- Registered owner
- Kuydendall David E
- Location
- Roland, IA
- Owner type
- Individual
- Serial number
- 239
- Year built
- 1965
- Type
- Glider
- Engine
- None
- Airworthiness
- Standard, utility
- Airworthiness date
- March 16, 1966
- Certificate issued
- June 29, 2017
- Expires
- June 30, 2027
- Mode S code
- ADD590
From the FAA registry file of October 24, 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.
| 1987 | 1 |
|---|---|
| 1988 | 2 |
Airframe · Schweizer SGU 2-22E
AD 87-17-01Tow Release InstallationAD 76-13-11 R1Aft Fuselage LongeronsAD 87-02-01Tow-Release Installation InspectionInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N9904JMatched 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 Schweizer SGU 2-22E aircraft
FAA incident reports
No FAA accident or incident reports matched to N9904JMatched 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 Schweizer SGU 2-22E aircraft
Service difficulty reports
No reports matched to N9904JGeneral 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 Schweizer SGU 2-22E aircraft
STCs that may be installed · 5
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Schweizer SGU 2-22E
STC SA01734SEApplication of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.STC SG01164CHInstall Cooper superflite 102 fabric.STC SA1351WEReplace existing fabric on wings, fuselage, empennage, and/or control surfaces, with Ceconite101 material. (262A Series -12)STC SG10WEReplace existing fabric on wings, fuselage, empennage, and/or control surfaces with Ceconite103 material.STC SG4-1240Installation of Eonnex cover on aircraft surfaces.