N188JB
Registered owner: LEEDERS CONSTRUCTION LLC, NM (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.
2 reports on file, 2014-01-24 – 2014-04-28.
Part: PRECOOLER — RUPTURED (BLEED AIR SYS) · airframe 2,645 hrs · 2,167 cycles
DURING CLIMBOUT, ENROUTE, OPERATING UNDER A PART 91, THE PILOT NOTICED AN ITT SPLIT OF AROUND 70 DEGREES BETWEEN THE LT & RT ENGINES, LT BEING ABNORMALLY HIGH. THE PILOT RETARDED THE LT ENGINE AND SHUTDOWN. ACFT DIVERTED. EVIDENCE WAS FOUND OF AN OVERHEAT IN THE LT PYLON AREA. ON CLOSER INSPECTION IT WAS FOUND THAT THE LT BLEED AIR PRE-COOLER IN THE PYLON HAD RUPTURED.
Part: PRECOOLER — RUPTURED (ZONE 400) · airframe 2,614 hrs · 2,145 cycles
ON ARRIVAL, SOME DISCOLORATION, MISSING PAINT WAS NOTED ON THE RT ENGINE PYLON. ON FURTHER INVESTIGATION IT WAS FOUND THAT THE PRE-COOLER HAD RUPTURED IN THE PYLON CAUSING SEVERE HEAT DAMAGE TO THE SURROUNDING STRUCTURE AND PYLON, FUSELAGE SKINS. IT WAS DETERMINED BY ENGINEERING THAT THE ENGINE SUPPORT BEAMS AND MOUNTS HAD NOT SUFFERED ANY DAMAGE AND THAT THE ACFT WOULD BE SAFE FOR A 1 TIME FERRY TO FOR REPAIRS. THE ONLY ANOMALY NOTED BY THE FLIGHT CREW WAS AN ITT SPLIT OF 50 DEGREES. THERE IS NO OVERHEAT DETECTORS IN THE PYLONS ON THE CJ2.