- Registered owner
- Sh1p Holdings LLC
- Location
- Wichita, KS
- Owner type
- LLC
- Serial number
- 58-855
- Year built
- 1958
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- November 7, 1984
- Certificate issued
- May 23, 2026
- Expires
- May 31, 2033
- Mode S code
- A07655
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 25
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1960 | 2 |
|---|---|
| 1966 | 1 |
| 1975 | 3 |
| 1976 | 1 |
| 1977 | 2 |
| 1978 | 3 |
| 1979 | 1 |
| 1982 | 1 |
| 1986 | 1 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 2 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 1 |
| 2021 | 1 |
| 2023 | 1 |
| 2024 | 1 |
Airframe · Sikorsky S-58JT
AD 2024-12-10Main Rotor Drive SystemAD 2023-11-07Ground Proximity SystemAD 95-26-08Main Rotor ShaftInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N129NHMatched 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 Sikorsky S-58JT aircraft
FAA incident reports
No FAA accident or incident reports matched to N129NHMatched 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 Sikorsky S-58JT aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR NYBA9712Ring Gear · making metalGEARBOX RING GEAR CAUSING METAL GENERATION. REPLACEDSDR 96ZZZX4781Engine · stallsDURING HIGH POWER DEMANDS, COMPRESSOR STALLS NOTED BY PILOT. DURING ACCELERATION CHECKS ON GROUND, MECHANIC NOTED COMPRESSOR STALLS. NYH BELIEVES THE COMPRESSOR STALLS ARE DUE TO DAMAGED 1ST STAGE COMPRESSOR BLADES (FOD). POWER SECTION REMOVED IAW S58T MM A
STCs that may be installed · 26
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.