- Registered owner
- Dls Holdings Inc
- Location
- Lewes, DE
- Owner type
- Corporation
- Serial number
- 0008
- Year built
- 1995
- Type
- Rotorcraft
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- September 14, 1995
- Certificate issued
- February 8, 2017
- Expires
- February 28, 2030
- Mode S code
- A800C2
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming HO-360 model are included below.
On this page
Airworthiness directives that may apply · 23
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1976 | 1 |
|---|---|
| 1977 | 1 |
| 1981 | 1 |
| 1982 | 1 |
| 1989 | 1 |
| 1991 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1999 | 2 |
| 2000 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 3 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2015 | 1 |
| 2017 | 2 |
| 2021 | 1 |
| 2023 | 1 |
| 2024 | 1 |
| 2026 | 1 |
Airframe · Schweizer 269C-1
AD 2023-11-07Ground Proximity SystemAD 2017-14-06Main Rotor Drive SystemAD 2015-23-01Tail Rotor DriveInformation bulletins that may apply · 8
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N61458Matched 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 269C-1 aircraft
FAA incident reports
No FAA accident or incident reports matched to N61458Matched 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 269C-1 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 97ZZZX3449Cover Assy · jammed throttleFLIGHT AFTER ANNUAL INSP FOR M/R TRACK AND BALANCE, THROTTLE STUCK FULL ON IN CRUISE FLT NOT ALLOWING REDUCTION IN POWER WITHOUT OVERSPEED OF ENG AND ROTOR. CAUSE FOUND IN-FLIGHT AND CORRECTED. BETWEEN PILOT'S AND COPILOT'S SEAT IS A VERTICAL PANEL THAT WHENSDR 95ZZZX6340Plug · missingLOWER PULLEY (CRANK) PLUG MISSING. STANDARD OIL PLUG INSTALLED IN ENGINE. LYCOMING P/N 77416 SHOULD BE INSTALLED IN ENGINES ON 269 SERIES HELICOPTERS PER LYCOMING SI 1180B. INSTALLED SCHWEIZER PLUG, PN 269A5513.
STCs that may be installed · 82
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 82 STCs