- Registered owner
- Siderius Construction Llp
- Location
- Kalispell, MT
- Owner type
- Partnership
- Serial number
- 0026A
- Year built
- 2000
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- September 29, 2000
- Certificate issued
- January 5, 2018
- Expires
- January 31, 2028
- Mode S code
- A4C32E
From the FAA registry file of October 21, 2026.
On this page
Airworthiness directives that may apply · 24
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 |
| 1996 | 1 |
| 1998 | 1 |
| 1999 | 3 |
| 2000 | 1 |
| 2001 | 1 |
| 2003 | 1 |
| 2005 | 4 |
| 2006 | 2 |
| 2010 | 1 |
| 2013 | 1 |
| 2015 | 3 |
| 2017 | 2 |
| 2018 | 2 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
See all 32 ADs
Information bulletins that may apply · 2
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N406CSMatched by N-number and event date. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Schweizer 269D aircraft
FAA incident reports
No FAA accident or incident reports matched to N406CSMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Schweizer 269D aircraft
Service difficulty reports · 7
SDR Z5FA071411N406CS1Smoke Detector · faultyDURING DESCENT, CREW RECEIVED BAGGAGE SMOKE LIGHT. CREW RAN THE CHECKLIST AND DECLARED AN EMERGENCY. THEY DIVERTED AND WERE MET BY EMERGENCY VEHICLES. THE LANDING WAS UNEVENTFUL WITH NO SIGN OF FIRE. INSPECTED ACFT AND FOUND NO VISIBLE SIGNS OF SMOKE OR FIRESDR Z5FA060910N406CS1Brake Sys · intermittentON ROLL-OUT AFTER LANDING, AS ACFT WAS SLOWING, CREW EXPERIENCED INTERMITTENT LOSS OF BRAKING FOR 1 TO 2 SECONDS. CREW TAXIED TO FBO CAUTIOUSLY AND STOPPED WITHOUT INCIDENT. MX INSPECTED SYS AND FAULT INDICATIONS WITH NO FAULTS FOUND. BRAKES WERE BLED AND CSDR Z5FA010309N406CS1Warning System · malfunctionedON CLIMB OUT, WHEN GEAR WAS RETRACTED, CREW NOTICED GEAR UNLOCK LIGHT STILL ON. CREW DIVERTED, DECLARED AN EMERGENCY AND LANDED SAFELY, BUT OVERWEIGHT. MX FACILITY SWUNG GEAR AND WAS UNABLE TO DUPLICATE REPORTED DISCREPANCY. ALL UP-LOCK SWITCHES AND WIRING WERSDR 7282008N406CSControl Cable · chafedELEVATOR TRIM CABLE CHAFED ON PULLEY BRACKET P/N 6361201-1 IN VERTICAL STABILIZER. ENGINEERING ORDER WRITTEN TO ADD FAIRLEADS TO PREVENT FURTHER CHAFING. (S)SDR 3302008N406CSPcb · burned outDURING APPROACH, WHEN LANDING GEAR WAS SELECTED DOWN, THE DOWN AND LOCKED GREEN LIGHTS DID NOT ILLUMINATE ALTHOUGH THE GEAR FELT LIKE IT EXTENDED. THE GEAR WAS BLOWN DOWN BUT THE INDICATION DID NOT APPEAR. THE COCKPIT FLOOD LIGHTS WERE SELECTED AND THE DOWN ANSDR 050807N406CS1Unknown · unknownON DESCENT INTO CYYZ THE BAGGAGE SMOKE LIGHT ILLUMINATED. NO VISUAL OR ODOR OF SMOKE WAS DETECTED BY THE FLIGHT CREW. THE CREW DECLARED AN ENERGENCY AND DIVERTED TO BUF. LANDING WAS UNEVENTFUL. NO SIGNS OF SMOKE OR FIRE INSIDE THE BAGGAGE COMPARTMENT WAS DETECSDR 33106N406CS1Engine · malfunctionedEN ROUTE FROM PHX TO LAN,THE CREW NOTICED LOW AND FLUCTUATING OIL PRESSURE ON RIGHT ENGINE. DURING DESCENT, THE LOW OIL PRESSURE LIGHT ILLUMINATED. THE CREW THEN ELECTED TO DECLARE AN EMERGENCY AND SHUT DOWN THE RIGHT ENGINE. ATC DIVERTED THEM TO GRR AND TH