Awesome Flight, LLC.
Also recorded as: Awesome Flight, LLC.
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
No NTSB accidents or incidents linked to this operator.
FAA enforcement actions
No FAA enforcement actions linked to this operator.
Maintenance disclosure history
Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal. To verify a report, search its control number at the FAA SDRS site.
Reports span 2012–2025. Most-reported systems: Communications (23) — 1; Main rotor drive (63) — 1; ATA 85 — 1. Most-common natures of condition, as filed: OTHER — 1; VIBRATION/BUFFET; FLT CONT AFFECTED — 1; VIBRATION/BUFFET; PARTIAL RPM/PWR LOSS — 1.
3 reports on file.
Part: ELECTRONIC UNIT — CORRODED (ZONE 200) · airframe 41,625 hrs · 49,523 cycles
RIGHT ACP NOT WORKING AND STUCK MIC DURING CRUISE, FLIGHT CREW RETURNED TO BASE. R & R REMOTE ELECTRONIC UNIT IAW WITH SAAB 340 AMM 23-50-05-04, OPS TEST SATISFACTORY.
Part: CLUTCH ACTUATOR — CRACKED · airframe 3,138 hrs
FAILURE OF ACTUATOR ASSEMBLY. THE BRACKETS DISCONNECTING THAT CAUSED THE UPPER BREAK.â MR. WEBSTER ALSO STATED THIS WAS A âMAINTENANCE ISSUE THAT SHOULD HAVE BEEN ADDRESSED. WE HAVE A SERVICE BULLETIN OUT JUST FOR THAT.â HOWEVER, UNDER THE CURRENT SERVICE BULLETIN 94 THE INSPECTION REQUIREMENT WAS ONLY DUE TO BE INSPECTED âAT THE NEXT 100-HOUR INSPECTION OR ANNUAL INSPECTION, WHICHEVER OCCURS FIRST.â IT IS IMPORTANT TO NOTE THAT WHEN THIS SERVICE BULLETIN WAS PUBLISHED THE HELICOPTER WAS NOT YET DUE FOR ITS NEXT 100-HOUR INSPECTION. THE FAILURE OCCURRED PRIOR TO THE NEXT 100 HOUR INSPECTION WHICH WAS DUE IN 13 HOURS.
Part: INTAKE VALVE — FRACTURED (ENGINE CYLINDER) · airframe 1,261 hrs
REMOVAL OF THE NR 1 CYLINDER FOR VISUAL INSPECTION REVEALED A FAILURE OF THE INTAKE VALVE. ENGINE MONITOR SHOWED MASSIVE INGESTION OF ENGINE OIL INTO REMAINING CYLINDERS CAUSING LOSS OF POWER FROM OIL FOULING OF UNAFFECTED SPARK PLUGS. AFFECTED CYLINDER SHOWED CATASTROPHIC DAMAGE TO PISTON AND COMBUSTION AREA FROM MULTIPLE PHYSICAL CONTACT. VALVE FURTHER FRACTURED AND PARTS BECAME WEDGED IN THE INDUCTION TUBE AS WELL AS THE COMMON MANIFOLD AREA. WHEN THE INTAKE ROCKER ASSEMBLY WAS REMOVED ALONG WITH THE CAP, DISCOVERED THE TOP OF VALVE, ABOVE VALVE KEYS WAS THE AREA OF SEPARATION AND FAILURE. VISUAL INSPECTION WITH A 30X MICROSCOPE, MECHANIC'S CONSIDERED OPINION THAT THE FAILURE OF THE INTAKE VALVE MAY HAVE BEEN CAUSED FROM A STRESS RISER CREATED DURING MANUFACTURING AT EITHER THE MACHINING, HEAT TREATING PROCESS, OR PERHAPS WAS AT A MOLECULAR LEVEL DURING THE CREATION OF THE RAW MATERIAL. IT SHOULD BE DULY NOTED THAT THE AIRCRAFT WAS IN COMPLIANCE WITH SERVICE BULLETIN SB388C EXACTLY 85.8 HOURS EARLIER AND NO DEFECT OR ABNORMALITIES WERE NOTED AT THE TIME OF THE INSPECTION.
Linked aircraft
| N-number | Make / model | Year | Status | Link basis |
|---|---|---|---|---|
| N326AG | ROBINSON HELICOPTER CO R66 | 2014 | Valid Registration | Matched by certificate designator |
Aircraft with earlier records under this certificate
Maintenance and accident records on this page also cover aircraft that are not in this operator's current FAA fleet list. Charter and management fleets change — owners switch management companies, sell, or export aircraft. Where the registry shows what became of a tail, it is noted below.
- N188DD — records 2012–2017 · no longer on the FAA registry