N119RM
Registered owner: BALD 3 LLC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Hera Flight, LLC (5JHA) | Certificate holder | — | Matched by certificate designator |
| Hera Flight, LLC (5JHA) | Operator | on 2026-05-09 | Operator named in NTSB report |
Accident & incident history
Operated by Hera Flight, LLC (per NTSB report)
Not yet finalized — may be revised.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.
5 reports on file, 2018-02-15 – 2025-03-07.
Part: OVERHEAT SENSOR — FALSE INDICATION (ZONE 400) · airframe 8,380 hrs · 4,742 cycles
THE LH AND RH HYDRAULIC TEMP SENSORS GIVE FALSE INDICATIONS. WE HAVE REPLACED 5 SENSORS IN THE LAST FEW YEARS AND THE LATEST ONE THAT IS BRAND NEW FAILED AFTER TWO WEEKS IN SERVICE.
Part: NONE — NONE · airframe 6,012 hrs · 3,625 cycles
ON TAKEOFF THE CREW SAW THE MAIN CABIN DOOR CAS MESSAGE ILLUMINATE AS WELL AS THE CABIN VENT DOOR CAS MESSAGE. BOTH CAME ON AT 11,000 FEET WHILE DEPARTING ASPEN. THEY RETURNED TO ASPEN AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE INTERIOR CABIN DOOR HANDLE LOOSE. IT WAS TIGHTENED AND OPS CHECK GOOD.
Part: POSITION SENSOR — DEFECTIVE (RUDDER) · airframe 3,631 hrs · 2,272 cycles
DURING FLIGHT CONTROL CHECKS, PRIOR TO FLIGHT, IT WAS DISCOVERED THAT THE UPPER RUDDER CHANNEL B FAILED THE PRE-FLIGHT CHECKS. THE UPPER RUDDER POSITION WOULD STAY FULLY DEFLECTED UNTIL RESET. THE MAINTENANCE FOUND THE CHANNEL B RUDDER POSITION SENSOR DEFECTIVE. THE SENSOR WAS REPLACED AND OPS AND TRAVEL CHECKS WERE NORMAL.
Part: HYDRAULIC LINE — CHAFED · airframe 3,542 hrs · 2,205 cycles
DURING POST FLIGHT INSPECTIONS, THE RT THRUST REVERSER PRESSURE HYDRAULIC LINE WAS FOUND TO BE CHAFED BY NEARBY B-NUT CAUSING A HYDRAULIC LEAK. . THE LOCATION OF THE CHAFED HYDRAULIC LINE WAS WITHIN THE AFT MAINTENANCE BAY ON THE RT SIDE OF THE COMPARTMENT JUST ABOVE AND AFT OF THE WATER SEPARATOR. THE B-NUT WAS LOCATED AFT OF A CHECK-VALVE THE CHAFED HYDRAULIC LINE ROUTES VERTICALLY AFT OF THE WATER SEPARATOR. THE AREA CHAFED IS NOT READILY SEEN AND COULD BE MISSED DURING VISUAL INSPECTION. THE HYD LINE WAS REPLACED AND ADJUSTMENTS WERE MADE TO ACHIEVE CLEARANCE.
Part: SEAL — LEAKING (COCKPIT A/C PACK) · airframe 3,474 hrs · 2,160 cycles
WHILE WAITING FOR PASSENGERS WITH THE APU RUNNING AND THE AIR CONDITIONING OPERATING, THE CREW REPORTED THAT VISIBLE SMOKE WAS SEEN IN THE COCKPIT WITH THE ODORS OF SOMETHING GETTING HOT, WERE UNABLE TO CONTROL THE COCKPIT TEMP. THE CREW SHUTOFF THE COCKPIT AIR CONDITIONING PACK AND THE ODOR AND SMOKE DISSIPATED. TROUBLESHOOTING DETERMINED THAT THE COCKPIT AIR CONDITIONING PACK OIL SEALS FAILED ALLOWING THE AC PACK OIL TO BYPASS. THE PACK WAS REPLACED WITH A NEW UNIT. OPS CHECKED SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.