N405AE

EUROCOPTER AS 350 B3 · 2000 · Rotorcraft · 1 engine · 6 seats · Valid Registration

Registered owner: TEMSCO HELICOPTERS INC, AK (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Temsco Helicopters, Inc (HXSA)Certificate holderMatched by certificate designator

Accident & incident history

Accident · 2000-09-23 Matched by aircraft (N-number)
Eurocopter AS-350B-3 No injuries Part 91Temsco Helicopters, Inc
Source: NTSB case ANC00LA132

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.

8 reports on file, 2002-06-05 – 2006-03-02.

OTHER · 2006-03-02 Matched by certificate designator
ATA 7250

Part: RING — CRACKED (ENGINE)

IN COMPLIANCE WITH AD AND SB, OUR MECHANIC WAS INSPECTING THE ABOVE DESCRIBED ENGINE AND FOUND THE COMPONENT LISTED BELOW TO BE OUT OF SERVICEABLE LIMITS AS INDICATED IN THE 2 DOCUMENTS. REMOVED THE CONTAINMENT RING FROM SERVICE AND INSTALLED A NEW POST MOD TU-22 RING AS ADVISED. (K)

Source: SDR 2006FA0000268
OTHER · 2004-05-07 Matched by certificate designator
ATA 6410

Part: BLADE — CRACKED (TAIL ROTOR)

INSPECTOR FOUND CRACK IN TAIL ROTOR PROTRUDING OUT OF RIVET LOCATION ON TRIM TAB. CRACK WAS FOUND DURING INSPECTION IAW AD 2001-26-55. (AL05200402466)

Source: SDR HXSD2004517
OTHER · 2003-07-18 Matched by certificate designator
ATA 7603

Part: ROLL PIN — FAILED (TORQUE TUBE)

AIRCRAFT FAILED POWER CHECKS DUE TO TORQUE FAILURE. INVESTIGATED SITUATION AND DETERMINED THAT A ROLL PIN FAILURE HAD OCCURED.

Source: SDR HXS2003F00004
OTHER · 2002-10-14 Matched by certificate designator
ATA 5310

Part: STRUCTURE — BUCKLED (FUSELAGE)

FUSELAGE BOX STRUCTURE CROSS BRACES BUCKLED. SENT FOR JIG SET AND REPAIR.

Source: SDR HXSA0000403
OTHER · 2002-09-18 Matched by certificate designator
ATA 7712

Part: MODULE — FAILED (TORQUE)

TORQUE INDICATION STARTED TO FLUCTUATE, AIRCRAFT GROUNDED.

Source: SDR HXS2002F00001
NO TEST · 2002-07-10 Matched by certificate designator
ATA 7712

Part: MODULE — FAILED (TORQUE INDICATOR)

TORQUE INDICATION STARTED TO FLUCTUATE. REMOVED MO1 MODULE WHICH HOURS THE TORQUE TUBE AND INSTALLED RENTAL MODUAL, SENT MO1 TO MFG. THIS WAS THEIR RENTAL. THEY DID NOTIFICATION THAT THIS WAS THE SAME TYPE OF FAILURE BEFORE IN THE FACT THAT THE ROLL PINS ON THE TORQUE TUBE HAD SHEARED.

Source: SDR HXS2002F00003
NO TEST · 2002-06-18 Matched by certificate designator
ATA 7712

Part: MODULE — FAILED (TORQUE INDICATOR)

REMOVED ENGINE MODULE 1 DUE TO TORQUE SYSTEM REFERENCE SHAFT PHONIC WHEEL ROLL PINS SHEARING CAUSING LOSS OF TORQUE INDICATION VEMD. REMOVED LOANER MODULE 1 FOR REPAIR. INSTALLED LOANER MODULE. SENDING UNIT TO MFG FOR REPAIR.

Source: SDR HXSA0000375
NO TEST · 2002-06-05 Matched by certificate designator
ATA 7712

Part: MODULE — FAILED (TORQUE INDICATOR)

TORQUE INDICATION STARTED TO FLUCTUATE. REMOVED NR 1 MODULE WHICH HOUSES THE TORQUE TUBE AND INSTALLED A RENTAL. SENT NR 1 OUT FOR REPAIR. IT WAS DETERMINED THAT THE ROLL PINS IN TORQUE TUBE HAD SHEARED OFF.

Source: SDR HXS2002F00002