N600G

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.

4 reports on file, 1995-06-08 – 1996-07-11.

OTHER · 1996-07-11 Unresolved
ATA 2460

Part: BREAKER — FAILED (COMM NR 2)

COMM 2 CIRCUIT BREAKER OPENED DURING FLIGHT AND WOULD NOT RESET. CIRCUIT BREAKER WAS REPLACED WITH NEW BREAKER.

Source: SDR 96ZZZX5024
OVER TEMP · 1995-06-19 Unresolved
ATA 2432

Part: BATTERY — COVER MELTED (DC SYSTEM)

BATTERY PACK COVER MELTED AROUND TERMINAL POSTS. THIS CONDITION CAUSED BY LOOSE/HIGH RESISTANCE CONNECTION BETWEEN TERMINAL POSTS AND CELL TABS. SUBMITTER RECOMMENDS MANUFACTURER USE THICKER MATERIAL FOR COVER PERHAPS OF A PHENOLIC AS THEY USED TO DO IN PREVIOUS YEARS. EARLIER PACKS ALSO INCORPORATED A SCREW AND JAM NUT CONFIGURATION TO MAINTAIN A SECURE CONNECTION.

Source: SDR 95ZZZX3655
OTHER · 1995-06-08 Unresolved
ATA 2730

Part: ELEV QUADRANT — CORRODED (AFT OF HORZ STAB)

DURING A VISUAL INSPECTION OF THE ELEVATOR QUADRANT, WHITE POWDER WAS NOTED AROUND THE UPPER CONTROL CABLE ATTACH POINT BARREL. REMOVAL OF BOTH CABLES FOUND DEEP CORROSION IN THE CONTROL CABLE ATTACH POINTS ON THE QUADRANT, THE 2400-HOUR 24 AND 48-MONTH INSPECTION CALL OUT FOR AN INSPECTION OF COMPONENTS AND CABLES IN THE HORIZONTAL STABILIZER AREA. NOTHING ABOUT REMOVING CABLES, WITHOUT REMOVING THE CONTROL CABLES AND BARRELS FROM QUADRANT, THIS AREA WOULD NOT BE LOOKED AT.

Source: SDR 95ZZZX3099
OTHER · 1995-06-08 Matched by certificate designator
ATA 2730

Part: QUADRANT — CORRODED (ELEV CONTL)

DURING A VISUAL INSPECTION OF THE ELEVATOR QUADRANT, WHILE POWDER WAS NOTED AROUND THE UPPER CONTROL CABLE ATTACH POINT BARREL. REMOVAL OF BOTH CABLES FOUND DEEP CORROSION IN THE CONTROL CABLE ATTACH POINTS ON THE QUADRANT. THE 2400-HOUR, 24- AND 48-MONTH INSPECTIONS CALL OUT FOR AN INSPECTION OF COMPONENTS AND CABLES IN THE HORIZONTAL STABILIZER AREA. NOTHING ABOUT REMOVING CABLES. WITHOUT REMOVING THE CONTROL CABLES AND BARRELS FROM QUADRANT, THIS AREA WOULD NOT BE LOOKED AT.

Source: SDR 95ZZZX3434