- Serial number
- 5500597
- Year built
- 1989
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 11, 1998
- Certificate issued
- October 1, 2022
- Expires
- October 31, 2029
- Mode S code
- A1C580
- Registered owner
- N213js LLC
- Location
- Lewes, DE
- Owner type
- LLC
From the FAA registry file of October 20, 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. Not a compliance determination.
| 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. Matched the same way as ADs.
Historical bulletins · 2
NTSB investigations
No NTSB investigations matched to N213JSMatched by N-number and event date. 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 N213JSMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 550 aircraft
Service difficulty reports · 2
SDR 2009F00017Uplock Switch · malfunctionedAFTER TAKEOFF, GEAR WAS SELECTED UP. THE GEAR INDICATION SHOWED THAT THE RT MAIN GEAR DID NOT RETRACT. THE GEAR HANDLE WAS THEN SELECTED DOWN AND ALL (3) GEAR SHOWED DOWN AND LOCKED. ACFT WAS THEN LANDED NORMALLY.SDR ESE2004F00000Connector · inoperativeA FIRE WARNING OCCURRED DURING CLIMBOUT. ON THE RT ENGINE. NO EMERGENCY DECLARED. AIRCRAFT MADE A PRECAUTIONARY LANDING. NO SECONDARY INDICATION OF MALFUNCTION WERE EVIDENT. CREW COULD NOT DUPLICATE PROBLEM. RT ENGINE FIRE DETECTOR CONNECTOR.