- Registered owners
- Kinney James RKinney Joan M
- Location
- Vermillion, SD
- Owner type
- Co-owned
- Serial number
- 04439
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- August 5, 1963
- Certificate issued
- March 31, 2011
- Expires
- March 31, 2030
- Mode S code
- A445B5
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 37
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1961 | 1 |
|---|---|
| 1963 | 1 |
| 1964 | 1 |
| 1966 | 3 |
| 1970 | 3 |
| 1971 | 2 |
| 1972 | 4 |
| 1975 | 1 |
| 1976 | 5 |
| 1977 | 3 |
| 1978 | 1 |
| 1979 | 1 |
Airframe · Dehavilland DH104 DOVE 6A
AD 79-02-07Wing to Fuselage AttachmentAD 78-09-04Main Spar Bottom Boom LugsAD 77-16-04Wing StructureInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N3745GMatched 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 Dehavilland DH104 DOVE 6A aircraft
FAA incident reports
No FAA accident or incident reports matched to N3745GMatched 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 Dehavilland DH104 DOVE 6A aircraft
Service difficulty reports
No reports matched to N3745GGeneral 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 Dehavilland DH104 DOVE 6A aircraft
STCs that may be installed · 49
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Dehavilland DH104 DOVE 6A
STC SA04776NYThe HIPEC Covering and Finishing System must be performed and maintainedSTC SA02283SE PAGE 2Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30PSTC SA02402SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C