N932BG
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.
6 reports on file, 2012-05-24 – 2016-12-28.
Part: BLADE — CRACKED (MAIN ROTOR) · airframe 5,029 hrs
A NINE INCH LONG CRACK ON MAIN ROTOR BLADE BETWEEN STATIONS 166 - 173.
Part: FIRE DETECTOR — INOPERATIVE (ENGINE BAY) · airframe 4,325 hrs
AFTER TAKEOFF, THE FIRE WARNING LIGHT ILLUMINATED. ACFT WAS IMMEDIATELY RETURNED AND LANDED WITHOUT EVENT. MAINTENANCE FOUND A BAD FLAME DETECTOR, PN: 92310-04802-105, SN:5853 REMOVED, INSTALLED SN: 4565. THERE WERE NO INDICATIONS THAT A FIRE HAD OCCURRED, ACFT RETURNED TO SERVICE.
Part: FIRE DETECTOR — DEFECTIVE (ENGINE) · airframe 4,325 hrs
12/26/2014 AT APPROX 09:45, ON TAKEOFF, THE FIRE WARNING LIGHT ILLUMINATED. ACFT WAS IMMEDIATELY RETURNED & LANDED WITHOUT EVENT. MX FOUND A BAD FLAME DETECTOR, PN 92310-04802-105, SN REMOVED 5853, INSTALLED SN 4565. THERE WAS NO INDICATION THAT A FIRE HAD OCCURRED, ACFT RETURNED TO SERVICE.
Part: STRINGER — CRACKED (FUSELAGE)
DURING 1250 HOUR INSPECTION, REMOVED BAGGAGE COMPARTMENT HEADLINER AND FOUND STRINGER CRACKED ABOUT 3 INCH LONG. SPOT DRILLED CRACK. FABRICATED DOUBLER. INSTALLED IAW DRB 2013-5A-92-059.
Part: LIFE RAFT — UNWANTED DEPLOY (CABIN) · airframe 1,943 hrs
WHILE PILOT WAS PERFORMING PREFLIGHT CHECKS, THE LIFE RAFT DEPLOYED. VERIFIED THAT SWITCHES WERE IN CORRECT POSITIONS ACCORDING TO ACFT CHECKLIST. S92 TECH REP REVEALED THAT THIS IS AN ISSUE THAT IS KNOWN AND IS CURRENTLY BEING INVESTIGATED. ACCORDING TO THE REPS THE PROBLEM STEMS FROM ELECTRICAL CONNECTORS TO THE SQUIBS WHICH ARE UNACCESSIBLE TO MX TECH. FURTHER INFORMATION HAS BEEN REQUESTED FROM TECH REPS WHEN INFORMATION BECOMES AVAILABLE.
Part: STRUT — FLUID LOSS (LT MLG) · airframe 2,211 hrs
LEFT MAIN GEAR STRUT COLLAPSED AND FLUID ON GROUND.