- Registered owner
- Ultra Aviation Management Inc
- Location
- Miami, FL
- Owner type
- Corporation
- Serial number
- 404-0417
- Year built
- 1979
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- April 17, 1979
- Certificate issued
- October 6, 2014
- Expires
- October 31, 2027
- Mode S code
- A5E7D1
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 20
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1978 | 2 |
|---|---|
| 1980 | 3 |
| 1984 | 1 |
| 1986 | 1 |
| 1989 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 2 |
| 2000 | 1 |
| 2001 | 1 |
| 2005 | 2 |
| 2023 | 2 |
See all 20 ADs
Information bulletins that may apply · 7
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N48SAMatched 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 404 aircraft
FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20160802013519ILanding: Rollout · Miami, FLAirman said runway had standing water which caused the aircraft to hydroplane resulting in loss of directional control. Aircraft veered left onto grassy area. No damage to airport or aircraft resulted.Accident 19950905027879ALa Verne, CADuring landing rollout, right main gear collapsed, aircraft slid off runway into a field.Incident 19851001055189INormal Cruise · Reno, NVEngine shutdown after oil pressure decay and visible oil leak. Safe landing. Gasket on starter adapter ruptured.
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 97ZZZX2670Gear Pin · wornDURING A RECENT 404 TITAN GEAR INSPECTION ON THE MAIN LANDING GEAR, FOUND TRAILING LINK PIVOT PINS WORN EXCESSIVELY. THE PHENOLIC-LINED BUSHINGS WERE SITHIN MANUFACTUER'S SPECS. NEW PINS WERE INSTALLED.SDR 97ZZZX2669Gear Pin · wornDURING A RECENT 404 TITAN GEAR INSPECTION ON THE MAIN LANDING GEAR, FOUND TRAILING LINK PIVOT PINS WORN EXCESSIVELY. THE PHENOLIC-LINED BUSHINGS WERE WITHIN MANUFACTUER'S SPECS. NEW PINS WERE INSTALLED.SDR 97ZZZX2668Hiloks · looseDURING A RECENT MDL 404 GEAR INSPECTION, NOTED THE NOSE GEAR ACTUATOR ATTACH STRUCTURE HAD NUMEROUS LOOSE HI-LOKS.SDR 96ZZZX6100Fuel Control · defectivePILOT REPORTED ENGINE STUMBLE ON TAKEOFF AND AT CLIMB POWER SETTING. EXTENSIVE TROUBLESHOOTING FOUND LOOSE BUSHING AT RIGHT ENGINE. MIXTURE CONTROL SHAFT INSTALLED USED SERVICEABLE FUEL CONTROL ASSY. TEST FLOWN OK.SDR 96ZZZX3319Cylinder · head crackedFOUND NR 2 CYLINDER HEAD CRACKED AT LOWER SPARK PLUG HOLE.SDR 96ZZZX2986Exhaust Riser · misoverhauledRECEIVED OVERHAULED EXHAUST RISER FROM OVERHAULER. DURING INSPECTION PRIOR TO INSTALLATION, FOUND MOUTH FOR SLIP JOINT MANUFACTURED TOO SMALL AND NOT ALLOWING SLIP JOINT TUBE TO SLIDE IN. SUSPECT CAUSE IS POOR MANUFACTURING AND QUALITY CONTROL PRACTICES. SUSDR 96ZZZX2509Lift Detector · shortedAFTER FLIGHT THROUGH RAIN, WATER ENTERS LIFT DETECTOR AND CAUSES STALL WARNING HORN TO SOUND CONTINUOUSLY. UNIT IS NOT EASY TO DRY OUT REQUIRING REPLACEMENT. SUBMITTER STATED THIS IS A RECURRING PROBLEM. RECOMMEND IMPROVED INTERNAL SEALING OF LIFT DETECTOR.SDR 96ZZZX1271Relay · failedLEFT ENGINE STARTER BURNED UP DUE TO RUNNING CONTINUOUSLY DUE TO RELAY STICKING. POOR DIAGNOSIS CAUSED STARTER TO BE REPLACED WITHOUT REPLACING SOLENOID. SECOND STARTER FAILED ALSO. SAME CONDITION. RELAY REPLACED WITH SECOND NEW STARTER. SUBMITTER SUGGESTSDR 95ZZZX6054Hose · rupturedLEFT MAIN GEAR 'UP' HYDRAULIC LINE HOSE SEPARATED FROM END FITTING. HYDRAULIC FLUID DUMPED OVERBOARD. PILOT BLEW GEAR 'DOWN' WITH NITROGEN BOTTLE. HOSE HAD BEEN FABRICATED FROM NEW PARTS 65 HOURS PREVIOUSLY.SDR 95ZZZX5634Cooler · crackedOIL COOLER CRACKED UNDER NORMAL CONDITIONS, LEAKING OIL. SUBMITTER SUGGESTS RE-DESIGN COOLER.
STCs that may be installed · 157
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 404
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller