N499SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| STINGER WELDING INC | Operator | on 2012-12-19 | Operator named in NTSB report |
Accident & incident history
Operated by STINGER WELDING INC (per NTSB report)
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.
20 reports on file, 2001-06-11 – 2003-08-24.
Part: FUEL CONTROL — MALFUNCTIONED (LT ENGINE) · airframe 8,320 hrs · 6,773 cycles
ON FINAL APPROACH TO SLC, HAD LEFT ENGINE OIL PRESSURE MESSAGE ON EICAS. SHUT DOWN THE LEFT ENGINE PER THE QRH AND CONTINUED IN TO SLC. INSTALLED LEFT FUEL CONTROL PER RII 73-401.
Part: DRAIN LINE — LEAKING (HYD SYSTEM) · airframe 8,114 hrs · 6,610 cycles
AFTER T/O AT APPROX 22,000 FT, TOTAL LOSS OF HYDRAULIC PRESSURE & FLUID NR 1. RETURNED TO SLC WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NR 1 HYDRAULIC CASE DRAIN LINE. OPS AND LEAK CHECK GOOD. P/N: 601-75238-5
Part: SELECTOR VALVE — MALFUNCTIONED (ANTI SKID SYS) · airframe 7,536 hrs · 6,173 cycles
UPON TAKEOFF, RECEIVED ANTI-SKID INBOARD CAUTION MSG FOLLOWED BY A GEAR DISAGREE WARNING AND PARKING BRAKE SOV CAUTION. FOLLOWED QRH PROCEDURE AND RETURNED TO THE AIRPORT.REMOVED AND REPLACED MLG SELECTOR VALVE IAW MM 32-32-10. OPS CHECK GOOD. LEAK CHECK GOOD.
Part: ACTUATOR — FAILED (HORIZONTAL STAB) · airframe 6,924 hrs · 5,711 cycles
STAB CH 1 WILL ENGAGE BUT DISCONNECTS WHEN THE TRIM SWITCH IS ACTIVATED. REMOVED AND REPLACED MOTOR CONTROL AND TRIM ACTUATOR. OPS CHECKED GOOD. P/N: 7062-3, S/N OFF: 138, S/N ON: 777.
Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 6,897 hrs · 5,696 cycles
ENTERING DOWNWIND AT SLC, 11,000 FT, LEFT ENGINE FAILED. RED OIL LOW PRESS WARNING AND YELLOW CAUTION MESSAGES. BELIEVE THE FUEL FLOW WENT TO ZERO. REMOVED AND REPLACED THE LEFT ENGINE WITH A SERVICEABLE UNIT. OPS AND LEAK CHECKS GOOD.
Part: PCU — FAILED (RIGHT SPOILER) · airframe 6,634 hrs · 5,487 cycles
RIGHT OUTBOARD SPOILER PCU FAILED DURING TAXI OUT. REMOVED AND REPLACED RIGHT O/B PCU. OPS CHECK GOOD IAW 27-60-01.
Earlier reports · 2001–2002 · 14 reports
2002
Part: COMPUTER — MALFUNCTIONED (NR 2 AHRS) · airframe 6,422 hrs · 5,319 cycles
FIRST OFFICER'S HEADING KEPT DRIFTING LEFT IN FLIGHT CAUSING EFIS COMP MONITOR CAUTION MESSAGE. FOLLOWED QRH, SWITCHED TO DG MODE AND HEADING KEPT DRIFTING. RETURNED TO DFW. REPLACED NR 2 AHARS COMPUTER IAW 34-21-01. OPS CHECK GOOD.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 4,992 hrs · 4,167 cycles
LEFT JET PIPE OVERHEAT FAIL MESSAGE ON CLIMBOUT FROM LAS AT 27,000 FT. MESSAGE CLEARED, THEN RETURNED. LEFT JET PIPE OVERHEAT SYSTEM OPS CHECK GOOD AT THIS TIME. NO FAULTS FOUND.
Part: WIRE — BROKEN (CABIN) · airframe 4,939 hrs · 4,129 cycles
FORWARD RED FLOOR EMERGENCY LIGHTS INOP. REPLACED WIRE AS NEEDED FOR FORWARD EMERGENCY LIGHTS. OPS CHECK GOOD.
Part: LATCH — FAILED (PAX DOOR) · airframe 4,884 hrs · 4,091 cycles
PASSENGER DOOR INNER HANDLE DISCONNECTED. REMOVED AND REPLACED DOOR LATCH MECHANISM PER MM 52-11-02. CHECKS OK.
Part: FIRE LOOP — MALFUNCTIONED (LT ENGINE) · airframe 4,816 hrs · 4,037 cycles
L JETPIPE OVHT FAIL MESSAGE ILLUMINATED AT FL350. FOLLOWED QRH PROCEDURE, SWITCHED TO LOOP A. MESSAGE DID NOT PERSIST. TEN MINUTES LATER L JET PIPE OVHT WARNING SOUNDED. FOLLOWED EMERGENCY MEMORY ITEMS FOR THIS. THE WARNING EXTINGUISHED AT APPR. 70% N1 AND WE DIVERTED TO PNS FOR A NORMAL LANDING.INSPECTED TAIL PIPE FOR HOT SPOTS. COULD NOT DUPLICATE FAILURE DURING TEST AND RUN UP. PERFORMED CHECK AND INSPECTED WIRES ON LEFT JET PIPE LOOPS. COULD NOT GROUND DUPLICATE PROBLEM. OPS CHECK GOOD.
Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 4,821 hrs · 4,043 cycles
CREW ESCAPE HATCH OUTER HANDLE SEIZED. (DISCOVERED DURING C-CHECK INSPECTION). OUTER HANDLE ASSEMBLY FREED AND FOUND TO BE SEVERELY CORRODED. OUTER HANDLE ASSEMBLY REPLACED PER AMM 52-22-02.
Part: PCU — MALFUNCTIONED (SPOILER) · airframe 4,635 hrs · 3,889 cycles
RECEIVED SPOILERON FAULT STATUS MESSAGE ON TAXI OUT. REMOVED AND REPLACED RIGHT SPOILERON INBOARD PCU PER 27-62-01. OPS AND LEAK CHECK GOOD.
Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 3,773 hrs · 3,225 cycles
APU OIL TEMPERATURE CAUTION MESSAGE. DIVERTED TO KGJT. FOUND ENGINE OIL OVERSERVICED. SERVICED TO PROPER LEVEL. RAN, GROUND TEST GOOD.
Part: OIL COOLER — DIRTY (APU) · airframe 3,867 hrs · 3,298 cycles
APU OIL TEMP CAUTION MSG. DIVERTED FROM SLC TO GJT. CLEANED THE OIL COOLER COOLING FINS. RAN THE APU FOR 30 MINS. OPS CHECK GOOD.
2001
Part: PCU — MALFUNCTIONED (SPOILER) · airframe 3,753 hrs · 3,209 cycles
FLIGHT SPOILERS FAULT MESSAGE ON TAXI OUT. CONSULTED WITH MAINTENANCE. RESET CIRCUIT BREAKERS AS DIRECTED. OPS CHECK GOOD. WHILE ROLLING THE YOKE LEFT DURING FLIGHT CONTROL CHECK, LEFT SPOILERON AND LEFT FLIGHT SPOILER BOTH DEPLOY, RECEIVED A FLT SPOILERS FAULT STATUS MESSAGE. REMOVED AND REPLACED LEFT OUTBOARD PCU. OPS AND LEAK CHECK GOOD.
Part: LEVER — MALFUNCTIONED (SPOILER CONTROL) · airframe 2,791 hrs · 2,452 cycles
ON A TEN MILE FINAL, WHILE RETRACTING FLIGHT SPOILERS, AIRCRAFT ROLLED LEFT AT 1/4 DETENT. FULLY RETRACTING SPOILERS CORRECTED THE PROBLEM.NO FAULTS LOGGED IN MDC OR SECU'S. SPOILER RIGGING CHECKS GOOD. REMOVE AND REPLACE FLIGHT SPOILER CONTROL LEVER IAW CRJ MM 27-61-01. OPS CHECK GOOD.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 2,583 hrs · 2,286 cycles
AFTER LEAVING SLC RECEIVED ON EICAS NR 1 (4 MESSAGES): 1. PITOT BASE HEAT; 2. LEFT AOA HEAT; 3. LEFT STATIC HEAT; 4. LEFT PITOT HEAT.REMOVED AND REPLACED LEFT PROBE HEATERS SENSOR CONTROLLER IAW MM 30-31-15. OPS CHECK GOOD.
Part: SENSOR — FAILED (TE FLAPS) · airframe 2,178 hrs · 1,963 cycles
FLAPS FAIL IN FLIGHT WITH FLAPS UP. REMOVED AND REPLACED RIGHT BRAKE POSITION SENSING UNIT IAW 27-51-10. CHECKS GOOD. COMPLIED WITH AD 98-20-01. P/N: 855D100-9 S/N ON: 303B S/N OFF: 155B
Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 2,102 hrs · 1,903 cycles
FLAPS FAIL CAUTION MESSAGE ENROUTE AT FL 310. ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURE H 8-8. COMPLIED WITH MAINTENANCE PROCEDURE OF AD 98-20-01. FLAPS OPERATED NORMAL AT THIS TIME AND NO DISCREPANCIES NOTED.