N321GL

No registry detail on file · not in current registry

Operators of this aircraft

Who operated this tail, and how firmly we know it.

No operator established for this aircraft.

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

F J · 2001-05-22 Matched by certificate designator
ATA 2750

FLAP CIRCUIT BREAKER POPS WHEN FLAPS ARE SELECTED DOWN. CORRECTIVE ACTION: FOUND DIODE ON TB-28 IN RIGHT MAIN LANDING GEAR. WHEEL WELL SHORTED. INSTALLED NEW DIODE. PROBABLE FAILURE RELATED TO DIODE AND PC BOARD BEING EXPOSED TO ALL WEATHER ELEMENTS, CORROSION.

Source: SDR 20010613CW001 · FAA SDRS
K · 1999-08-30 Matched by certificate designator
ATA 2910

THE LEFT ENGINE HYDRAULIC PRESSURE LINE CRACKED UNDER AN ADEL CLAMP THAT SECURED THE LINE TO THE AIRCRAFT STRUCTURE LOCATED ABOVE AND AFT OF THE GENERATOR CONTROL UNIT. THE LINE HAD BEEN BADLY WORN BY TWO CLAMPS. ANYTIME AN ACCUMULATION OF BLACK RESIDUE IS NOTED AROUND THESE CLAMPS DURING AN INSPECTION, REMOVE THE CLAMPS AND INSPECT THE TUBING FOR WEAR.

Source: SDR 99ZZZX3496 · FAA SDRS