N985SA

No registry detail on file · not in current registry

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
Safari Aviation, Inc. (XSFA)Operatoron 2019-12-26Operator named in NTSB report
Safari Helicopter, Inc.Operatoron 2001-02-01Operator named in NTSB report

Accident & incident history

Accident · 2019-12-26 Operator named in NTSB report
AIRBUS AS350B2 Fatal injury Part 135Safari Aviation, Inc.

Operated by Safari Aviation Inc. (per NTSB report)

Source: NTSB case ANC20MA010
Accident · 2001-02-01 Operator named in NTSB report
Eurocopter AS-350-B2 Minor injury Part 135Safari Helicopter, Inc.

Operated by Safari Helicopter, Inc. (per NTSB report)

Source: NTSB case LAX01LA083

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, 2000-06-06 – 2013-10-05.

SMOKE/FUMES/ODORS/SPARKS · 2013-10-05 Matched by certificate designator
ATA 3422

Part: GYRO — FAILED (DIRECTIONAL) · airframe 15,732 hrs · 21,122 cycles

PILOT REPORTED AN ELECTRICAL TYPE BURNING ODOR FOLLOWED BY LIGHT WISPS OF SMOKE FROM UNDER THE INSTRUMENT PANEL HOOD. FLIGHT WAS ABORTED, AND A PRECAUTIONARY LANDING WAS MADE, WHERE THE ACFT WAS SHUTDOWN AND REMOVED FROM SERVICE. UPON FURTHER INSPECTION BY MAINTENANCE IT WAS DETERMINED THE DIRECTIONAL GYRO HAD OVERHEATED. THE AFT COVER OF THE DIRECTIONAL GYRO HAD CRACKED ALLOWING OVERHEATED GREASE TO SEEP FROM THE CASE. IT WAS DETERMINED THAT THE GREASE WAS THE SOURCE OF THE ODOR, AND WAS PRESUMED TO BE THE SOURCE OF THE LIGHT SMOKE. INSPECTION OF ALL THE OTHER INSTRUMENT SYS REVEALED NO OTHER DAMAGE. THE DIRECTIONAL GYRO WAS DISABLED, AND THE ACFT WAS GROUND RUN WITH ALL SYSTEMS RUNNING FOR APPROXIMATELY 15 MINUTES. ALL SYSTEMS FUNCTIONED NORMAL, WITH NO FURTHER INDICATION OF ODOR, OR SMOKE. A SHORT MAINTENANCE FLIGHT WAS CONDUCTED TO RETURN THE ACFT TO BASE. ALL SYSTEMS FUNCTIONED NORMAL, WITH NO PROBLEMS NOTED. A SERVICEABLE DIRECTIONAL GYRO WAS INSTALLED, AND THE ACFT WAS RETURNED TO SERVICE.

Source: SDR XSFA201310170001
FLUID LOSS · 2000-06-06 Matched by certificate designator
ATA 6320

Part: SEAL — LEAKING (MAIN ROTOR INPUT)

INPUT SEAL, MAIN ROTOR GEARBOX, LEAKING POST LIP. (X)

Source: SDR 20000717SH018