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N255MG

Open the Markdown

2011 Costruzioni Aeronautiche Tecna P2006T · Rotax 912S series

Open in FAA registry

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Registered owner
Central Valley Flight School LLC
Location
Hanford, CA
Owner type
LLC
Serial number
087/US
Year built
2011
Type
Fixed wing multi engine
Engine
4 cycle
Airworthiness
Standard, normal
Airworthiness date
January 20, 2012
Certificate issued
January 10, 2025
Expires
January 31, 2032
Mode S code
A26B2B
Costruzioni Aeronautiche Tecna P2006TAirframe model · 4 seats · 2 engines · 104 registeredTCDS A62CEAirframe · Costruzioni Aeronautiche Tecna P2006TTCDS E00051ENEngine · Rotax 912S series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Rotax 912S model are included below.

On this page

Airworthiness directives that may apply · 24

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

2002In forceSuperseded2026
See all 26 ADs

Information bulletins that may apply · 3

Advisory, not mandatory.

Historical bulletins · 1
SAIB NE-05-84Issued Aug 30, 2005

NTSB investigations

No NTSB investigations matched to N255MGMatched 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 Costruzioni Aeronautiche Tecna P2006T aircraft

FAA incident reports · 1

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

Incident 20170326006189ILanding: Rollout · Ogden, UTUpon landing the nose gear collapsed inside the nose gear well. The pilot stated that the landing was a smooth landing however when the weight of the aircraft settled on all the wheels the nose dropped. It was part 141 commercial training flight.Mar 26, 2017 · Minor damage

Service difficulty reports · 8

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

SDR 2020FA0000515Bracket · looseSUGGEST EMERGENCY AD. DURING 100 HOUR INSPECTION, LEFT ENGINE ALTERNATOR AND BELT WAS LOOSE ON ITS MOUNT WITH ALL HARDWARE TIGHT AND SECURE. REMOVAL REVEALED THE INTERNAL ALTERNATOR MOUNTING LUG HAD WORN TO EGG SHAPE AND MOUNTING BRACKET HOLES SYMMETRICALLY Nov 28, 2020 · N255MG · Tecnam P2006T · Electrical Power SystemSDR 2020FA0000514Bracket · damagedSUGGEST EMERGENCY AD. DURING 100 HOUR INSPECTION, LEFT ENGINE ALTERNATOR AND BELT WAS LOOSE ON ITS MOUNT WITH ALL HARDWARE TIGHT AND SECURE. REMOVAL REVEALED THE INTERNAL ALTERNATOR MOUNTING LUG HAD WORN TO EGG SHAPE AND MOUNTING BRACKET HOLES SYMMETRICALLY Nov 28, 2020 · N255MG · Tecnam P2006T · Electrical Power SystemSDR 2016FA0000365Strut · crackedDURING INSPECTION, SMALL CRACK DETECTED ON NOSE STRUT WHERE WELDS COME TOGETHER. THE CRACK ALLOWS NITROGEN AND HYDRAULIC FLUID TO ESCAPE LETTING THE STRUT GO FLAT. CRACK IS VISUAL AND DETECTABLE WITH LEAK CHECK. CRACK REQUIRES REPLACEMENT OF STRUT.Jul 28, 2016 · N255MG · Tecnam P2006T · Nose/Tail Landing Gear Strut/AxleSDR QFBR20140613003Nose Rib · crackedDURING 100HR INSPECTION OF AIRCRAFT 3 LEADING EDGE RIBS, ONE AT 83", ONE AT 97" AND ONE AT 110" FROM FUSELAGE CENTER (NO WING STATION GIVEN IN M/M) JUST OUTBOARD OF EACH ENGINE NACELLE WERE FOUND CRACKED AROUND LOWER AFT RIVET WHERE THEY CONNECT TO THE FORWARDJun 11, 2014 · N255MG · Tecnam P2006T · Wing, Rib/BulkheadSDR QFBR20140613004Nose Rib · crackedDURING 100HR INSPECTION OF AIRCRAFT 3 LEADING EDGE RIBS, ONE AT 83", ONE AT 97" AND ONE AT 110" FROM FUSELAGE CENTER (NO WING STATION GIVEN IN M/M) JUST OUTBOARD OF EACH ENGINE NACELLE WERE FOUND CRACKED AROUND LOWER AFT RIVET WHERE THEY CONNECT TO THE FORWARDJun 11, 2014 · N255MG · Tecnam P2006T · Wing, Rib/BulkheadSDR QFBR20140613002Nose Rib · crackedDURING 100HR INSPECTION OF AIRCRAFT, THREE LEADING EDGE RIBS, ONE AT 83", ONE AT 97" AND ONE AT 110" FROM FUSELAGE CENTER (NO WING STATION GIVEN IN M/M) JUST OUTBOARD OF EACH ENGINE NACELLE WERE FOUND CRACKED AROUND LOWER AFT RIVET WHERE THEY CONNECT TO THE FJun 11, 2014 · N255MG · Tecnam P2006T · Wing, Rib/BulkheadSDR QFBR20140613001Nose Rib · crackedDURING 100HR INSPECTION OF AIRCRAFT 3 LEADING EDGE RIBS, ONE AT 83", ONE AT 97" AND ONE AT 110" FROM FUSELAGE CENTER (NO WING STATION GIVEN IN M/M) JUST OUTBOARD OF EACH ENGINE NACELLE WERE FOUND CRACKED AROUND LOWER AFT RIVET WHERE THEY CONNECT TO THE FORWARDJun 11, 2014 · N255MG · Tecnam P2006T · Wing, Rib/BulkheadSDR 2012FA0000491Flex Hose · chafedLOWER ENGINE COOLANT HOSE AND EXHAUST SCAT HOSE ARE IN CONSTANT CONTACT DUE TO INSTALLATION DESIGN. CHAFING CAUSED WIRE FROM SCAT HOSE TO PUNCTURE LOWER COOLANT HOSE. SUBSEQUENT LOSS OF ALL COOLANT CAUSED ENGINE OVERHEATING. WHILE PILOT WAS DETERMINING CAUSEJul 16, 2012 · N255MG · Tecnam P2006T · Reciprocating Engine Liquid Cooling

STCs that may be installed · 17

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

See all 17 STCs