N408CT

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.

5 reports on file, 2007-05-16 – 2014-12-02.

WARNING INDICATION · 2014-12-02 Matched by certificate designator
ATA 3020

Part: VALVE — FAILED (ENGINE) · airframe 9,054 hrs · 6,662 cycles

VALVE FAILED TO EXTINGUISH ENGINE HEAT LIGHT IN FLIGHT. ITT RISE WHEN SELECTED. FAILED TO TEST ON GROUND. SWAPPED WITH OTHER SIDE AND PROBLEM INDICATION FOLLOWED. R & R VALVE. VALVE IN SERVICE 148 HOURS SINCE OVERHAUL. OBTAINED FROM MFG.

Source: SDR 2014FA0000685
OTHER · 2010-06-16 Unresolved
ATA 5210

Part: DOOR — LEAKING · airframe 8,198 hrs · 5,941 cycles

WHISTLING NOISE HEARD FROM CABIN DOOR AREA, AND 6000' IAW MINUTE CABIN PRESSURE CLIMB NOTICED WHILE AT CRUISE ALTITUDE OF 34,000'. EMERGENCY DESCENT PERFORMED.

Source: SDR T17A408CT6/16
OTHER · 2009-09-11 Unresolved
ATA 3222

Part: FORK — BROKEN (NLG) · airframe 8,091 hrs · 5,862 cycles

NOSE GEAR FORK BROKE AT LT AXLE ATTACH POINT. IT IS SUSPECTED A PREVIOUS ANTI-ICE FLUID (TKS) LEAK IN THE NOSE AREA HAD DILUTED THE WHEEL BEARING GREASE AND CAUSED CORROSION TO SEIZE THE BEARING.

Source: SDR T17A408CT9/29
OTHER · 2007-05-16 Unresolved
ATA 3418

Part: COMPUTER — DEFECTIVE (STICK SHAKER) · airframe 6,897 hrs · 5,085 cycles

STICK SHAKER DID NOT ACTIVATE WHEN DOING STALL RECOGNITION/RECOVERY TRAINING.

Source: SDR 5083
WARNING INDICATION · 2007-05-16 Unresolved
ATA 3418

Part: COMPUTER — DEFECTIVE (STALL WARNING) · airframe 6,897 hrs · 5,085 cycles

STICK SHAKER DID NOT ACTIVATE WHEN DOING STALL RECOGNITION/RECOVERY TRAINING.

Source: SDR 01