- Registered owner
- Patterson Frederick W III
- Location
- American Canyon, CA
- Owner type
- Individual
- Serial number
- 150
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Certificate issued
- November 14, 2011
- Expires
- November 30, 2027
- Mode S code
- A39401
From the FAA registry file of October 22, 2026.
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.
| 1976 | 1 |
|---|---|
| 1979 | 1 |
| 1996 | 1 |
Airframe · Bellanca CH300 PACEMAKER
AD 96-12-22Full Flow Engine Oil AdapterAD 79-07-02BatteriesAD 76-20-07Wood Decayed Wing SparsInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N33FPMatched 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 Bellanca CH300 PACEMAKER aircraft
FAA incident reports
No FAA accident or incident reports matched to N33FPMatched 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 Bellanca CH300 PACEMAKER aircraft
Service difficulty reports
No reports matched to N33FPGeneral 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 Bellanca CH300 PACEMAKER aircraft
STCs that may be installed · 6
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Bellanca CH300 PACEMAKER
STC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specificationSTC SA02825NY PAGE 1Installation of Aerospace Logic Aircraft InstrumentsSTC SA4005NMPrecise Flight Inc. Pulselite Control SystemSTC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.STC SA931NWInstallation of Hayes Industries tapered axles to accommodate Hayes 27 inch wheel assemblies (PN G31A), Hayes 11 x 2 brake assembly (PN H-12-19), Warner Aircraft brake master cylinders (PN 3150-5) and associated tires and plumbingSTC SA4-320Installation of Edo 6470 Floats