Owner type
Corporation
Serial number
SH3623
Type
Fixed wing multi engine
Engine
Turbo-prop
Certificate issued
April 8, 1996
Expires
March 31, 2030
Mode S code
A7CB29

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 0

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

No ADs matched this aircraft’s modelsADs on appliances, propellers and installed equipment aren’t matched by model; check those separately.

Information bulletins that may apply

Advisory, not mandatory.

No bulletins matched this aircraft’s models

NTSB investigations

No NTSB investigations matched to N601CAMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Short Bros SHORTS SD3-60 aircraft

FAA incident reports · 3

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Reports on N601CA not matched to an aircraft · 2

They name N601CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

Service difficulty reports · 7

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR DATA20210921001Fitting · corrodedWHILE PERFORMING AN INSPECTION OF THE VERTICAL STABILIZER ATTACH FITTING PER AD 2005-13-31 AND SERVICE BULLETIN SD360-53-45, FOUND CORROSION ON SHEAR ATTACHMENT FITTING P/N SD3-12-6978. FITTING WAS REMOVED AND REPLACED WITH NEW FITTING IAW SB SD360-53-45 AND ASep 17, 2021 · N601CA · Stbros SD360 · Vertical Stabilizer, Attach FittingsSDR DATA20210921002Torque Tube · corrodedWHILE PERFORMING AN INSPECTION FOUND HEAVY CORROSION ON RUDDER TORQUE TUBE. RUDDER TORQUE TUBE WAS REPLACED WITH A NEW UNIT AND AIRCRAFT RETURNED TO SERVICE.Sep 16, 2021 · N601CA · Stbros SD360 · Rudder StructureSDR DATA2014121801Accumulator · leakingSHORTLY AFTER TAKEOFF, HYD LT CWP LIGHT ILLUMINATED. CREW DISCUSSED THE ISSUE & RETURNED TO BASE & SWAPPED PLANES. UPON TROUBLESHOOTING, MAINTENANCE DISCOVERED THE FLAP ACCUMULATOR TO HAVE AN INTERNAL LEAK. ACCUMULATOR WAS REPLACED. OPERATIONS CHECKED SATISDec 18, 2014 · N601CA · Stbros SD360 · Hydraulic Power Accumulator, MainSDR DATA20130812003Downlock Switch · faultyDURING APPROACH, CREW SELECTED LANDING GEAR DOWN. RT MAIN SHOWED UNSAFE. CREW ABORTED APPROACH AND PERFORMED QRH PROCEDURES TO ATTEMPT TO REMEDY THE PROBLEM. UNSAFE INDICATION REMAINED, CREW DECLARED AN EMERGENCY. LANDING PROCEEDED WITHOUT INCIDENT. THE UNSAAug 7, 2013 · N601CA · Stbros SD360 · Landing Gear Position and WarningSDR DATA20110000002Control Cable · brokenDURING FLIGHT CONTROL CHECK PRIOR TO TAKEOFF, FLAPS WERE OPERATED FULL DOWN. LEFT FLAP DID NOT RETRACT WHEN COMMANDED TO FULL UP POSITION. MAINTENANCE OBSERVED LEFT FLAP CABLE BROKEN IN TRAILING EDGE OF WING NEAR FLAP SELECTOR VALVE.Mar 9, 2011 · N601CA · Stbros SD360 · Trailing Edge Flap Control SystemSDR DAT2005F00007Tire · failedAC HAD NORMAL STARTUP, TAXI OUT AND WAS CLEARED FOR TAKEOFF. FO WAS FLYING, CAPTAIN SET THE POWER, MADE THE CALLOUTS AND HAD JUST FINISHED SAYING (AIRSPEED ALIVE) WHEN FLIGHT CREW HEARD AN EXPLOSION, FELT THE LT WING DIP JUST AFTER A SLIGHT LT YAW. FLIGHT CRJul 7, 2005 · N601CA · Stbros SD360 · TireSDR 98ZZZX1168Timer · failedTHE TAIL DE-ICE BOOTS WERE INOPERABLE DURING THE FLIGHT. THE DE-ICE TIMER WAS REPLACED. OPS CHECK GOOD.Feb 9, 1998 · N601CA · Stbros SD360 · Airfoil Anti/De-ice System

STCs that may be installed

No STCs matched this aircraft’s modelsSTCs are matched through the model’s type certificate data sheet, and this registry model isn’t matched to one.