BOHLKE, LLC
Also recorded as: BOHLKE, 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.
8 reports on file.
DURING A PRE-BUY INSPECTION OF THE LT AND RT ENGINES ON THIS AIRCRAFT, A BORESCOPED WAS PERFORMED. FOUND THAT THE SOME OF THE DIFFUSER ATTACHING HARDWARE INSIDE THE CASE LINER WERE LOOSE OR MISSING FROM THEIR RESPECTIVE HOLES AND LAYING IN THE BOTTOM OF THE ENGINE CASE LINER ON BOTH ENGINES. NO LOSS OF ENGINE PERFORMANCE OR INDICATION DURING PREVIOUS OPERATION WAS NOTED.
ON DEPARTURE, THE GEAR HANDLE WOULD NOT COME UP, AND THE GEAR REMAINED IN THE DOWN AN LOCKED POSITION. DID NOT DECLARE AN EMERGENCY. NORMAL LANDING. EVALUATED THE AIRCRAFT AND FOUND NOTHING ABNORMAL AND TAXIED TO THE HANGAR. THE LANDING GEAR SYSTEM WAS INSPECTED AND A WORN SQUAT SWITCH ACTUATOR WAS DETERMINED TO BE THE CAUSE. THE SWITCH ACTUATOR) WAS REPLACED AND THE LANDING GEAR SYSTEM WAS FUNCTIONALLY CHECKED IAW MM 32-01-00.
RIGHT BRAKE LOCKED UP AFTER LANDING WAS COMPLETED, WHILE TRYING TO TURN AROUND ON RUNWAY.
LEFT BRAKE LOCKED UP AFTER LANDING WAS COMPLETED WHILE TRYING TO TURN ONTO TAXI WAY.
DURING A SCHEDULED PHASE 5 INSPECTION, FOUND FITTING IN VERTICAL STAB TO BE CRACKED. OPEN
NR 1 THRUST REVERSER "ARM" LIGHT ILLUMINATED CONTINUOUSLY, WITH ENGINES SHUTDOWN. THE FAULT LIES IN THE ARM LIGHT PRESSURE SWITCH. INSTALLING A NEW SWITCH FIXED THE PROBLEM.
THE COLLAR HAS A CRACK WHERE THE TAPER PIN GOES THROUGH. POSSIBLE SOMEONE OVER TORQUED THE TAPER PIN. (K)
FOUND FUEL FILTER INLET FITTING O-RING EXTRUDED FROM FITTING. THERE WAS NO EVIDENCE OF FUEL LEAKING. DISCOVERED IMPROPERLY MACHINED LAND ON FITTING WOULD NOT ALLOW SEAL TO PROPERLY MATE WITH SEAL RECESS IN HOUSING. REPLACED FITTINGS WITH NEW PARTS WHICH DID NOT HAVE LANDS. LEAK CHECK NORMAL.
Linked aircraft
| N-number | Make / model | Year | Status | Link basis |
|---|---|---|---|---|
| N49KW | CESSNA 550 | 2002 | Valid Registration | Matched by certificate designator |
| N55WL | CESSNA 550 | 1980 | Valid Registration | Matched by certificate designator |
| N573M | CESSNA 550 | 2003 | Valid Registration | Matched by certificate designator |
| N773RB | CESSNA 560 | 1990 | Valid Registration | Matched by certificate designator |
| N82ML | CESSNA 550 | 1982 | Valid Registration | Matched by certificate designator |
| N880GP | — | — | Matched by certificate designator | |
| N990TC | CESSNA 550 | 2001 | Valid Registration | Matched by certificate designator |
| N999UP | MITSUBISHI MU-2B-60 | 1982 | Valid Registration | Matched by certificate designator |