Owner type
Government
Serial number
7184
Year built
2011
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
July 25, 2011
Certificate issued
February 16, 2012
Expires
February 29, 2028
Mode S code
A16F99

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 98

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1985In forceSuperseded2026
ADs by the year they took effect: 141 ADs
19851
19902
19991
20003
20012
20026
20038
20043
20052
20063
20076
20081
20092
20109
20114
20125
201311
20147
20154
20162
20175
20186
20193
20205
202116
20227
20232
20241
20254
202610
See all 144 ADs

Information bulletins that may apply · 9

Advisory, not mandatory.

Historical bulletins · 2

NTSB investigations

No NTSB investigations matched to N192AMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on American Eurocopter AS350B3 aircraft

FAA incident reports

No FAA accident or incident reports matched to N192AMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on American Eurocopter AS350B3 aircraft

Service difficulty reports · 5

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2012FA0000226Sensor · misinstalledINTERMITTENT FLUCTUATIONS ON NR GAUGE DURING OPERATION. FOLLOWED TROUBLESHOOTING STEPS AND FOUND NR TACH SENSOR TO BE IMPROPERLY SHIMMED BY MFG CAUSING CONTACT OF THE SENSOR AND THE PICK UP TEETH ON THE MAIN ROTOR MAST, DAMAGING THE NR TACH SENSOR AND MAIN ROMar 9, 2012 · N192A · Snias AS350B3 · Rotor Drive Indicating SystemSDR 2012FA0000078Connector · misinstalledLIGHT FOUND TO BE INOPERATIVE. FOUND PINS AT CONNECTOR TO NOT BE CRIMPED AND WIRES LOOSE. RECOMMEND IMPROVEMENT IN QC DURING INSTALLATION.Jan 19, 2012 · N192A · Snias AS350B3 · Light System WiringSDR 2012FA0000075Light · misinstalledLIGHT FOUND TO BE INOPERATIVE. FOUND PINS AT CONNECTOR TO NOT BE CRIMPED AND WIRES LOOSE. RECOMMEND IMPROVEMENT IN QC DURING INSTALLATION.Jan 19, 2012 · N192A · Snias AS350B3 · Exterior LightingSDR 2012FA0000074Ground Wire · brokenPITOT LIGHT ON CAUTION PANEL NOT FUNCTIONING. FOUND GROUND WIRE FOR THE PITOT LIGHT CIRCUIT TO BE BROKEN. WIRE DID NOT HAVE THE SLACK REQUIRED WHEN INSTALLED, PLACING A STRAIN ON THE WIRE WHICH BROKE DURING OPERATION OF THE ACFT. RECOMMEDN IMPROVEMENTS IN QJan 19, 2012 · N192A · Snias AS350B3 · Ice/Rain Protection System WiringSDR 2012FA0000073Magnetic Seal · leakingOIL FOUND ON ENGINE DECK DURING ALF CHECK. LEAK WAS DETERMINED TO COME FROM THE FRONT MAGNETIC SEAL OF THE FREEWHEEL SHAFT. LEAK RATE WAS MEASURED AT 11.94 ML/H. MAX LEAK RATE ALLOWED IS 10 ML/H AS SPECIFIED IN MFG TROUBLESHOOTING BOOK 71-00-06-816-804-B01.Jan 19, 2012 · N192A · Snias AS350B3 · Engine/Transmission Coupling

STCs that may be installed · 401

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 401 STCs