CORPORATE EAGLE MANAGEMENT SERVICES, INC.

Part 135 operator · designator DJXA

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

Also recorded as: CORPORATE EAGLE, CORPORATE EAGLE MANAGEMENT SERVICES, INC., Corporate Eagle Management Services, Inc.

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.

11 reports on file.

O · 2013-01-11 Matched by certificate designator
N948CE · ATA 5520

RIVETS LOOSE, HOLDING INBD ATTACH BELLCRANK LEVER TO TORQUE TUBE. BELLCRANK LEVER HAS PLAY TO TORQUE TUBE.

Source: SDR DJX2013F00000 · FAA SDRS
O · 2013-01-11 Matched by certificate designator
N948CE · ATA 2730

RIVETS LOOSE, HOLDING INBD ATTACH BELLCRANK LEVER TO TORQUE TUBE. BELLCRANK LEVER HAS PLAY TO TORQUE TUBE.

Source: SDR DJX2013F00001 · FAA SDRS
O · 2006-10-21 Matched by certificate designator
N942CE · ATA 5610

ON A LEG, ENROUTE, AT CRUISE ALTITUDE OF FL250, THE INNER PANE OF THE RT WINDSCREEN SHATTERED, THE CREW THEN LANDED AT THE NEAREST SUITABLE AIRPORT (ERI), WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS FERRIED BACK, WHERE THE WINDSCREEN WAS REPLACED WITH P/N 101-384025-24.

Source: SDR 2006F00050 · FAA SDRS
O · 2006-10-21 Matched by certificate designator
N942CE · ATA 5610

ON A LEG, AT CRUISE ALTITUDE OF FL250, THE INNER PANE OF THE RT WINDSCREEN SHATTERED, THE CREW THEN LANDED AT THE NEAREST SUITABLE AIRPORT (ERI), WITHOUT FURTHER INCEDENT. THE AIRCRAFT WAS FERRIED BACK TO DEPARTURE WERE THE WINDSCREEN WAS REPLACED WITH P/N 101-384025-24.

Source: SDR 2006F00051 · FAA SDRS
O · 2005-11-22 Matched by certificate designator
N946CE · ATA 5610

AT 27,000 FT THE PILOT SIDE WINDSHIELD SHATTERED. THE PILOTS VIEW WAS TOTALLY OBSTRUCTED. THE COPILOT WAS ABLE TO LAND THE AIRCRAFT SAFELY. AFTER REMOVAL, THE OUTSIDE PANEL WAS NOT DAMAGED. THE INSIDE PANEL WAS STILL IN TACT BUT COMPLETELY SHATTERED. THE LARGEST PIECE WAS ONLY .5 INCH IN DIAMETER. AFTER TALKING TO MFG, IT WAS REVEALED THAT THIS WAS A COMMON PROBLEM AND AN NEW STYLE WINDSHIELD WAS BEING USED. (K)

Source: SDR 2005FA0001590 · FAA SDRS
O · 2004-07-24 Matched by certificate designator
N946CE · ATA 2720

DURING A RUDDER BOOST TEST THE RT RUDDER PEDAL, REMAINED AT FULL DEFLECTION EVEN WITH THE ENGINES AT IDLE. BY TURNING THE SYSTEM OFF BOTH PDEALS WOULD RETURN TO CENTER. IF THE SYSTEM FAILED ON FINAL AND OR DURING TAKE OFF THE END RESULT COULD BE DEVASTATING.

Source: SDR DJX2004F00000 · FAA SDRS
O · 2002-08-15 Matched by certificate designator
N942CE · ATA 5542

FOUND A 3.5 INCH CRACK APPROXIMATELY 6 INCHES DOWN AND .0200 INCH ON THE RIGHT SIDE TRAILING EDGE OF THE RUDDER.

Source: SDR 2002FA0001136 · FAA SDRS
G J · 2000-05-11 Matched by certificate designator
N943CE · ATA 2432

CLIMBING THROUGH 13,000 FEET, LEFT GENERATOR FAILED, NO RESET CAPABILITY, AUTO-PILOT TRIPPED OFF, BOTH NR 1 AND NR 2 INVERTERS FAILED. BATTERY-ON HORN KEPT HONKING INTERMITTENTLY AT 2 TIMES PER SECOND RATE. ALL CO-PILOT FLIGHT INSTRUMENTS FLAGGED OFF. ALL PILOT FLIGHT INSTRUMENTS FLAGGED OFF, EXCEPT FOR PILOT''''S ADI HORIZON. AIRCRAFT LANDED AT PTK WITHOUT INCIDENT. CHANGED RIGHT BATTERY CONTACTOR, FIXED THE PROBLEM. (M)

Source: SDR 20000727AP005 · FAA SDRS
O · 1999-10-16 Matched by certificate designator
N946CE · ATA 3222

HEAVILY CORRODED IN CYLINDER BORE. CORROSION FILLED IN WITH PUTTY. SUBMITTER STATED CAUSE AS DISSIMILAR METALS AND MOISTURE.

Source: SDR 99ZZZX4149 · FAA SDRS
X · 1997-04-08 Matched by certificate designator
N942CE · ATA 7314

ENGINE WENT TO IDLE CUT OFF IN-FLIGHT. (FLAME OUT.) MAIN ENGINE PUMP SEIZED. ENGINE SHAFT BECAME WORN AND ROUNDED OFF SPLINES.

Source: SDR 97ZZZX1745 · FAA SDRS
X · 1997-03-10 Matched by certificate designator
N942CE · ATA 7314

LEFT ENGINE ROLLED BACK TO IDLE CUT-OFF IN FLIGHT. (FLAME OUT.) MAIN ENGINE FUEL PUMP SEIZED CAUSING ROUNDING OFF OF SPLINE ON PUMP AND DRIVE COUPLING. SUBMITTER SUGGESTED TO INCREASE FREQUENCY OF INSPECTION FOR THIS COMPONENT.

Source: SDR 97ZZZX1328 · FAA SDRS

Linked aircraft

N-numberMake / modelYearStatusLink basis
N306BHDASSAULT AVIATION FALCON 20002005Valid RegistrationMatched by certificate designator
N623HDDASSAULT AVIATION FALCON 20001996Valid RegistrationMatched by certificate designator
N850TCDASSAULT AVIATION FALCON 20001999Valid RegistrationMatched by certificate designator
N942CERAYTHEON AIRCRAFT COMPANY B2002000Valid RegistrationMatched by certificate designator
N946CEMatched by certificate designator
N981CEHAWKER BEECHCRAFT CORP HAWKER 900XP2012Valid RegistrationMatched by certificate designator
N982CEHAWKER BEECHCRAFT CORP HAWKER 900XP2007Registration pendingMatched by certificate designator
N983CEHAWKER BEECHCRAFT CORP HAWKER 900XP2009Valid RegistrationMatched by certificate designator
N984CEHAWKER BEECHCRAFT CORP HAWKER 900XP2008Valid RegistrationMatched by certificate designator
N986CEHAWKER BEECHCRAFT CORP HAWKER 900XP2008Valid RegistrationMatched by certificate designator
N987CEMatched by certificate designator
N989CEMatched by certificate designator
N991CEDASSAULT AVIATION FALCON 20002001Valid RegistrationMatched by certificate designator
N992CEDASSAULT AVIATION FALCON 2000EX2003Valid RegistrationMatched by certificate designator