Registered owner
Pa1 208b-0566 LLC
Owner type
LLC
Serial number
208B0566
Year built
1996
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
December 11, 1996
Certificate issued
September 12, 2026
Expires
September 30, 2033
Mode S code
A0618C

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 26

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

1988In forceSuperseded2026
ADs by the year they took effect: 32 ADs
19881
19902
19961
19972
19982
20012
20021
20031
20042
20052
20063
20071
20083
20093
20121
20141
20151
20211
20221
20231
See all 32 ADs

Information bulletins that may apply · 5

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N1232YMatched 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 Cessna 208B aircraft

FAA incident reports

No FAA accident or incident reports matched to N1232YMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 208B aircraft

Service difficulty reports · 6

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

SDR ENHA LP230674Autopilot Sys · activatedAUTOPILOT ENGAGED AND DISCONNECTED 3 TIMES. HAD TO PULL CIRCUIT BREAKER. MECHANICS RAN SELF TEST AND FOUND ELECTRONIC STABILITY AND PROTECTION (ESP) ENABLED AND WORKING NORMALLY. REF POH AND GFC600 PILOTS GUIDE 2.6.May 23, 2023 · N1232Y · Cessna 208B · Auto Flight SystemSDR EPUA20151022001Skin · crackedRIGHT WING LE EDGE SKIN WAS FOUND CRACKED DURING A PHASE INSPECTION. THE CRACK ORIGINATED FROM THE FIRST ROUND INSPECTION PANEL NEAR WS 60.0, ON THE BOTTOM SIDE OF THE LE. ENGINEERING APPROVAL FOR REPAIR WAS OBTAINED & A REPAIR FOR THE AREA WAS PUT IN PLACE,Oct 19, 2015 · N1232Y · Cessna 208B · Wing, Plate/SkinSDR EPUA201505042015Probe · defectiveWHILE INFLIGHT PILOT NOTICED HIGH ITT, ACFT RETURNED TO BASE. INSPECTED INDICATING SYS & FOUND TRIM PROBE STICK BAD. REPLACED AFFECTED PROBE. OPERATIONS CHECKED GOOD.May 4, 2015 · N1232Y · Cessna 208B · Engine EGT/TIT Indicating SystemSDR EPUA20130730001Brake Assy · brokenPILOT REPORTED LOCKED BRAKE ON LANDING. ACFT STOPPED ON THE SIDE OF THE RUNWAY AND WAS UNABLE TO TAXI OFF THE RUNWAY. FOUND LT TIRE WORN, LT BRAKE CALIPER WITH BROKEN AND MISSING SLIDE PINS, LT TORQUE PLATE BUSHING WORN OUT, AND BOTH LT AND RT BRAKE PADS WORN Jul 28, 2013 · N1232Y · Cessna 208B · Landing Gear Brake SystemSDR 2007FA0000981Relief Valve · separatedRELIEF VALVE FOR BLEED AIR PNEUMATIC SYSTEM END WASHER AND CAP SEPARATED FROM VALVE AND LAYING IN BOTTOM OF COWLING. SUSPECT RIVET HOLDING PARTS ON IS TOO SOFT. THIS IS THE THIRD VALVE TO FAIL LIKE THIS ON DIFFERENT AIRCRAFT IN THE LAST MONTH. AND ALL WERE NNov 3, 2007 · N1232Y · Cessna 208B · Vacuum Distribution SystemSDR 2005FA0001056Antenna · inoperativeFOUND LOWER UAT ANTENNA UNSERVICEABLE DURING UAT UPGRADE. (K)Apr 29, 2005 · N1232Y · Cessna 208B · Central Display

STCs that may be installed · 306

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 306 STCs