- Registered owner
- Corporate Flight Inc
- Location
- Waterford, MI
- Owner type
- Corporation
- Serial number
- 550-0238
- Year built
- 1980
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- January 22, 1981
- Certificate issued
- February 6, 1997
- Expires
- July 31, 2029
- Mode S code
- A1A117
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.
On this page
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.
| 1975 | 1 |
|---|---|
| 1978 | 1 |
| 1980 | 2 |
| 1988 | 2 |
| 1989 | 1 |
| 1990 | 2 |
| 1991 | 1 |
| 1993 | 2 |
| 1994 | 2 |
| 1995 | 1 |
| 1996 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2001 | 2 |
| 2004 | 2 |
| 2006 | 3 |
| 2007 | 1 |
| 2013 | 1 |
| 2015 | 1 |
| 2023 | 1 |
| 2025 | 1 |
| 2026 | 1 |
See all 32 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
Historical bulletins · 2
NTSB investigations
No NTSB investigations matched to N204CFMatched 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 N204CFMatched 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 · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR BTAA20200810001Pressure Switch · failedTHE PRESSURE SWITCH FAILED INTERMITTENTLY WHICH IS CONTROLLING THE GROUND FOR THE RELAY TO TURN ON AND OFF THE HYDRAULIC PUMP MOTOR TO GIVE THE AIRCRAFT POWER BRAKES. ON LANDING THE BRAKES FELT SOFT BUT STOPPED THE AIRCRAFT JUST FINE (ALSO HAD THRUST REVERSERSDR BTAA2013F00001Skin · corrodedLEFT WING L/E SKIN UNDER DE-ICING BOOT CORRODED. BLENDED OUT CORROSION AND FOUND REMAINING SKIN THICKNESS UNDER MINIMUMS. CUTOUT DAMAGE SKINS AND PERFORMED REPLACEMENT IAW ACFT SRM 57-20-07.SDR BTA2004F00000Seat · crackedUPPER CHAIR BASE ASSY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. CHAIR WAS REPAIRED IAW STC ST01042WI STRUCTURAL SEAT REPAIR.SDR 2004FA0000003Seat · crackedUPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. CHAIR WAS REPAIRED IAW STC ST01042WI STRUCTURAL SEAT REPAIR.
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.
Airframe · Cessna 550
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST01823WIInstallation of Garmin GTS Traffic Sensor with Garmin GTX 3000 Mode S Transponders with ADS-B Out.