N915FG
Registered owner: FGF SOVEREIGN LLC, TX (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
THE FLIGHT CREW REPORTED LEFT HYDRAULIC LOW PRESSURE MESSAGE IN FLIGHT. THE FLIGHT WAS DIVERTED AND LANDED WITHOUT INCIDENT. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THE LEFT HYDRAULIC PUMP WAS DEFECTIVE. THE PUMP WAS REMOVED AND REPLACED THE HYDRAULIC PUMP AND FILTERS AS REQUIRED. OPS CHECKS AND LEAK CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.
THE FLIGHT CREW REPORTED THAT THE RIGHT SUPPLY BLEED LEAK INDICATOR ILLUMINATED. WAS UNABLE TO CLEAR THE FAULT PER CHECKLIST. THE MAINTENANCE VENDOR TROUBLESHOT AND INSTALLED NEW ORING ON COMPRESSOR OUTLET DUCT. OPS CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE .
LEFT WINDOW IN COCKPIT CRACKED DURING FLIGHT
CORROSION WAS FOUND AT MULTIPLE SITES ON THE VERTICAL STABILIZER REAR SPAR CAPS. AFTER BLENDING, THE REMAINING THICKNESS AT EACH SITE WAS MEASURED USING ULTRASOUND. ALL CORROSION DAMAGE WAS REMOVED BY BLENDING AND CESSNA ENGINEERING ISSUED A REPAIR DEFINITION AND APPROVAL FOR REMAINING THICKNESS TO REMAIN IN SERVICE. FINAL METAL TREATMENT WAS CARRIED OUT USING ALODINE, PRIMER AND TOP COAT.
DURING INSPECTION, THE VERTICAL STEM OF THE LOWER REAR SPAR CAP AFT ANGLE - RH OF THE REAR SPAR ASSEMBLY WAS FOUND TO BE CORRODED AT ABOUT CWS 325 WITH .078" REMAINING THICKNESS ON THE WEB STEM FLANGE. REPAIR DEFINITION WAS RECEIVED FROM CESSNA ENGINEERING TO REPAIR CORRODED AREA BY BLENDING / ALODINE TREATMENT / PRIMER APPLICATION. REPLACEMENT OF RIVETS WERE NECESSARY UPON REASSEMBLY WITH NEW RIVETS.\ IN THE AREA
DURING A SCHEDULED INSPECTION, MICROBIAL GROWTH WAS FOUND IN THE CENTER TANKS. AFTER CLEANING THE TANKS, CORROSION WAS FOUND ON THE LOWER SKIN AND CONNECTING STRUCTURE.
GEAR UNLOCK LIGHT STAYS ON AFTER GEAR RETRACTION. CYCLED GEAR & LIGHT EXTINGUISHED.
AT 11,000 FEET & 40 MILES FROM HOU. THERE WAS A POP SOUND WITH AN AMBER CAS MESSAGE OF ACM BLEED LEAK & A BLUE CAS MESSAGE BAGGAGE HEAT OFF. A FEW SECONDS LATER THERE WAS THE SMELL OF SMOKE IN THE COCKPIT. NEVER SAW THE CAS MESSAGE FOR EMERGENCY PRESSURIZATION ON.