N6094E

AEROSPATIALE AS350B2 · 1994 · 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 holder—Matched by certificate designator
SUTTON AGENCY,Operatoron 1973-11-26Operator named in NTSB report

Accident & incident history

Accident · 1973-11-26 Operator named in NTSB report
BEECH 35 Serious injury — SUTTON AGENCY,

Operated by SUTTON AGENCY, (per NTSB report)

Source: NTSB case MKC74AK027
BEECH K35 No injuries Part 91 — operator not named in the NTSB record
Source: NTSB case NYC68D0011

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, 2005-07-30 – 2008-09-29.

OTHER · 2008-09-29 Matched by certificate designator
ATA 6720

Part: BRACKET — CRACKED (RUDDER PEDALS)

ON THE BOTTOM SIDE OF THE FOOT PEDAL CONTROLS, ON THE RT PILOT SIDE, THE BRACKET THAT IS PART OF THE BELLCRANK ASSY, BRACKET PN 350A21-1313-24, HAS A CRACK IN IT. REMOVED BRACKET AND REPLACED WITH A SERVICEABLE BRACKET AND RETURNED AC TO SERVICE. THIS AC HAS BEEN PREVIOUSLY CONVERTED TO LT PILOT IN CHARGE SEAT IAW MFG MODIFICATIONS. THIS BRACKET IS WHAT HOLDS THE CENTERING ROD FOR THE FOOT PEDAL BELLCRANK IN THE FOOT PEDAL FLIGHT CONTROLS. (K)

Source: SDR HXS2008F00002
WARNING INDICATION · 2005-07-30 Matched by certificate designator
ATA 2612

Part: PROBE — FAULTY (FIRE DETECTION)

PILOT REPORTED THAT HIS FIRE INDICATION LIGHT HAD FLICKERED A COUPLE OF TIMES BUT THEN WENT AWAY. LIGHT WOULD NOT FLICKER ON THE GROUND WHILE NOT RUNNING. MECHANIC COULD NOT FIND THE FAULT. CLEANED THE CONNECTIONS AND FIRE DETECTION PROBES AND TRIED A RUN UP. FIRE LIGHT AGAIN FLICKERED A COUPLE OF TIMES THEN WENT OUT. TROUBLESHOOTING AGAIN FOUND A FIRE DETECTION PROBE TO BE PROBABLE. CHANGED THE PROBE AND AGAIN RAN UP THE AC. THIS TIME THE FIRE SYSTEM WORKED IAW THE MM. TOOK THE AC FOR A FLIGHT TO DETERMINE PROPER FUNCTION UNDER FLIGHT LOADS AND AGAIN THE SYSTEM WORKS IAW MM. RETURNED THE AC TO SERVICE. (K)

Source: SDR 2005FA0001318