- Registered owner
- Dodson International Parts Inc
- Location
- Rantoul, KS
- Owner type
- Corporation
- Serial number
- 5500243
- Year built
- 1981
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 17, 2004
- Certificate issued
- May 6, 2025
- Expires
- May 31, 2032
- Mode S code
- A8DAF5
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada JT15D 5 model are included below.
On this page
Airworthiness directives that may apply · 29
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1980 | 2 |
|---|---|
| 1988 | 1 |
| 1989 | 1 |
| 1990 | 2 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 2 |
| 1994 | 2 |
| 1995 | 1 |
| 1996 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2001 | 2 |
| 2004 | 2 |
| 2006 | 3 |
| 2007 | 1 |
| 2009 | 1 |
| 2013 | 1 |
| 2015 | 1 |
| 2023 | 1 |
| 2025 | 1 |
| 2026 | 1 |
See all 31 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
Airframe · Cessna 550
SAIB AIR-21-15R1Navigation SystemSAIB NM-14-08Fuselage: Aerodynamic FairingsSAIB CE-12-19Fuel: Aircraft Fuel System on Cessna Model 500/501/550 AirplanesSAIB CE-10-49R1Equipment/Furnishings Drain Mast HeaterSAIB NM-10-13Navigation: Flight Management SystemEngine · Pratt & Whitney Canada JT15D 5 series
SAIB NE-07-03Dual-engine flameoutsHistorical bulletins · 2
NTSB investigations
No NTSB investigations matched to N67SFMatched 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 N67SFMatched 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
Reports on N67SF not matched to an aircraft · 1
They name N67SF, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR SFOA20110106001Door · out of adjustTHE AIRCRAFT TOOK OFF AND MADE A NORMAL CLIMB TO CRUISE ALTITUDE. AFTER A FEW MINUTES IT WAS NOTED THAT THE LANDING GEAR UNLOCK AND HYD PRESS ON ANNUNCIATORS ILLUMINATED, A THUMP/BUMP WAS HEARD AND FELT, AFTER WHICH THE ANNUNCIATORS EXTINGUISHED. THIS HAPPENSDR SFOA67Wire · chafedDURING POST ENGINE START/PREFLIGHT CHECKS, NOTED THE "SPEED BRAKE EXTENDED" ANNUNCIATOR FAILED TO ILLUMINATE. VISUAL INSPECTION CONFIRMED THE BRAKES EXTENDED, & "HYD PRESS" LIGHT EXTINGUISHED CONFIRMING SYS HAD COMPLETED IT’S CYCLE. ANNUNCIATOR LIGHT TEST PERSDR 2008FA0000500Wire · chafedON CLIMB OUT, AFTER DEPARTURE, THE LT THRUST REVERSER DEPLOY LIGHT ILLUMINATED. NO ABNORMAL FLIGHT CHARACTERISTICS WERE FELT IN THE AC. AFM PROCEDURES WERE FOLLOWED AND A SAFE LANDING BACK AT DEPARTURE AIRPORT WAS MADE. AFTER LANDING, THE PILOT CYCLED THE L
Reports on N67SF not matched to an aircraft · 5
They name N67SF, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 20001227SH014Valve · failedPILOT REPORTED THE EMERGENCY PRESSURIZATION WAS COMING ON WHEN THE WING DEICE WAS SWITCHED ON. NO INDICATION ON ANNUNCIATOR PANEL TO INDICATE EITHER OF THE EMERGENCY PRESS SYSTEMS BEING ACTIVATED. DISCOVERED THE RT EMERG PRESSURIZATION VALVE WAS LEAKING BY ASDR 20001017SH027Actuator · brokenAFTER LANDING, HYD FLUID FOUND LEAKING FROM RT MLG DOOR, RT INBD WING. INVEST REVEALED THE OTBD RT MLG RETRACT/EXTEND ACTUATOR HAD BROKEN AT WING ATTACH FITTING , INBD (RETRACT) HYD FITTING BENT. ACT HOUSING WAS DAMAGED AT FITTING PORT DUE TO MOVEMENT OF ACTSDR 98ZZZX91Hose · leakingCREW COMPLAINED OF FUEL ODOR IN AFT BAGGAGE COMPT. INVEST REVEALED A FUEL HOSE LEAKING THRU OUTER JACKET. HOSE IS APPROX 16 INCHES LONG AND LOCATED ABOVE RT FWD CEILING OF AFT BAGGAGE COMPT BETWEEN APU FUEL SHUT-OFF VALVE AND A UNION. THE OTHER SIDE IS ATT
STCs that may be installed · 325
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.