- Owner type
- Individual
- Serial number
- S1SS-4
- Year built
- 2019
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Experimental, amateur built
- Airworthiness date
- May 13, 2020
- Certificate issued
- November 12, 2025
- Expires
- November 30, 2032
- Mode S code
- A2A625
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Superior IO-360 model are included below.
On this page
Airworthiness directives that may apply · 3
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2008 | 1 |
|---|---|
| 2009 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2021 | 1 |
Engine · Superior IO-360 series
AD 2020-25-12Reciprocating Engine Power SectionAD 2012-03-06Fuel servo diaphragmAD 2009-02-03Fuel injection servosSuperseded and historical ADs · 3
Information bulletins that may apply · 1
Advisory, not mandatory.
Engine · Superior IO-360 series
SAIB NE-09-04Fuel Control/Reciprocating EnginesNTSB investigations
No NTSB investigations matched to N27WPMatched 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 William M Oprendek PITTS S1S aircraft
FAA incident reports
No FAA accident or incident reports matched to N27WPMatched 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 William M Oprendek PITTS S1S aircraft
Service difficulty reports
No reports matched to N27WPGeneral 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 William M Oprendek PITTS S1S aircraft
Reports on N27WP not matched to an aircraft · 2
They name N27WP, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2009FA0001025Outflow Valve · defectiveDURING APPROACH AT 4000MSL THE PILOT LOST PRESSURIZATION CONTROL IN THE AUTO AND MANUAL MODE. A "MAX DIFF" CAS MESSAGE WAS DISPLAYED.SDR 20000517SH001Sensor · looseFLIGHT CREW REPORTED ENCOUNTERING COMPRESSOR STALLS AND AIRCRAFT YAW TO LEFT CLIMBING THROUGH FL 230. LEFT ENGINE CONTROLS MOVED TO FLIGHT IDLE AND SHUT DOWN LT ENGINE. FLIGHT DIVERTED TO LIT DASSAULT SERVICE CENTER. INVESTIGATION REVEALED T2 SENSOR CONNECT
STCs that may be installed · 4
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · Superior IO-360 series
STC SE04651CHTo allow use of l00R grade aviation fuel meeting Swift Fuel, LLC specification SPEC-l00R-22STC SE04349CHInstallation of SureFly electronic ignitionSTC SE04577CHInstall an electronic engine ignition systemSTC SE02409AKInstallation of the Superior Air Parts Cold Air Induction System (CAIS)
Earlier aircraft with this N-number · 1
This aircraft carried N27WP before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.