N6NY
Registered owner: LJ ASSOCIATES INC, PA (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
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.
10 reports on file, 2014-07-22 – 2025-08-29.
Part: WINDOW FRAME — CORRODED (ZONE 200) · airframe 2,820 hrs · 2,492 cycles
DURING COMPLIANCE WITH SB525C-56-01 CORROSION FOUND ON ALL WINDSHIELD FRAMES AND SURROUNDING STRUCTURE REQUIRING REPLACEMENT OF ALL COCKPIT WINDSHIELD FRAMES AND ATTACHING SKINS.
Part: ACTUATOR — DRAGGING (ZONE 300) · airframe 2,064 hrs · 1,659 cycles
NOTICEABLE YAWING WITH SMALL DISPLACEMENT BUMPS LEFT & RIGHT WITH AUTOPILOT ON OR OFF. INSPECTION FOUND RUDDER BIAS ACTUATORS DRAGGING AND SEALS NEEDED CLEANED AND LUBRICATED.
Part: PIN — OUT OF ADJUST (TRIM INDICATOR) · airframe 7,776 hrs · 7,726 cycles
AFTER TAKEOFF AIRCRAFT AGGRESSIVELY PITCHED UP AND REQUIRED ELEVATOR TRIM MORE THAN USUAL TO LEVEL AIRCRAFT. THE DECISION WAS MADE TO LAND FOR MAINTENANCE AND THE AIRCRAFT RETURNED TO ITS HOME BASEE. AFTER INSPECTING THE AIRCRAFT IT WAS FOUND THAT THE PITCH TRIM WHEEL INDICATOR PIN WAS LOOSE AND OUT OF ADJUSTMENT. ADJUSTED AND SECURED AS NECESSARY.
Part: SWITCH — OUT OF LIMITS (ENGINE A/I) · airframe 7,589 hrs · 7,497 cycles
DURING TROUBLESHOOTING OF THE ANTI-ICE SYSTEM, THE ENGINE ANTI-ICE TEMP SWITCH WAS FOUND OUT OF LIMITS ON THE INDICATION. THE SWITCH WAS REPLACED WITH NEW.
Part: SWITCH — INACCURATE (WING ANTI ICE) · airframe 7,589 hrs · 7,497 cycles
DURING TROUBLESHOOTING, THE WING LEADING EDGE LOW TEMP SWITCH WAS INACCURATE AND REPLACED WITH NEW.
Part: SENSOR — FAULTED (LT WING A/I) · airframe 7,589 hrs · 7,497 cycles
WING ANTI-ICE SYSTEM TROUBLESHOOTING SHOWING THAT THE TEMP SENSOR WAS SHOWING OPEN WHEN IN FACT IT SHOULD HAVE BEEN CLOSED, FAULTY SENSOR AND REPLACED WITH NEW PART.
Part: SENSOR — FAULTY (WING TEMP) · airframe 7,589 hrs · 7,497 cycles
AFTER TAKEOFF, THE ANTI-ICE SYSTEM WAS ON AND THE RIGHT SIDE ENGINE & WING ANTI-ICE ANNUNCIATOR LIGHT WOULD NOT EXTINGUISH. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND THE WING TEMP SENSOR WAS AT FAULT.
Part: UNLOCK SWITCH — OUT OF TOLERANCE (THRUST REVERSER) · airframe 7,519 hrs · 7,406 cycles
AFTER TAKEOFF AND IN CLIMB WHILE RETRACTING THE FLAPS TO ZERO THE RIGHT ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED, THE EMERGENCY STOW SWITCH WAS ACTIVATED AND THE SYSTEM WORKED CORRECTLY. THE ARM LIGHT CAME ON AND THE UNLOCK LIGHT EXTINGUISHED. THE CHECKLIST WAS FOLLOWED AND THE AIRCRAFT DIVERTED TO KLBE AND LANDED WITHOUT INCIDENT. TROUBLESHOOTING DETERMINED THAT THE FAULT WAS WITH THE THRUST REVERSER STOW LIMIT SWITCH.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 6,428 hrs · 6,259 cycles
REJECTED TAKEOFF DUE TO BRIEF BATTERY OVER TEMP LIGHT. INSPECTION PERFORMED OF LEAD ACID BATTERY INSTALLATION & FOUND WITHIN LIMITATIONS. FOUND ZONE WARM DUE TO EXTENDED GND OPERATION WITH ADJACENT FREON AIR CONDITIONING SYS UNDER HIGH AMBIENT TEMPERATURES. OPENED AREA TO ALLOW COOLING, NO FURTHER MALFUNCTIONS. AFM EMER PROCEDURES FOR BATTERY OVER TEMP NOT APPLICABLE DUE TO LEAD ACID BATTERY INSTALLATION.
Part: WARNING LIGHT — FALSE ACTIVATION (BATTERY) · airframe 6,428 hrs · 6,259 cycles
REJECTED TAKEOFF DUE TO BRIEF BATTERY OVER-TEMP LIGHT AT INITIAL POWER UP. RESOLUTION, INSPECTION PERFORMED ON LEAD ACID BATTERY INSTALLATION AND FOUND ZONE WARM DUE TO EXTENDED GROUND OPERATION WITH ADJACENT FREON AIR-CONDITIONING UNIT UNDER HIGH AMBIENT TEMPERATURES. OPENED AREA TO ALLOW COOLING, SYSTEM CHECKED OK. NO FURTHER MALFUNCTIONS. AFM EMERGENCY PROCEDURES FOR BATTERY OVER-TEMP NOT APPLICABLE TO LEAD ACID BATTERY INSTALLATION.