N8624B
Registered owner: SUMMIT PEAK HOLDINGS LLC, MT (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
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, 1997-05-13 – 2016-10-08.
Part: CYLINDER — BROKEN
PILOT REPORT A VIBRATION WHILE IN FLIGHT AND LANDED. FURTHER INSPECTION FOUND THAT ONE OF THE COOLING FINS HAD BROKEN OFF. THE COOLING FIN CRACKED IN BETWEEN THE INSTALLATION RIVETS. ABOVE THE RIVET LINE REMAINED ON THE ASSEMBLY AND THE LOWER HALF WAS FOUND INSIDE THE COWLING. THE TOTAL TIME OF THE ASSEMBLY IS NOT KNOW ALONG WITH THE TOTAL TIME OF THE BLADE.
Part: CONTROL CABLE — BINDING (THROTTLE)
THROTTLE CONTROL CABLE INTERNAL BINDING CAUSES PARTIAL TO FULL LOSS OF THROTTLE CONTROL. UNIT IN SERVICE 36 WEEKS.
Part: CONTROL CABLE — BINDING (THROTTLE)
THROTTLE CONTROL CABLE INTERNAL BINDING CAUSES PARTIAL TO FULL LOSS OF THROTTLE CONTROL. UNIT IN SERVICE 12 WEEKS.
Part: UNIVERSAL HSNG — CRACKED (SWASHPALTE)
MOUNTING WEBS FOR CONTROL ROD BEARINGS AND UNIVERSAL JOINT OF LOWER SWASHPLATE FOUND CRACKED AT INSPECTION. THIS IS A PRIMARY FLIGHT CONTROL PART. THIS PART HAS A RETIREMENT LIFE OF 17,700 HOURS. PART NON-REPAIRABLE. REPLACED WITH NEW PART 28-16119-1.
Part: UNIVERSAL HSNG — CRACKED (SWASHPLATE)
MOUNTING WEBS FOR CONTORL ROD BEARINGS AND UNIVERSAL JOINT OF LOWER SWASHPLATE FOUND CRACKED AT INSPECTION. THIS IS A PRIMARY FLIGHT CONTROL PART. THIS PART HAS A RETIREMENT LIFE OF 17,700 HOURS. PART NON-REPAIRABLE. REPLACED WITH NEW PART 28-16119-1.