N383JP
Registered owner: ATLANTA AIR CHARTER INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ATLANTA AIR CHARTER, INC. (V6HA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
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
LANDING GEAR WAS RETRACTED ON FINAL DEPARTURE FOR THE DAY RETURNING TO HOME BASE.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.
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.
REMOVED AND REPLACED AFT CABIN DOOR FRAME PRESSURATION PROBLEM.