- Registered owner
- Phi Aviation LLC
- Location
- Lafayette, LA
- Owner type
- LLC
- Serial number
- 920021
- Year built
- 2005
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- August 31, 2005
- Certificate issued
- December 15, 2022
- Expires
- December 31, 2029
- Mode S code
- A170E6
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 42
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2005 | 1 |
|---|---|
| 2006 | 3 |
| 2007 | 1 |
| 2009 | 4 |
| 2010 | 3 |
| 2011 | 4 |
| 2012 | 4 |
| 2013 | 3 |
| 2014 | 3 |
| 2015 | 2 |
| 2016 | 3 |
| 2017 | 7 |
| 2018 | 1 |
| 2019 | 1 |
| 2020 | 1 |
| 2021 | 5 |
| 2022 | 4 |
| 2023 | 2 |
| 2024 | 2 |
See all 54 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N192PHMatched 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 Sikorsky S-92A aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR HEEA20120808463Wire Harness · damagedNR 2 ENGINE FIRE WARNING LIGHT AND AURAL WARNING CAME ON IN CUISE FLIGHT. LANDING UNEVENTFUL. INSTALLED NEW FLAME DETECTOR AND HARNESS AND COMPLIED WITH SHRINK WRAP MODIFICATION.SDR HEEA20120726365Fire Detector · false activationNR 2 ENGINE INTERMITTENT FIRE WARNING LIGHT WITH AURAL WARNING CAME ON 5 TIMES. LIGHT WENT OUT IMMEDIATELY EACH TIME. MAINTENANCE REPLACED THE NR 2 ENGINE AFT FLAME DETECTOR AND AFT FIRE DETECTION HARNESS, PN 925582-04112-042.SDR HEEA129499Wire Harness · shortedNR 2 ENGINE FIRE LIGHT CAME ON INTERMITTENTLY, NO SECONDARY INDICATIONS. INSPECTED FIRE DETECTION SYS AND FOUND SHORT IN NR 2 ENG AFT FLAME DETECTOR HARNESS.SDR HEEA128373Frame · crackedFOUND CRACKED FRONT FRAME AT 6 O'CLOCK POSITION INSIDE INLET AREA. OIL LEAKAGE SEEMED TO BE CARRIED THROUGH TO THE PARTICLE SEPARATOR BLOWER AND DEPOSITED ON THE TAILBOOM, RATHER THAN INTO THE COMPRESSOR. SENT ENGINE FOR REPAIR.SDR HEEA127544Compressor · failedDURING IFR CRUISE FLIGHT, PASSENGERS REPORTED FUMES IN CABIN. DECLARED "EMERGENCY". PROCEEDED TO DESTINATION. LANDED WITHOUT INCIDENT. MX FOUND THE AIR CONDITIONING COMPRESSOR MOTOR TO HAVE FAILED. REPLACED THE COMPRESSOR PALLET ASSY, PN 92309-04851-108, SDR HEEA126214Fire Warning · false activationDURING TAKEOFF THE NR 2 ENGINE FIRE LIGHT ILLUMINATED. ABORTED TAKEOFF AND LANDED ON THE FLYWAY. TAXIED TO THE PARKING AREA AND NOTIFIED MAINTENANCE. CLEANED CONNECTORS AND INSPECTED SYSTEM. FOUND NO DEFECTS. RAN AIRCRAFT, TESTED SYSTEM AND PERFORMED CHECSDR HEER118276Spar Cap · crackedFORWARD SPAR CAP ANGLE AT TOP OF THE DRIVESHAFT TUNNEL IS CRACKED AT TOP OF THE LAST LARGE HL64-8 PIN. CONTACTED MFG FOR 8110 REPAIR.SDR HEER118215Angle · crackedFWD LT CAP ANGLE CRACKED. REPORTED PROBLEM TO MFG.SDR HEEA111385Seal · leakingOIL PRESSURE WAS NORMAL AFTER TAKEOFF, ABOUT 35 MIN IN CRUISE FLIGHT, NR 2 ENGINE OIL PRESSURE HAD DROPPED TO 55 PSI, THEN ON ARRIVAL, NR 2 ENGINE OIL PRESSURE WAS BETWEEN 47 AND 50 PSI. REPLACED G AXIS SEAL.SDR HEEA107335Line · rupturedNR 2 HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE FOUND NR 2 HYDRAULIC PUMP DISCHARGE HOSE HAD RUPTURED. REPLACED HOSE.
STCs that may be installed · 120
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 120 STCs