- Registered owner
- Ocf Air LLC
- Location
- Phoenix, AZ
- Owner type
- LLC
- Serial number
- 2048
- Year built
- 2010
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- July 14, 2010
- Certificate issued
- October 28, 2022
- Expires
- October 31, 2029
- Mode S code
- A79141
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 26
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1981 | 1 |
|---|---|
| 1988 | 1 |
| 1991 | 1 |
| 1993 | 2 |
| 1998 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 3 |
| 2003 | 1 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 5 |
| 2009 | 1 |
| 2010 | 1 |
| 2012 | 2 |
| 2022 | 1 |
| 2023 | 3 |
| 2024 | 1 |
Airframe · Cirrus Design SR20
AD 2024-24-11Power LeverAD 2022-03-15Fuel Quantity IndicatorAD 2009-05-05Primary Flight DisplaysInformation bulletins that may apply · 19
Advisory, not mandatory.
See all 20 bulletins
NTSB investigations
No NTSB investigations matched to N587PUMatched 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 Cirrus Design SR20 aircraft
FAA incident reports
No FAA accident or incident reports matched to N587PUMatched 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 Cirrus Design SR20 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 2015FA0000559Keyway · wornDURING AN ACFT PROGRESSIVE 50 HOUR INSPECTION, DISCOVERED ALTERNATOR NR 2 COOLING FAN LOOSE ON ALTERNATOR SHAFT. THE FAN IS PART OF ALTERNATOR. THE KEY WAY OF THE FAN HUB WEARS PREMATURELY ALLOWING ROTATIONAL MOVEMENT OF THE FAN ON THE SHAFT. WE HAVE SEEN THSDR 2015FA0000568Pump · low pressureDURING A ACFT PROGRESSIVE INSPECTION, PROGRAM 50 HR INSPECTION DISCOVERED ENGINE FUEL FLOW TO BE LOW OUT OF LIMITS. IN THIS CASE WE WERE ABLE TO ADJUST THE FUEL FLOW TO WITHIN LIMITS IAW CMI SID97-3F. DURING FLIGHT CHECK IAW SID97-3, FUEL FLOW WAS LOW OUT OFSDR 2012FA0000036Exhaust Valve · bindingDURING A ROUTINE PRE-INSPECTION ENGINE RUN-UP, THE MX TECH DISCOVERED THAT THE ENGINE WAS RUNNING ROUGH AND WAS UNABLE TO REACH STATIC RPM. THE TECH ALSO NOTED LOW EGT ON CYLINDERS NR 1 AND NR 5. THE CYLINDER NR 1 AND NR 5 EXHAUST VALVE ROCKER COVERS AND EXHAU
STCs that may be installed · 138
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cirrus Design SR20
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