ATLANTA AIR CHARTER, INC.
Also recorded as: ATLANTA AIR CHARTER, INC., Atlanta Air Charter, 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.
9 reports on file.
DURING A PHASE 4 INSPECTION ON OUR KING AIR 200 N383JP, IT WAS DISCOVERED THAT THE MANUAL GEAR DOWN ACTUATION LEVER WOULD NOT OPERATE. UPON INSPECTION, IT WAS DETERMINED THAT THE ACTUATING LEVER CABLE GOING FROM THE ACTUATION LEVER TO THE LANDING GEAR GEARBOX WAS BROKEN APPROXIMATELY 18 INCHES FROM THE CONNECTION OF THE GEARBOX CLEVIS. THIS WOULD NOT ALLOW THE MANUAL GEAR DOWN PUMPING HANDLE TO ENGAGE AND ALLOW PUMPING OF THE LANDING GEAR DOWN IN CASE OF A LANDING GEAR MALFUNCTION. IT COULD NOT BE DETERMINED WHEN THE CABLE BROKE, OR THE ROOT CAUSE.
DURING FLIGHT, WHILE DECENDING TO FL220, THE CREW REPORTED THAT THEY COULD NO LONGERCONTRO THE AIRCRAFT CABIN PRESSURE SYSTEM. CREW DECLARED AN EMERGENCY & DECENDED TO FL10000, IN THAT TIME REGAINED CABIN PRESSURE CONTROL. NO PAX ABOARD. LANDED WITHOUT ISSUE. ROOT CAUSE NOT DETERMINED & UNDER INVESTIGATION. OPEN
WHEN PERFORMING AND AFTER PHASE INSPECTION CHECK FLIGHT, FOLLOWING TAKEOFF AND LANDING GEAR RETRACTION THE RED IN-TRANSIT LIGHT IN THE GEAR HANDLE WOULD REMAIN ILLUMINATED. THE AIRCRAFT RETURNED AND WAS PLACED ON JACKS. REPEATED LANDING GEAR CYCLES WERE NORMAL AND THE ISSUE COULD NOT BE GROUND DUPLICATED. ANOTHER CHECK FLIGHT WAS ACCOMPLISHED WITH THE RED LIGHT REMAINING AFTER RETRACTION. THE AIRCRAFT WAS AGAIN JACKED AND AGAIN, ALL CYCLES WERE NORMAL. UPLOCK SWITCH RIGGING WAS CHECKED AND FOUND NORMAL. AIRLOADS WERE SIMULATED ON THE GEAR AND ALL HANGAR RETRACTIONS WERE NORMAL. ANOTHER CHECK FLIGHT WAS ACCOMPLISHED WITH THE RED LIGHT REMAINING AFTER RETRACTION. THE AIRCRAFT WAS AGAIN JACKED AND THE GEAR CYCLED, AND OPERATION AND INDICATIONS WERE NORMAL. THE LANDING GEAR MOTOR WAS REPLACED AND THE LANDING GEAR WAS OPERATIONALLY CHECKED AND FOUND NORMAL. LANDING GEAR OPERATION AND INDICATIONS WERE NORMAL ON THE SUBSEQUENT CHECK FLIGHT, AND HAS BEEN NORMAL SINCE THAT REPLACEMENT.
LANDING GEAR WAS RETRACTED ON FINAL DEPARTURE FOR THE DAY RETURNING TO HOME BASE. ON LANDING GEAR RETRACTION, THE LANDING GEAR MOVEMENT STOPPED PRIOR TO COMPLETE RETRACTION AND THE CIRCUIT BREAKER FOR THE LANDING GEAR MOTOR TRIPPED. THE LANDING GEAR WAS MANUALLY EXTENDED PER CHECKLIST PROCEDURES AND PROPER DOWN AND LOCKED INDICATIONS WERE NOTED. THE AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTION OF THE AIRCRAFT INDICATED THAT THE RIGHT INBOARD LANDING GEAR DOOR HAD CONTACTED THE MAIN LANDING GEAR DURING RETRACTION AND MINOR DEFORMATION AT THE DOOR CONTACT POINT WAS NOTED. THE FLIGHT CREW REPORTED THAT STRONG AND GUSTY WINDS WERE PREVAILING DURING THE SUBJECT TAKE-OFF. THE AIRCRAFT HAS BEEN REPOSITIONED TO A CERTIFIED REPAIR STATION UNDER SPECIAL FLIGHT PERMIT TO ACCOMPLISH FURTHER INSPECTION AND REPAIRS.
LEFT ENGINE OIL PRESSURE REPORTED AS READING HIGH - OFF OF THE SCALE. ALL OTHER ENGINE INDICATIONS WERE NORMAL. REMOVED DEFECTIVE TRANSMITTER AND INSTALLED SERVICEABLE PART AND INDICATIONS WERE OPERATIONALLY CHECKED AND FOUND NORMAL.
ON RE-POSITIONING FLIGHT FOR MAINTENANCE OF OTHER SYSTEM, AIRCRAFT WAS ON AUTO-PILOT AND ALTITUDE HOLD WAS SELECTED AND WAS INDICATED AS ENGAGED. THE AIRCRAFT DRIFTED OFF OF ALTITUDE HOLD SETTING TO A HIGHER ALTITUDE WHICH OCCURRED VERY GRADUALLY. UPON ARRIVAL, THE TROUBLESHOOTING OF SYSTEM IDENTIFIED THE AIR DATA COMPUTER AS THE ISSUE. INSTALLED AN OVERHAULED UNIT AND OPERATIONAL TESTED ALTITUDE HOLD SYSTEM AND FOUND PROPER OPERATION.
CABIN PRESSURE WARNING LIGHT ILLUMINATED AT FL 250, DESCENDED TO FL 210 AND COULD NOT CONTROL CABIN PRESSURE. NORMAL LANDED. MAINTENANCE PERFORMED INSPECTIONS OF OUTFLOW VALVES AND PILOT WING WINDOWS AND EMERGENCY EXIT DOOR AND CABIN ENTRY DOOR. FOUND CABIN DOOR STRUCTURE CRACKED AT DOOR HINGE ATTACH POINT. CABIN DOOR REMOVED AND SENT OUT FOR REPAIR.
AFTER TAKEOFF AT 3000 FT AGL, LT BLEED FAIL, LIGHT ILLUMINATED. LT BLEED SWITCH WAS SELECTED "OFF" AND RTB WITH OUT INCIDENT. OVERHEAT DETECTION TUBING UNDER CO-PILOTS FLOOR WAS FOUND CHAFED AND PREVIOUSLY REPAIRED, TUBING WAS REPLACED WITH NEW. LT FIREWALL BLEED AIR SHUTOFF VALVE FOUND FAILED IN OPEN POSITION. VALVE AND CONNECTOR WERE CLEANED AN OPS CHECKED GOOD.
RT WINDSHIELD CRACKED.
Linked aircraft
| N-number | Make / model | Year | Status | Link basis |
|---|---|---|---|---|
| N143DE | BEECH 200 | 1979 | Valid Registration | Matched by certificate designator |
| N332CA | BEECH 200 | 1981 | Valid Registration | Matched by certificate designator |
| N383JP | BEECH 200 | 1980 | Valid Registration | Matched by certificate designator |
| N700NA | BEECH B200 | 1994 | Valid Registration | Matched by certificate designator |