N5401G

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.

11 reports on file, 1996-09-25 – 2003-04-11.

OTHER · 2003-04-11 Matched by certificate designator
ATA 2435

Part: BRUSHES — DETACHED (STARTER GEN) · airframe 19,598 hrs

PART IS DISBONDED. THE ATTACHING LEAD AND SPRING WEAR PLATE AND RIVET CAME APART. REPLACED ALL FOUR BRUSHES AND RAN IN BRUSHES.

Source: SDR AC2A086266
OTHER · 2003-03-02 Matched by certificate designator
ATA 5320

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,509 hrs

COROSION FOUND ON ANGLE DURING INSPECTION. PART WAS REPLACED.

Source: SDR AC2A084872
FALSE WARNING · 2001-12-27 Matched by certificate designator
ATA 7921

Part: THERMOSTAT — INACCURATE (OIL COOLER) · airframe 18,256 hrs

HIGH ENGINE OIL TEMPERATURE IN FLIGHT. REPLACED THERMOSTAT. CURED PROBLEM.

Source: SDR AC2A077544
OTHER · 2001-12-27 Matched by certificate designator
ATA 7922

Part: THERMOSTAT — INOPERATIVE (ENGINE OIL)

THERMOSTAT, HIGH ENGINE OIL TEMPERATURE IN FLIGHT. REMOVED AND REPLACED THERMOSTAT. CURED PROBLEM.

Source: SDR AC2A0000301
OTHER · 2001-04-05 Matched by certificate designator
ATA 2435

Part: BEARING — DETERIORATED (DRIVE END)

PART IS DETERIORATED. BEARING CAGE FAILED ALLOWING ALL BALLS TO GROUP TOGETHER. NO BALLS WERE LOST OR DETERIORATED OVERHAULED STARTER - GENERATOR AND REPLACED BEARINGS.

Source: SDR AC2A072790
OTHER · 2000-10-17 Matched by certificate designator
ATA 6700

Part: FITTING — CRACKED (FLIGHT CONTROLS) · airframe 16,882 hrs

PART IS CRACKED. REPLACED CRACKED COLLECTIVE SOCKET.

Source: SDR AC2A072770
OTHER · 2000-07-07 Matched by certificate designator
ATA 6210

Part: BLADE — CORRODED (MAIN ROTOR)

DURING ZONE 1 INSPECTION, CORROSION WAS FOUND THROUGHOUT THE LOWER SURFACE OF THE YELLOW MAIN ROTOR BLADE. THE ALUMINUM WIRE MESH WAS FOUND WITH NUMEROUS SMALL PITS OF CORROSION THROUGHOUT THE LOWER SURFACE OF THE BLADE. REMOVED CORROSION AND SPOT PAINTED PER COMPOSITE REPAIR MANUAL. (X)

Source: SDR AC2A0000067
OTHER · 2000-07-07 Matched by certificate designator
ATA 6210

Part: BLADE — CORRODED (MAIN ROTOR)

DURING ZONE 1 INSPECTION, CORROSION WAS FOUND THROUGHOUT LOWER SURFACE OF MAIN ROTOR BLADE. THE ALUMINUM WIRE MESH WAS FOUND WITH NUMEROUS CORROSION PITS THROUGHOUT THE LOWER SURFACE OF THE BLADE. REMOVED CORROSION AND SPOT PAINTED PER COMPOSITE REPAIR MANUAL. (X)

Source: SDR AC2A0000068
OTHER · 1999-09-20 Unresolved
ATA 2200

Part: POTENTIOMETER — FAILED (AFCS)

FEEDBACK POTENTIOMETER PREMATURE FAILURE, SHOULD LAST UNTIL OVERHAUL TIME OF 3,000 HOURS. SUBMITTER STATED CAUSED ACTUATOR TO KICK IN-FLIGHT. COMPONENT P/N 7690001802106.

Source: SDR 99ZZZX4159
OTHER · 1997-05-08 Unresolved
ATA 5210

Part: HINGE — CORRODED (DOOR)

CORROSION WHERE BUSHINGS GO THROUGH HINGE. REPLACED DOOR HINGE.

Source: SDR 97ZZZX2755
FLUID LOSS · 1996-09-25 Unresolved
ATA 2910

Part: MODULE — LEAKING (HYD)

HYDRAULIC MODULE ASSEMBLY PN 76650-09801-104 WAS REPORTED LEAKING AT CYLINDER OF MODULE. REMOVED CYLINDER PN 0711311-202 O-RING PN 0711311-237 AND INSTALLED ANOTHER SERVICEABLE CYLINDER AND O-RING. C/W LEAK CHECK OF MODULE ASSY. FOUND TO BE SERVICEABLE.

Source: SDR 96ZZZX6185