMB 120 MM 32-01-01. OPS CHECK GOOD AT THIS TIME. P/N ON: 20505-0010.
Part: RELAY — FAILED (MLG) · airframe 30,427 hrs · 36,812 cycles
ON TAKEOFF GEAR WOULD NOT COME UP, ALL GREEN LIGHTS STAYED ON. NOSE AND RIGHT MAIN RED ''A'' CAME ON WITH HANDLE IN UP POSITION. IN DOWN POSITION ALL REDS OUT AND ALL GREENS ON, NORMAL DOWN INDICATION. REPLACED LANDING GEAR RELAY BOX WHICH WAS CHATTERING IAW MM 32-31 -02. S/N ON: 120071R AND S/N OFF: 120119. OPS CHECK GOOD.
Part: SIGN — INOPERATIVE (CABIN) · airframe 30,251 hrs · 36,609 cycles
RIGHT EMERGENCY EXIT SIGN LIGHT IS INOP. RESECURED WIRES, OPS CHECK GOOD.
Earlier reports · 1995–1999 · 22 reports
1999
Part: DOOR — NOT LATCHED (FUEL SYST)
AIRCRAFT RETURNED TO FIELD FOR SERVICE DOOR LIGHT. SECURED LATCH ON INBOARD FUEL DOOR. NO OTHER APPARENT DAMAGE OR DEFECTS, OPS GOOD.
Part: ACTUATOR — FAILED (LT TE FLAP)
ON CLIMB-OUT GOT A NACELLE FLAP DISAGREEMENT. RESET UNSUCCESSFUL. RETURNED TO RDD. REPLACED LEFT NACELLE FLAP ACTUATOR IAW EMB 120 MM 27-50-03. OPS CHECK GOOD.
Part: CONNECTOR — DIRTY (TE FLAPS)
FLAP CONTROL FAULT CAME ON AFTER TAKEOFF AND WOULD NOT RESET. RETURNED TO SLC. CLEANED FLAP ACTUATOR CANNON PLUGS. COULD NOT DUPLICATE ON GROUND. OPS CHECKED GOOD.
Part: FUEL PUMP — MALFUNCTIONED (LT ENGINE)
AFTER TAKEOFF LEFT ENGINE LOST POWER, RPM AND NP FOR MAYBE 5 SECONDS THEN RPM AND TQ SURGED FOR ABOUT 4 MORE SECONDS. RETURNED TO SLC. REMOVED AND REPLACED LEFT ENGINE FUEL PUMP AND HMU IAW MM 73-21-00. OPS AND LEAKS CHECKS GOOD.
1998
Part: OUTFLOW VALVE — FAILED (CABIN)
CABIN DEPRESSURIZED WHILE CLIMBING OUT OF 13,000 FT AND WAS UNABLE TO CONTROL IT MANUALLY. RETURNED TO FIELD. SECURED OUTFLOW VALVES IN OPEN POSITION IAW MEL 21-30-01. REMOVED AND REPLACED ELECTRO-PNEUMATIC OUTFLOW VALVE. OPS CHECKS GOOD IAW 21-33-00.
1997
Part: ACTUATOR — FAILED (RUDDER)
RIGHT RUDDER TRAVEL IS RESTRICTED IN FLIGHT WITH YAW DAMPER OFF. REPLACED RUDDER A ACTUATOR IAW MM 27-20-00. OPS CHECK GOOD WITH NO LEAKS NOTED.
Part: FLOORBEAM — CORRODED (CABIN)
FORWARD CENTER OMEGA FLOORBEAM CORRODED PAST SERVICEABLE LIMIT. INSTALLED NEW FORWARD CENTER OMEGA FLOORBEAM, SRM 51-00-00.
Part: SILL — CORRODED (CABIN)
RIGHT FORWARD CABIN SILL HAS HEAVY CORROSION. REMOVED CORRODED RIGHT FORWARD CABIN SILL THRESHOLD AND REPLACED WITH A NEW THRESHOLD SILL, IAW SRM 51-40-00.
Part: STRAP — CORRODED (FUSELAGE)
RIGHT BUTT STRAP UNDER LAVATORY CORRODED BEYOND LIMITS. REMOVED CORRODED BUTT STRAP RIGHT SIDE UNDER LAVATORY AND REPLACED WITH A NEW BUTT STRAP IAW MM 51-40-00.
Part: SEAT TRACK — CORRODED (CABIN)
LEFT SEAT TRACK HAS INTERGRANULAR CORROSION AT NUMEROUS SCREWS HOLES. REMOVED AND REPLACED THE LEFT SEAT TRACK WITH NEW IAW SRM 51-40-02.
Part: ANTENNA — CORRODED (FUSELAGE)
THIRD BELLY ANTENNA AFT IS SHOWING SIGNS OF CORROSION. REMOVED THIRD BELLY ANTENNA AFT CLEANED CORROSION AND REPLACED ANTENNA.
Part: STRAP — CORRODED (FUSELAGE)
LEFT BUTT STRAP UNDER GALLEY AND ENTRY CORRODED BEYOND LIMITS. REMOVED AND REPLACED LEFT BUTT STRAP UNDER GALLEY IAW SRM 51-40-02.
Part: SILL — CORRODED (CABIN)
FORWARD CABIN FLOOR SILLS LEFT AND RIGHT HAVE HEAVY CORROSION. REMOVED AND REPLACED LEFT FORWARD CABIN SILL IAW SRM 51-40-00.
Part: SEAT TRACK — CORRODED (CABIN)
RIGHT SEAT TRACK HAS INTERGRANULAR CORROSION AT NUMEROUS SCREW HOLES. REMOVED AND REPLACED RIGHT SEAT TRACK IAW SRM 51-00-00.
Part: FLOORBEAM — CORRODED (BS 6467)
LEFT OMEGA BEAM IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED LEFT OMEGA BEAM FROM COCKPIT TO FS 6467.6 IAW SRM 51-40-02.
Part: STRAP — CORRODED (FUSELAGE)
FORWARD CENTER BUTT STRAP (SHORT WIRE BUTT STRAP) CORRODED. REPLACED FORWARD CENTER BUTT ON STRAP ON CENTER FORWARD CABIN IAW SRM 51-40-02.
Part: STRAP — CORRODED (CABIN)
FORWARD CENTER BUTT STRAP, AFT OF SHORT WIDE CENTER BUTT STRAP IS CORRODED. REPLACED CENTER BUTT STRAP IN FORWARD PART OF CABIN IAW SRM 51-40-02.
Part: NP INDICATOR — FAILED (LT ENGINE)
OUT OF 15,000 FEET AND CLIMBING, LEFT NP INDICATION BOTH ANALOG AND DIGITAL BECAME ERRATIC THEN DROPPED TO ZERO. ON DESCENT, INDICATIONS RETURNED TO NORMAL THEN BECAME ERRATIC AGAIN THROUGH 8,000 FT. RETURNED TO LAX. REPLACED NR 1 NP INDICATOR AND RAN LEFT ENGINE FOR 30 MINUTES AT DIFFERENT SPEED SETTINGS, NP INDICATIONS OPS CHECKS GOOD.
1996
Part: GEAR LIGHT — MALFUNCTIONED (NLG)
AFTER TAKEOFF WITH GEAR HANDLE IN UP POSITION, SYSTEM -A+ GEAR POSITION INDICATION LIGHT FOR NOSE GEAR STAYED ILLUMINATED. SYSTEM -B+ LIGHT SHOWED NORMAL OPERATION. DID NOT CONCUR WITH -A+ SYSTEM. LOW RUMBLE HEARD FROM ENGINE DURING RETRACT PERIOD. INSPECTED NOSE LANDING GEAR IAW WITH MM 32. PERFORMED SEVEN GEAR SWINGS. NO DEFECT NOTED, ALL CHECKS GOOD.
1995
Part: CONNECTOR — FAILED (TE FLAPS)
FLAPS WILL NOT SET AT 15 DEGREES FOR TAKEOFF. SHOWS SWS FAILURE. WILL NOT RESET. REPLACED RIGHT OUTBOARD FLAP ACTUATOR AND CANNON PLUG. OPERATED FLAPS APPROXIMATELY SIX TIMES AT EACH INTERIM. FLAPS OPERATIONALLY CHECKS GOOD. LEAK CHECKS GOOD.
Part: ANNUNCIATOR — FAILED (TE FLAPS)
CONTROL FAULT ON OUTBD FLAP. CONTROL FAULT WILL NOT RESET. CHECKED CONNECTOR AT OUTBOARD ACTUATORS. FOUND GOOD. CYCLED FLAPS AND RECEIVED A CONTROL FAULT (INTERMITTENTLY) WITH OUTBOARD SEGMENTS FLASHING. RESET USING OVERRIDE SWITCH. SUSPECT BAD ANNUNICATOR PANEL. REPLACED FLAP ANNUNCIATOR PANEL ASSEMBLY. OPERATED FLAPS TEN TIMES. OPS CKS GOOD.
Part: FUEL CONTROL — MALFUNCTIONED (RT ENGINE)
RIGHT EEC CAUSES POWER SURGES ON THE RIGHT ENGINE. DEFERRED PER MEL 73-21-1. RAN THE RIGHT ENGINE, CND. PERFORMED HMU SOL TEST IAW MM OK. CHECKED EEC HARNESS AND INPUTS IAW SL 120-072-0001 EMB EEC TS GUIDE. NO DISCREPANCIES NOTED. SWAPPED LEFT AND RIGHT NH SENSORS FOR TS. RAN ENGINES. OPS CHECKS GOOD AT THIS TIME.