- Registered owners
- Youngs William D JrYoungs Carol J
- Location
- Moravia, NY
- Owner type
- Co-owned
- Serial number
- D-4955
- Year built
- 1957
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard
- Airworthiness date
- February 9, 1957
- Certificate issued
- September 12, 2013
- Expires
- September 30, 2029
- Mode S code
- A92D22
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental O-470 model are included below.
On this page
Airworthiness directives that may apply · 55
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 |
|---|---|
| 1965 | 1 |
| 1967 | 1 |
| 1969 | 2 |
| 1970 | 1 |
| 1972 | 3 |
| 1973 | 1 |
| 1975 | 2 |
| 1979 | 1 |
| 1980 | 1 |
| 1981 | 2 |
| 1984 | 1 |
| 1985 | 1 |
| 1988 | 1 |
| 1989 | 2 |
| 1991 | 1 |
| 1993 | 2 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 2 |
| 1997 | 3 |
| 1998 | 1 |
| 1999 | 2 |
| 2000 | 3 |
| 2001 | 2 |
| 2002 | 1 |
| 2003 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 2 |
| 2009 | 1 |
| 2010 | 2 |
| 2022 | 3 |
| 2023 | 6 |
| 2024 | 1 |
See all 67 ADs
Information bulletins that may apply · 10
Advisory, not mandatory.
Airframe · Beech H35
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-12-36Flight Controls: AileronSAIB CE-12-18Flight Controls: Elevator Control Cable ConditionSAIB CE-11-21Flight Controls: Trailing Edge Flaps; Flap Nose Rib CrackingSAIB CE-09-02Publication error of AD 89-05-02 in the FAA Regulatory Guidance LibraryEngine · Continental O-470 series
SAIB NE-20-05POWERPLANT - Engine Camshaft Gear Tooth FractureSAIB NE-16-13Powerplant - Prohibited use of sealantSAIB NE-13-04Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing InspectionSAIB NE-10-09Reciprocating Engine Power Section: Hydraulic Valve LiftersSAIB NE-09-08Reciprocating Engine Cylinder SectionNTSB investigations
No NTSB investigations matched to N6900VMatched 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 Beech H35 aircraft
FAA incident reports
No FAA accident or incident reports matched to N6900VMatched 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 Beech H35 aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 99ZZZX32Blade · corrodedTHE BLADE WAS FOUND TO HAVE CORROSION BELOW THE PITCH LINES IN THE THREADS. SUBMITTER STATED THIS MAY HAVE BEEN PREVENTED IF THE RECOMMENDED TBO'S WERE FOLLOWED.SDR 99ZZZX31Blade · corrodedTHE BLADE WAS FOUND TO HAVE CORROSION BELOW THE PITCH LINE IN THE THREADS. SUBMITTER STATED THIS MAY HAVE BEEN PREVENTED IF THE RECOMMENED TBO'S WERE FOLLOWED.SDR 99ZZZX30Hub · corrodedTHE HUB WAS FOUND TO HAVE CORROSION IN THE RETENTION THREADS BEYOND ACCEPTABLE LIMITS. SUBMITTER STATED THIS MAY HAVE BEEN PREVENTED IF MAINTAINED ON THE RECOMMENDED TBO'S.
STCs that may be installed · 557
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech H35
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