- Registered owner
- Spartan Education LLC
- Location
- Tulsa, OK
- Owner type
- LLC
- Serial number
- 4496019
- Year built
- 1997
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- October 14, 1997
- Certificate issued
- January 7, 2013
- Expires
- January 31, 2029
- Mode S code
- ACE1FF
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O&VO-360 model are included below.
On this page
Airworthiness directives that may apply · 65
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1963 | 1 |
|---|---|
| 1964 | 1 |
| 1966 | 1 |
| 1967 | 1 |
| 1969 | 2 |
| 1977 | 2 |
| 1979 | 5 |
| 1980 | 6 |
| 1981 | 4 |
| 1982 | 1 |
| 1988 | 1 |
| 1989 | 2 |
| 1991 | 1 |
| 1992 | 1 |
| 1994 | 2 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 2 |
| 1998 | 2 |
| 2000 | 1 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 4 |
| 2006 | 5 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 3 |
| 2012 | 2 |
| 2013 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2021 | 1 |
| 2022 | 2 |
| 2024 | 2 |
| 2026 | 1 |
Airframe · Piper PA-44-180
AD 2024-10-04Wing, Attach FittingsAD 2022-03-15Fuel Quantity IndicatorAD 2015-26-08Rudder Control SystemInformation bulletins that may apply · 21
Advisory, not mandatory.
See all 30 bulletins
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2010FA0000270Rotor Shaft · shearedROTOR SHAFT SHEARED AT SPLIT FOR POINT CAM.SDR 2009FA0000928Shaft · shearedROTOR SHAFT SHEARED AT SPLIT FOR POINT CAM. MFG IS AWARE OF DEFECT DURING MFG OF ROTOR. (K)SDR 2009FA0000831Control Cable · frayedCABLE IS FRAYED WHERE IT PASSES NEXT TO THE FLAP SELECTOR HANDLE UNDER THE CENTER FLOORBOARD TUNNEL. DIFFICULT TO SEE DEFECT WITHOUT REMOVING FLAP SELECTOR HANDLE. CABLE FRAYED APPROX 50 PERCENT AT THIS LOCATION. IT IS NOTED THAT WHEN THE FLAP IS EXTENDED TSDR 2002FA0001397Control Cable · brokenDURING 100 HOUR INSPECTION, FOUND THAT THE FOLLOWING CONTROL CABLE WHERE BROKEN ON THE ENGINE SIDE WHERE TWO PIECES OF SHROUD OF SWAGED TOGETHER.SDR 2002FA0001396Control Cable · brokenDURING 100 HOUR INSPECTION, FOUND THAT THE FOLLOWING CONTROL CABLES WHERE BROKEN ON THE ENGINE SIDE WHERE TWO PIECES OF SHROUD OF SWAGED TOGETHER.SDR 2002FA0001395Control Cable · brokenDURING 100 HOUR INSPECTION FOUND THAT THE FOLLOWING CONTROL CABLES WERE BROKEN ON THE ENGINE SIDE WHERE TWO PIECES OF SHROUD OF SWAGED TOGETHER.SDR 2002FA0001394Control Cable · brokenDURING 100 HOUR INSPECTION, FOUND THAT THE FOLLOWING CONTROL CABLES WERE BROKEN ON THE ENGINE SIDE WHERE TWO PIECES OF SHROUD OF SWAGED TOGETHER.SDR 2002FA0001393Control Cable · brokenDURING 100 HOUR INSPECTION FOUND THAT THE FOLLOWING CONTROL CABLE WHERE BROKEN ON THE ENGINE SIDE WHERE TWO PIECES OF SHROUD OF SWAGED TOGETHER. PROBABLE CAUSE MAY BE DUE TO THE WAY THE CABLES ARE ROUTED.SDR 2002FA0001077Pushrod · bentTHE NUMBER 2 CYLINDER EXHAUST PUSH ROD BENT IN FLIGHT.SDR 2001FA0000302Tube · crackedFOUND NR 3 INTAKE TUBE LEAKING AT 100 HOUR INSPECTION. REMOVED TUBE AND FOUND A CRACK AT FLANGE CRACK APPEARS TO HAVE BEEN REPAIRED BUT WELD DOESNT COVER THE WHOLE CRACK.SDR 99ZZZX1065Stop · brokenPLASTIC STOP PLATE ASSY BROKE AT BOTTOM OF PLATE ON EACH SIDE DIRECTLY UNDER LT AND RT PROP CONTROL LEVERS. THE BROKEN PIECES WERE RETAINED BY THE SPRING WHICH IS PART OF THE ASSY. THESE PIECES PIVOT UP AND OUT WHEN THE PROP LEVERS WERE MOVED TO FEATHER. THSDR 98ZZZX2358Heat Box · brokenDURING ROUTINE 100-HOUR INSPECTION, FOUND RT ENGINE CARBURETOR HEAT AIRBOX BROKEN AT THE CARBURETOR HEAT INLET TUBE. PREVIOUS 100-HOUR INSPECTION FOUND LT ENGINE AIRBOX IN SAME CONDITION. AIRCRAFT TOTAL TIME 195.0 HRS. TOTAL TIME ON PREVIOUS AIRBOX, 99.6 HRSDR 98ZZZX918Harness · arcedSEVERAL LOUD POPS WERE HEARD IN THE TAILCONE OF THE AIRCRAFT WHEN THE STROBE LIGHTS WERE TURNED ON. INSPECTION OF STROBE POWER SUPPLY WIRING REVEALED BARE WIRES WHERE THE EXTERIOR INSULATION HAD BEEN STRIPPED. THE GRAY INSULATION WAS STRIPPED BY A TOOL THAT
STCs that may be installed · 249
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-44-180
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
Earlier aircraft with this N-number · 1
This aircraft carried N9290P before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.