N111PX
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.
16 reports on file, 1996-12-23 – 2002-05-17.
Part: TUBE — CRACKED (FLARE)
JUST AFTER ATTAINING V1 SPEED DURING TAKEOFF, THE LEFT ENGINE LOW OIL PRESSURE WARNING ILLUMINATED. THE CLIMB OUT CONTINUED TO SIX THOUSAND FEET AND THE FLIGHT CREW DETERMINED THAT WAS NOT AN INDICATION PROBLEM. THE FLIGHT CREW DECLARED AN EMERGENCY AND PERFORMED AN IN FLIGHT SHUT DOWN OF THE ENGINE IAW THE APPROVED CHECKLIST. THE AIRCRAFT CONTINUED WHERE AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE FOUND A BAD OIL PRESSURE SENSOR OIL LINE. THE LINE WAS REPLACED, THE ENGINE TOPPED OFF WITH OIL AND A GROUND RUN UP WAS PERFORMED. NO OIL FURTHER LEAKAGE WAS NOTED.
Earlier reports · 1996–1999 · 15 reports
1999
Part: HOT LIGHT — ILLUMINATED (LT TAIL PIPE)
LEFT TAIL PIPE HOT LIGHT CAME ON. INVESTIGATED LEFT TAIL PIPE HOT LIGHT ON. CHECKED ENGINE FOR BLEED LEAKS, NONE NOTED. CHECKED WIRING AT TAIL PIPE FOR CHAFFING NONE NOTED. OPS CHECKED GOOD. (M)
1998
Part: FIRE LOOP — MALFUNCTIONED (RT ENGINE)
RIGHT FIRE WARNING ILLUMINATED CWP AND HANDLE. BEGAN SHUT DOWN PROCEDURES, RETARDED POWER LEVER AND LIGHT WENT OUT. FOUND FIRE LOOP ON RIGHT ENGINE COMING IN CONTACT WITH ENGINE HOT SECTION. RE-ROUTED FIRE LOOP, OPS CHECK GOOD. (M)
Part: SEAL — LEAKING (RT ENG GEARBOX)
MCO-SYR - FLT 2226 - AFTER ONE HOUR OF FLT, THE RIGHT ENGINE OIL QTY BEGAN TO DROP FROM 16 QUARTS. THE OIL QUANTITY DROPPED APPROXIMATELY 1 QT PER 10 MINUTES AT CRUISE POWER. ALL OTHER ENGINE GAUGES WERE NORMAL. THE FLT DIVERTED TO ORF. DURING FLT IDLE DESCENT THERE WAS NO NOTICEABLE OIL LOSS. THE FLT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE CSD GARLOCK SEAL. DURING ENGINE RUN THE OIL QTY REMAINED NORMAL. (M)
Part: AIR VALVE — INOP (LEFT)
LEFT AIR VALVE LIGHT ILLUMINATED DURING CLIMB-OUT. REMOVED AND REPLACED LEFT HAND ASIBV. GROUND RUN CHECKS GOOD. (M)
Part: OVERHEAT SENSOR — MALFUNCTIONED (RT ENGINE)
RIGHT TAIL PIPE HOT LIGHT IN FLIGHT. CLEANED AND INSPECTED TAILPIPE SENSORS. NO DEFECTS NOTED ON GROUND RUN-UP. OK FOR SERVICE. (M)
Part: THERMAL CONTROL — FAILED (RT)
RIGHT INTAKE LIGHT COMES ON 5 SECONDS AFTER SWITCHED ON IN FLIGHT. REMOVED AND REPLACED RIGHT ENGINE INTAKE HEAT THERMAL CONTROLLER. (M)
1997
Part: SWITCH — FAILED (COCKPIT)
RETURN TO RAMP WITH ENGINE FIRE INDICATION GOING OFF. REMOVED AND REPLACED OVERHEAD PANEL (TEST 1) FIRE SHORT SWITCH. (M)
Part: CIRCUIT BREAKER — POPPED (RT EFIS SYSTEM)
RETURN TO RAMP WITH RT EFIS SYSTEM INOP. RETURNED TO RAMP AND FOUND CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER, OPS CHECK GOOD. (M)
Part: CIRCUIT BREAKER — TRIPPED (RIGHT)
INTAKE HEAT FAILED ON TAXI CHECK. RESET AIRCRAFT CIRCUIT BREAKER IN RIGHT GEAR WELL. (M)
Part: RUDDER LIMITER — NO LIGHT (RIGHT)
RUDDER LIMIT FEELS LIKE IT IS LIMITING WITHOUT RUDDER LIMIT LIGHT. DEFERRED RUDDER LIMITER. (M)
Part: FITTING — LEAKING (STATIC SYSTEM)
ON CLIMB FOS, ASI AND VSI ALT MALFUNCTIONED. REPLACED STATIC PRESSURE LINE UNION AT VSI ASI T-FITTING. (M)
Part: FIRE LIGHT — ILLUMINATED (COCKPIT)
FIRE DETECT FAIL LIGHT CAME ON. RERACKED WARNING ELECTRONIC UNIT. OPS CHECK GOOD. (M)
Part: BRAKES — WEAK (MLG)
BRAKES WEAK, BRAKE PSI GOOD. RAN AND TAXIED AIRCRAFT. TESTED BRAKE SYSTEM. NO DEFECTS NOTED. FOUND TO BE OK FOR SERVICE. (M)
Part: CONNECTORS — DIRTY (RT TAIL PIPE)
RIGHT TAIL PIPE HOT LIGHT IS ACTIVATED. CLEANED ALL CONNECTORS AND CANNON PLUGS. GROUND RUNS OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE. (M)
1996
Part: AHRS COMPUTER — FAILED (AVIONICS BAY)
HEADING SPLIT, HSI WOULD NOT SLAVE. REMOVED AND REPLACED AHRS AND REPAIRED WIRE ON SLAVE BUTTON. (X)