N139EH
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.
5 reports on file, 2006-12-13 – 2008-09-23.
Part: FIRE WARNING — ACTIVATED (COCKPIT)
IN LEVEL FLIGHT, WHILE CONDUCTING A PT91 FERRY FLIGHT, A NR1 ENGINE FIRE CAS MESSAGE AND AURAL WARNING OCCURRED WITHIN 30 SECONDS. THE NR 2 ENGINE FIRE CAS MESSAGE AND AURAL WARNING SOUNDED, THERE WAS NO OTHER INDICATION OF A FIRE. THE ECL`S FIRE BOTTLE SELECTORS OR THE PMS FIRE LIGHT WERE NOT ILLUMINATED. THE FIRE COULD NOT BE CONFIRMED. SHORTLY AFTER A NR1, NR2 EEC FAILURE, CAS MESSAGE OCCURRED, THERE WAS NO FLUCTUATION OF ENGINE PARAMETERS ON THE ENGINE POWERPLANT PAGE. PILOTS DESCENDED TO MINIMUM SAFE ALTITUDE AND LANDED AT BASE WITHOUT FURTHER INCIDENT. (K)
Part: FIRE WARNING — ILLUMINATED (NR 1 ENGINE)
IN LEVEL FLIGHT WHILE CONDUCTING A PT91 FERRY FLIGHT A NR 1 ENGINE FIRE CAS MESSAGE AND AURAL WARNING OCCURED WITHIN 30 SECONDS THE NR 2 ENGINE FIRE CAS MESSAGE AND AURAL WARNING SOUNDED THERE WAS NO OTHER INDICATION OF A FIRE THE ECL'S FIRE BOTTLE SELECTORS OR THE PMS FIRE LIGHT WERE NOT ILUMINATED THE FIRE COULD NOT BE CONFIRMED SHORTLY AFTER A NR1-NR 2 EEC FAILURE CAS MESSAGE OCCURED THERE WAS NO FLUCTUATION OF ENGINE PARAMETERS ON THE ENGINE POWERPLANT PAGE PILOTS DECENDED TO MINIMUM SAFE ALTITUDE AND LANDED AT BASE WITHOUT FURTHER INCIDENT.
Part: PANEL — DELAMINATED (FUSELAGE) · airframe 1,491 hrs · 2,400 cycles
AFT UPPER DECK BETWEEN STATIONS 7920MM AND 7720MM IS DEBONDED. THE AREA IS APPROXIMATELY 800MM WIDE AND 200MM LONG. WATER WAS FOUND INSIDE THE HONEYCOMB CORE.
Part: PANEL — DELAMINATED (FUSELAGE) · airframe 1,491 hrs · 2,400 cycles
AFT UPPER DECK BETWEEN STATIONS 7920MM AND 7720MM IS DEBONDED.THE AREA IS APPROXIMATELY 800MM WIDE AND 200MM LONG. WATER WAS FOUND INSIDE THE HONEYCOMB CORE.
Part: ATTACH FITTING — CRACKED (TAILBOOM) · airframe 1,065 hrs · 1,605 cycles
DURING ROUTINE INSPECTION FOUND CRACK AT UPPER LT TAILBOOM ATTACHMENT, STATION 8700. THE CRACK EXTENDED FROM A LOCK FASTNERS IN THE SUPPORT STRUCTURE.