- Registered owner
- Schellhorn Friedrick
- Location
- Harxheim/Mainz, DE
- Owner type
- Individual
- Serial number
- 337-0696
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- May 10, 1967
- Certificate issued
- December 16, 1992
- Expires
- April 30, 2029
- Mode S code
- A1EA6D
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 17
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1967 | 1 |
|---|---|
| 1970 | 1 |
| 1971 | 1 |
| 1977 | 1 |
| 1978 | 2 |
| 1987 | 1 |
| 1988 | 1 |
| 1990 | 1 |
| 1997 | 1 |
| 2000 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 1 |
| 2022 | 1 |
| 2023 | 2 |
See all 19 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
Airframe · Cessna T337B
SAIB AIR-21-16FLIGHT COMPARTMENT EQUIPMENT, Cessna Seat Back Attachment Bolt InspectionSAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-12-14Three Alternative Methods of Compliance for AD 2011-10-09SAIB CE-10-40R1Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanesSAIB CE-09-10Availability of Secondary Seat Stops for Pilot and Copilot SeatsNTSB investigations
No NTSB investigations matched to N222WKMatched 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 T337B aircraft
FAA incident reports
No FAA accident or incident reports matched to N222WKMatched 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 T337B aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 20010305CW007Pump · leakingWITH A HIGHWING TANK CONNECTED TO THE FUEL PUMP INLET PORT, THE NONE DRIVEN FUEL PUMP LEAKS REGARDLESS THE MIXTURE LEVER POSITION. WITH THE MIXTURE LEVER IN IDLE CUT OFF, THE FUEL FLOW IS THE SAME AS IN FULL RICH. 3 TO 4MM/0.012 TO 0.016IN/ AWAY FROM THE IDLSDR 20010305CW006Pump · leakingWITH A HIGHWING TANK CONNECTED TO THE FUEL PUMP INLET PORT, THE NONE DRIVEN FUEL PUMP LEAKS REGARDLESS THE MIXTURE LEVER POSITION. WITH THE MIXTURE LEVER IN IDLE CUT OFF, THE FUEL FLOW IS THE SAME AS IN FULL RICH. 3 TO 4 MM/0.012IN TO 0.016IN/ AWAY FROM THE SDR 20010305CW005Pump · failedHIGHWING TANK CONNECTED TO THE FUEL PUMP INLET PORT. THE NONE DRIVE FUEL PUMP LEAKS REGARDLESS THE MIXTURE LEVER POSITION. WITH MIXTURE LEVER IN IDLE CUTOFF, FUEL FLOW IS SAME AS IN FULL RICH. 3 TO 4 MM/0.012IN TO 0.016IN AWAY FROM THE IDLE CUT OFF STOP, THSDR 20010305CW008Pump · leakingWITH HIGHWING TANK CONNECTED TO THE FUEL PUMP INLET PORT, THE NONE DRIVEN FUEL PUMP LEAKS REGARDLESS THE MIXTURE LEVER POSITION. WITH THE MIXTURE LEVER IN IDLE CUT OFF, THE FUEL FLOW IS THE SAME AS IN FULL RICH. 3 TO 4MM/0.012IN TO 0.016IN/ AWAY FROM THE IDLSDR 20010305CW010Pump · leakingFUEL PUMP LEAKS THROUGH OUTLET PORT, WITH FUEL SELECTOR VALVE IN ON POSITION, WITH HIGHWING TANK CONNECTED TO FUEL PUMP INLET PORT, THE NONE DRIVEN FUEL PUMP LEAKS REGARDLESS THE MIXTURE LEVER POSITION. WITH MIXTURE LEVER IN IDLE CUT OFF, THE FUEL FLOW IS THESDR 20010305CW009Pump · leakingTESTED FUEL PUMP, MOTOR DRIVEN FUEL PUMP REACHED SPECIFIED CALIBRATING VALUES. WITH HIGHWING TANK CONNECTED TO THE FUEL PUMP INLET PORT, THE NONE DRIVEN FUEL PUMP LEAKS REGARDLESS THE MIXTURE LEVER POSITION THROUGH THE OUTLET PORT. WITH MIXTRUE LEVER IN IDL
STCs that may be installed · 189
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna T337B
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