SUNNYFIELD AVIATION ASSOCIATES, LLC

Part 135 operator · designator YYOA

Data confidence: All records on this page are linked by a shared certificate number or aircraft registration (N-number).

Also recorded as: SUNNYFIELD AVIATION ASSOCIATES, 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

FAA enforcement records haven't been loaded into GroundCheck yet, so none can be shown — a gap in our data, not evidence of a clean enforcement history.

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.

2 reports on file.

K · 2012-01-30 Matched by certificate designator
N232BG · ATA 3230

DURING APPROACH, SELECTED MLG DOWN & IT FAILED TO RESPOND. TRIED SEVERAL TIME TO EXTEND GEAR WITH NO RESULTS. PROCEEDED TO PUMP GEAR DOWN & RECEIVED 3 DOWN & LOCK LIGHTS WITHOUT FURTHER INCIDENT. FOUND 60 AMP CIRCUIT TRIPPED. NO OTHER DEFECTS NOTICED ON INITIAL INSPECTION. A RETRACTION WAS PERFORMED IAW MANUAL & GEAR RETRACTED WITH NO DEFECTS NOTED. WHEN GEAR DOWN SELECTED, RETRACT MOTOR BOGGED DOWN & TRIPPED THE 60 AMP CIRCUIT BREAKER. ON CLOSER INSPECTION, HYD FLUID OBSERVED LEAKING FROM AREA WHERE RETRACT MOTOR CONNECTS TO HYD POWER PACK. REMOVED HYD POWER PACK & RETRACT MOTOR ASSY. SOURCE OF HYD LEAK FOUND TO BE HYD POWER PACK GARLOCK SEAL OR SHAFT SEAL. SNAP RING TO RETAIN THE GARLOCK SEAL WAS MISSING. RETAINING SNAP RING PREVENTS GARLOCK SEAL FROM MOVING AND ALLOWING HYD FLUID TO LEAK INTO RETRACT MOTOR.

Source: SDR 2012FA0000105 · FAA SDRS
B · 2011-01-11 Matched by certificate designator
N232BG · ATA 2497

PILOT COMPLAINED OF INTERMITTENT POPPING OF STALL WARNING, RT PITOT HEAT, RECOGNITION LIGHT AND STROB LIGHT CIRCUIT BREAKER SWITCHES ON REMOVAL OF LT SUBPANEL REVEALED THAT THE BUSS BAR PN 101364084-219 WAS PHYSICALLY ATTACH TO THE STALL WARNING HEAT SWITCH. THE MAIN FEEDER WIRE PN P260A8 WAS ATTACHED TO THE SWITCH. THE BUS BAR WAS FOUND LAYING ON TOP OF THE SWITCH ATTACH SCREW AND EVENTUALLY STARTED ARCING AND POPPING THE CIRCUIT BREAKER SWITCHES DOWNSTREAM FOR IT. THE STALL WARNING HEAT SWITCH PN 7270-5-15 AND BUS BAR PN 101-364084-219 WERE REPLACED AND INSTALL PROPERLY.

Source: SDR 2011FA0000047 · FAA SDRS

Linked aircraft

N-numberMake / modelYearStatusLink basis
N232BGMatched by certificate designator