CAUSEY AVIATION SERVICE, INC.
Also recorded as: CAUSEY AVIATION SERVICE, INC.
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
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.
6 reports on file.
ACFT WAS AT 21,000 FT. AND APPROVED FOR HIGHER ALTITUDE. POWER WAS APPLIED AND RT ENGINE HAD NO RESPONSE. ACFT WAS RETURNED TO DEPARTURE POINT GSO. POWER CONTROL WAS EFFECTIVE BELOW 10,000 FT. ACFT WAS TURNED OVER TO SERVICE CENTER FOR REPAIRS NEEDED.
STARTING DESCENT, VIBRATION/NOISE WAS AUDIBLE INSIDE ACFT. NO INDICATIONS OF SYSTEM ISSUES OTHER THAN THE VIBRATION BUZZ NOISE. FLT DIVERTED. WHEN LANDING GEAR WAS EXTENDED FOR LANDING VIBRATION/NOISE WENT AWAY. ACFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS TURNED OVER TO SERVICE CENTER. STUD ON LEFT GEAR DOOR ROD WAS BROKEN. GEAR DOOR RECEIVED ABRASION DAMAGE FROM CONTACT WITH PAVEMENT.
AFTER DEPARTURE, THE CREW NOTICED THE ANNUNCIATOR WARNING LIGHT COME ON FOR THE RT ENGINE FUEL FILTER BYPASS. THE CREW NOTIFIED ATC, DECLARED AN EMERGENCY, AND WERE ROUTED FOR LANDING, AFTER ARRIVING SAFELY AND CONFERRING WITH THE MFG ON FIELD, THE RT FUEL FILTER WAS REPLACED AND THE BYPASS PRESSURE SENSOR WAS ALSO REPLACED CORRECTING THE PROBLEM. THE RT FUEL FILTER SHOWED NO SIGNS OF CONTAMINATION. (K)
THE AIRCRAFT WAS A CRUISE ALTITUDE 37,000 WHEN THE PILOTS NOTICED FIRST BLUE, AND THEN WHITE SMOKE FILLING THE FLIGHT DECK AND CABIN. REDUCED POWER, DECLARED AN EMERGENCY, AND LANDED AT LAGRANGE, GA. THERE WAS STILL SOME SMOKE IN THE AIRCRAFT UPON LANDING. AFTER EXITING THE AIRCRAFT, THE PILOTS REPORTED THAT THERE WAS OIL ON THE OUTSIDE OF THE LEFT ENGINE COWLING AND INSIDE TAILPIPE. NEITHER ENGINE WAS SHUT DOWN DURING THE INCIDENT. AT PRESENT, SUSPECT OIL LEAKAGE INTO BLEED AIR SYSTEM FROM DEFECTIVE CARBON SEAL INSIDE COMPRESSOR SECTION.
FOLLOW UP REPORT AFTER PILOT REPORT TO FSDO OF (LARGE) BIRD STRIKE TO INLET AND INGESTION INTO LT ENGINE.
GEAR SELECTED UP AFTER TAKEOFF. USAFE LIGHT WOULD NOT EXTINGUISH AND AIR NOISE FROM NOSE GEAR DOORS OPEN. ATTEMPTS TO GET DOORS TO CLOSE ON GEAR RETRACTION FAILED. RETURNED TO DEPARTURE AIRPORT AND ACFT.DELIVERED TO CITATION SERVICE CENTER AT GSO. NOSE GEAR UP LOCK SWITCH SWITCH FOUND DEFECTIVE: REPLACED AND OPERATION CHECKED GEAR NORMAL OPERATION.
Linked aircraft
| N-number | Make / model | Year | Status | Link basis |
|---|---|---|---|---|
| N108RL | RAYTHEON AIRCRAFT COMPANY HAWKER 800XP | 2003 | Valid Registration | Matched by certificate designator |
| N234AQ | CESSNA 560 | 1993 | Valid Registration | Matched by certificate designator |
| N325RD | CESSNA 650 | 1995 | Valid Registration | Matched by certificate designator |
| N560SJ | CESSNA 560XL | 2001 | Valid Registration | Matched by certificate designator |
| N622PM | CESSNA 650 | 1993 | Valid Registration | Matched by certificate designator |
| N734DB | CESSNA 560 | — | Valid Registration | Matched by certificate designator |
| N800XR | RAYTHEON CORPORATE JETS INC HAWKER 800XP | 1995 | Valid Registration | Matched by certificate designator |