- Registered owner
- Murphy Dale
- Location
- Pagosa Springs, CO
- Owner type
- Individual
- Serial number
- 938
- Year built
- 1936
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- January 16, 1961
- Certificate issued
- March 2, 2021
- Expires
- March 31, 2028
- Mode S code
- A07A5C
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental A40 model are included below.
On this page
Airworthiness directives that may apply · 1
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1993 | 1 |
|---|---|
| 2000 | 1 |
| 2014 | 1 |
Airframe · Piper J-2
AD 99-26-19 R1WingsSuperseded and historical ADs · 2
Information bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Piper J-2
SAIB ACE-99-01NTSB investigations
No NTSB investigations matched to N13RNMatched 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 J-2 aircraft
FAA incident reports
No FAA accident or incident reports matched to N13RNMatched 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 J-2 aircraft
Service difficulty reports
No reports matched to N13RNGeneral 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 J-2 aircraft
STCs that may be installed · 22
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Piper J-2
STC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specificationSTC SA01734SEApplication of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.STC SA00780SEInstallation of the True Lock Safety Retention Axle Lock Nut System