N122SA
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.
3 reports on file, 1999-02-03 – 2003-08-27.
Part: CONNECTOR — ARCED (COCKPIT) · airframe 24,689 hrs · 28,604 cycles
PILOT REPORTED DURING CRUSE FLT SMOKE ENTERED COCKPIT FROM AC ELECTRICAL PANEL AREA. NO SYSTEM MALFUNCTION WAS NOTED. NO ELECTRICAL POWER WAS LOST. ONCE ON GROUND DC POWER COULD NOT BE TURNED OFF THROUGH NORMAL SWITCHING. BATTERY WAS DISCONNECTED TO REMOVE DC POWER FROM AIRCRAFT. MAINTENANCE HAS DISCOVERED THAT SMOKE CAME FROM CONNECTOR J31, LOCATED IN LEFT OVERHEAD PANEL IN COCKPIT. CAUSE IS STILL UNDER INVESTIGATION.
Part: FILTER — LOOSE (NLG)
DURING CRUISE FLIGHT FROM GCN-LAS, FLIGHT CREW REPORTED HYDRAULIC PRESSURE FELL TO ZERO AND EMERGENCY PUMP DID NOT WORK EITHER. AN EMERGENCY WAS DECLARED TO ATC AND A SUCCESSFUL LANDING WAS MADE. COMPANY MAINTENANCE PERSONNEL FOUND HYDRAULIC FLUID LEAKING AT THREADED UNION OF NOSE WHEEL STEERING ACTUATOR AND ACTUATOR FILTER. HELICOIL THREADS IN ACTUATOR PORT APPEARED TO NOT PROVIDE ADEQUATE THREAD ENGAGEMENT TO FILTER ASSY. ACTUATOR WAS REPLACED. (M)
Part: HINGE — LOOSE (RT ELEVATGOR)
DURING SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND RT ELEVATOR HINGE PLATE RIVET FASTENERS WORKING LOOSE IN STABILIZER END RIB. UPON RFEMOVAL OF RT ELEVATOR TO ALLOW REPAIR, FOUND RIVETS PULLED THROUGH ELEVATOR BOTTOM OUTBOARD AND TRAILING EDGE SKINS. REPAIRS WERE ACCOMPLISHED BY REPLACEMENT OF DAMAGED PARTS.