Location
Portland, OR
Owner type
Corporation
Serial number
550-0681
Year built
1992
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Restricted, other
Airworthiness date
February 13, 1992
Certificate issued
August 13, 2020
Expires
August 31, 2027
Mode S code
A05617

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada JT15D-4 model are included below.

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Airworthiness directives that may apply · 31

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

1975In forceSuperseded2026
ADs by the year they took effect: 32 ADs
19751
19781
19802
19882
19891
19902
19911
19932
19942
19951
19961
19982
19991
20012
20042
20063
20071
20131
20151
20231
20251
20261
See all 32 ADs

Information bulletins that may apply · 5

Advisory, not mandatory.

Historical bulletins · 2

NTSB investigations

No NTSB investigations matched to N1200NMatched 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 550 aircraft

FAA incident reports

No FAA accident or incident reports matched to N1200NMatched 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 550 aircraft

Service difficulty reports · 5

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

SDR 2006FA0001127Hinge · corrodedAT INSPECTION THE HINGE WAS FOUND CORRODED AND THE PINS WORN PAST LIMITS. A FACTORY NEW HINGE ASSY WAS ORDERED AND INSTALLED. UPON COMPLETION OF THE WORK THE AIRCRAFT WAS PRESSURIZED AND THE HINGE ASSY WAS FOUND TO BE LEAKING. UPON CLOSER INSPECTION THE SKIN TNov 27, 2006 · N1200N · Cessna 550 · Fuselage, Door HingeSDR B3OR20060111Terminal · misinstalledWIRE TERMINAL WAS IMPROPERLY CRIMPED ONTO WIRE INSULATION WITH STRIPPED END OF WIRE STRANDS CONTACTING TERMINAL SCREW AT VOLTAGE METER CIRCUIT BREAKER. THIS DISCREPANCY CAUSED AN INTERMITTENT VOLTAGE METER READING FAILURE.Apr 19, 2006 · N1200N · Cessna 550 · Electrical Power System WiringSDR 030926CWire Harness · chafedDURING INTERNAL INSPECTION OF THE FUEL BAYS FOUND FUEL PUMP WIRING HARNESSES IN RIGHT WING WAS DAMAGED BY CHAFFING THROUGH THE WIRING INSULATION TO BEAR WIRE. WIRING WAS CHAFFING AGAINST ALUMINUM FUEL LINE INSIDE TANK. CHAFFING CAUSED WEAR BEYOND LIMITS TO ASep 25, 2003 · N1200N · Cessna 550 · Fuel System WiringSDR 2002TU65Actuator · damagedON PREINSTALLATION INSPECTION, THE MECHANIC NOTICED DAMAGE IN THE ATTACH THREADS ON THE ACTUATOR. THE BOLT WOULD NOT THREAD IN EVEN ONE TURN WITH OUT BINDING. AFTER FURTHER INVESTIGATING IT WAS FOUND TO HAVE PART OF A BROKEN BOLT STILL INSIDE THE HOUSING.THIJan 7, 2002 · N1200N · Cessna 550 · Rudder ActuatorSDR 20001207SH001Screw · improper partUPON INSPECTION OF AREA UNDER HEATED LEADING EDGE (TOP FORWARD SCREW), IT WAS FOUND THAT THE SCREW HAD CONTACTED THE SKIN SURFACE. THE SCREW HAD PENETRATED PART OF A RIVET HEAD ON THE LEFT WING AND EXTENDED INTO THE SKIN APPROXIMATELY 0.032” INCH. THE SCREW Dec 5, 2000 · N1200N · Cessna 550 · Wing, Plate/Skin

STCs that may be installed · 328

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

See all 328 STCs