N888DG

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

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

2 reports on file, 2001-07-05.

WARNING INDICATION · 2001-07-05 Matched by certificate designator
ATA 7810

Part: ADAPTER — WORN (EXHAUST PIPE)

FLIGHT CREW HAD A ZONE 1 FIRE WARNING WITH NO OTHER INDICATIONS. ON INSPECTION ON THE ENGINE, NR 14 CYLINDER WAS FOUND TO HAVE A LOOSE EXHAUST VALVE GUIDE CAUSING THE COMBUSTION CHARGE ACCESS TO THE EXHAUST SYSTEM. THE EXHAUST PIPE ADAPTER FOR THIS CYLINDER WAS WORN AND IT IS SUSPECTED THAT FLAMES FROM THIS CYLINDER LEAKED ONTO THE FIRE WARNING SYSTEM. THE FIRE WARNING SYSTEM ALSO HAD A 3 OHMS RESISTANCE VS. 2 OHMS WHICH WOULD HAVE MADE THE SYSTEM MORE SENSITIVE. NO OTHER FAULTS FOUND.

Source: SDR FXG2001F00000
WARNING INDICATION · 2001-07-05 Matched by certificate designator
ATA 8530

Part: VALVE GUIDE — LOOSE (CYLINDER)

FLIGHT CREW HAD A ZONE 1 FIRE WARNING WITH NO OTHER INDICATIONS. ON INSPECTION ON THE ENGINE, NR 14 CYLINDER WAS FOUND TO HAVE A LOOSE EXHAUST VALVE GUIDE CAUSING THE COMBUSTION CHARGE ACCESS TO THE EXHAUST SYSTEM. THE EXHAUST PIPE ADAPTER FOR THIS CYLINDER WAS WORN AND IT IS SUSPECTED THAT FLAMES FROM THIS CYLINDER LEAKED ONTO THE FIRE WARNING SYSTEM. THE FIRE WARNING SYSTEM ALSO HAD A 3 OHMS RESISTANCE VS. 2 OHMS WHICH WOULD HAVE MADE THE SYSTEM MORE SENSITIVE. NO OTHER FAULTS FOUND.

Source: SDR FXG2001F00001