N580JS
Registered owner: SOUTHERN AIRCRAFT CONSULTANCY INC TRUSTEE, WY (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
UPON REACHING AN ALTITUDE OF 30,000', PAX DOOR OPEN CAS WARNING MESSAGE ILLUMINATED. DECLARED AN EMERGENCY, STARTED AN EMERGENCY DESCENT AND RAN THE CHECKLIST IN THE QRH. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE OPERATED THE DOOR SEVERAL TIMES AND COULD NOT DUPLICATE THE DISCREPANCY.
PAX DOOR OPEN CAS MESSAGE DISPLAYED IN FLIGHT. SIMULTANEOUS DECREASE IN CABIN PRESSURE. THE CREW EXECUTED AN EMERGENCY DESCENT AND DECLARED AN EMERGENCY. CABIN ALTITUDE NEVER INCREASED ENOUGH TO CAUSE THE OXYGEN MASKS TO DROP. THE CREW PERFORMED A STANDARD CONFIGURATION LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED AN INSPECTION OF THE MED AND SEALS. NO DEFECTS WERE FOUND. MAINTENANCE ALSO PERFORMED A PRESSURIZATION CHECK AND A FUNCTIONAL CHECK OF MED INDICATIONS WITH NO DEFECTS FOUND. FOUND DOOR SUPPORT CABLE KINKED, OPERATED DOOR WITH NO DEFECTS FOUND.
BRAKE FAIL CAS MESSAGE OCCURRED AT 23,000 FT ENROUTE TO 36000 FT CLEARED TO LEVEL OFF AT 24,000. DIVERTED. CREW RAN CHECKLIST FOR THE BRAKE FAIL. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. PERFORMED BRAKE SYSTEM FUNCTIONAL TEST IAW 32-41-00-720-801-A WITH NO FAULTS EXCEPT PEDAL DISPLACEMENTS WERE NOT WITHIN PERCENTAGE RANGE. ADJUSTED NEUTRAL POSITION ON LT AND RT NEUTRAL BRAKE STOPS IAW AMM 32-41-02-820-801-A, AMM 2432, REV 32. PERFORMED FAILURE OF LT BRAKE CONTROL VALVE FIM TASK 32-41-00-810-805-A WITH NO FAULTS FOUND. CVDR DATA SHOWED A VARIATION IN LT BRAKE CONTROL VALVE. REMOVED LT BRAKE CONTROL VALVE, AND REPLACED WITH REPAIRED CONTROL VALVE IAW AMM TASK 32-41-01-000-801-A. REMOVED LT BRAKE CONTROL TRANSDUCER, AND REPLACED WITH NEW TRANSDUCER IAW AMM 32-41-05-000-801-A. PERFORMED NORMAL AND EMERGENCY PARKING BRAKE SYSTEM BLEEDING, PERFORMED MAIN BRAKE SYSTEM FUNCTION TEST AND PERFORMED MAIN HYDRAULIC SYSTEM BLEED OF AIR IAW AMM 2432, REV 32.