- Registered owner
- Joey Os LLC
- Location
- Darlington, PA
- Owner type
- LLC
- Serial number
- 27-2818
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Certificate issued
- March 5, 2021
- Expires
- March 31, 2028
- Mode S code
- A345F2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 48
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1964 | 1 |
|---|---|
| 1966 | 1 |
| 1968 | 1 |
| 1971 | 5 |
| 1972 | 2 |
| 1973 | 1 |
| 1974 | 3 |
| 1975 | 2 |
| 1976 | 3 |
| 1977 | 2 |
| 1978 | 2 |
| 1979 | 3 |
| 1980 | 1 |
| 1981 | 2 |
| 1982 | 1 |
| 1989 | 1 |
| 1993 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 2 |
| 2000 | 1 |
| 2003 | 1 |
| 2005 | 4 |
| 2006 | 2 |
| 2009 | 1 |
| 2011 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2022 | 2 |
| 2023 | 1 |
See all 52 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N31RCMatched 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 Piper PA-23-250 aircraft
FAA incident reports
No FAA accident or incident reports matched to N31RCMatched 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 Piper PA-23-250 aircraft
Service difficulty reports
No reports matched to N31RCGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Piper PA-23-250 aircraft
Reports on N31RC not matched to an aircraft · 4
They name N31RC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 99ZZZX6Igniter · damagedDURING PHASE B INSPECTION, FOUND LEFT ENGINE INBOARD IGNITER CENTER ELECTRODE LOOSE IN IGNITER BODY. ELECTRODE IS FREE TO MOVE IN AND OUT IGNITER BODY APROXIMATELY .3125 INCH. IGNITER HAS NORMAL WEAR AND NO OTHER APPARENT DAMAGE.SDR 98ZZZX878Coupling · crackedDURING ENGINE CHANGE, FOUND BLEED AIR CLAMP CRACKED IN RADIUS OF BOLT GUIDE SLEEVE, ALMOST COMPLETELY AROUND THE CIRCUMFERENCE.SDR 95ZZZX789Step Assy · block brokeUPON STOWING OF STEP ASSY, DETENT BLOCK SUPPORT BROKE. FOUND EXCESSIVE WEAR ON DETENT BLOCK CATCHES AND BLOCK. SUBMITTER SUGGESTS MORE FREQUENT LUBE OF CATCHES AND BETTER DEFINITION OF ALLOWABLE WEAR.
STCs that may be installed · 436
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Piper PA-23-250
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