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N881TW

Open the Markdown

2007 Pilatus PC-12/47 · Pratt & Whitney Canada PT6A-67B

Open in FAA registry

© OpenStreetMap
Registered owner
Hinterland Holdings LLC
Location
Anchorage, AK
Owner type
LLC
Serial number
806
Year built
2007
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
March 30, 2007
Certificate issued
February 13, 2026
Expires
February 28, 2033
Mode S code
AC234A
Pilatus PC-12/47Airframe model · 12 seats · 1 engine · 119 registeredTCDS A78EUAirframe · Pilatus PC-12/47TCDS E26NEEngine · Pratt & Whitney Canada PT6A-67B

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 15

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

1997In forceSuperseded2026
See all 22 ADs

Information bulletins that may apply · 3

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N881TWMatched 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 Pilatus PC-12/47 aircraft

FAA incident reports

No FAA accident or incident reports matched to N881TWMatched 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 Pilatus PC-12/47 aircraft

Service difficulty reports

No reports matched to N881TWGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Pilatus PC-12/47 aircraft
Reports on N881TW not matched to an aircraft · 8

They name N881TW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

SDR U5QA06022Flap · malfunctionedON FLIGHT FROM CMH TO SUA CREW OBSERVED A "FLAP FAIL" MESSAGE AT APPROX FLAP 20 DEGREE. CREW ELECTED TO DIVERT TO PBI FOR LONGER RUNWAY. MAINTENANCE WAS ABLE TO CLEAR SQUAWK BY RESETTING SYSTEM. FLAP SYSTEM OPERATING NORMAL.Dec 22, 2009 · N881TW · Cndair CL6002B16 · Trailing Edge Flap Control SystemSDR U5QA06021AAFlap System · malfunctionedON FLIGHT FROM CMH TO SUA CREW OBSERVED A "FLAP FAIL" MESSAGE AT APPROX FLAP 20 DEGREE. CREW ELECTED TO DIVERT TO PBI FOR LONGER RUNWAY. MAINTENANCE WAS ABLE TO CLEAR SQUAWK BY RESETTING SYSTEM. FLAP SYSTEM OPERATING NORMAL.Dec 22, 2009 · N881TW · Cndair CL6002B16 · Trailing Edge Flap Control SystemSDR 2009F00136Windshield · crackedIN CRUISE PILOTS WINDSHIELD CRACKED JUST RT OF CTR LINE FROM BOTTOM TO THE TOP OF THE PANE. DIVERTED FOR INSPECTION. MX INSPECTED AND APPLIED TAPE IAW CH56-10-01. MEL'D THE WINDSHIELD HEAT. CONTINUED ON.Dec 10, 2009 · N881TW · Cndair CL6002B16 · Wing Structure

STCs that may be installed · 123

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

See all 123 STCs