# N15SK: Autogyro Certification CALIDUS

- Status: Valid registration
- Airframe: [Autogyro Certification CALIDUS](https://openairdocs.org/model/autogyro-certification-calidus) (registry code 7730116, 2 seats)
- Data sheets: [TCDS R00006RD](https://openairdocs.org/tcds/R00006RD) (AutoGyro Certification Limited) (OpenAirDocs)
- Serial number: C00606
- Type: Gyroplane
- Engine type: Reciprocating
- Certificate issued: August 24, 2026
- Expires: August 31, 2033
- Mode S code: A0C970
- Registered owner: [Kelly Stacy L](https://openairdocs.org/faa-owner/KELLY%20STACY%20L)
- Location: [N Richland Hills, TX](https://openairdocs.org/faa-place/TX/N%20Richland%20Hills)
- Owner type: Individual
- Owner's area on the map: 32.8865° N, 97.2081° W: Placed by OpenAirDocs at the center of ZIP code 76182, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=15SK
- Page: https://openairdocs.org/aircraft/N15SK

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 1 in force

### Matched by airframe (Autogyro Certification CALIDUS)

- [AD 2022-13-07](https://openairdocs.org/ad/2022-13-07): Main Rotor Blades · AutoGyro Certification Calidus, Cavalon and MTOsport 2017. Effective Jul 7, 2022

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N15SK.

## FAA accident and incident reports

None matched to N15SK.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N15SK not matched to an aircraft (9)

They name N15SK, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR IMJ2007F00000](https://openairdocs.org/sdr/IMJ2007F00000), Apr 18, 2007: ELBOW. CRACKED. DURING AN ENGINE REPLACEMENT (INSTALLATION OF A RENTAL ENGINE WHILE THE ORIGINAL ENGINE IS BEING OVERHAULED) WE CAREFULLY EXAMINED THE BLEED AIR ELBOW ASSY FOR 
- [SDR IMJ2006F00000](https://openairdocs.org/sdr/IMJ2006F00000), Jan 1, 2006: CLAMP. FAILED. AIRCRAFT MASTER CAUTION AND CABIN ABOVE 10,000 SEGMENT ILLUMINATED AND PAX OXYGEN MASKS DROPPED. EMERGENCY DECLARED, AIRCRAFT DESCENDED AND RETURNED TO DEPARTUR
- [SDR IMJ2005F00000](https://openairdocs.org/sdr/IMJ2005F00000), Jan 11, 2005: ELBOW. RUPTURED. AC FAILURE OF NR2 ENG OB BRAIDED BLEED AIR LINE. FAILURE HAPPENED ABOUT 5 MIN AFTER T/O, WHILE INITATING A CLIMB FROM 2000 FT TO 6000 FT. FIRE WARNING ANNUN ILL
- [SDR IMJ2004F00000](https://openairdocs.org/sdr/IMJ2004F00000), Nov 18, 2003: RELAY. CONTAMINATED. ON TAXI (POWER BRAKE) AND (ANTI SKID) LIGHTS ILLUMINATED INTERMITTENTLY. FOUND ANTI SKID RELAY TO BE AT FAULT. SUSPECT THAT SKYDROL HAD MIGRATED INTO THE RELAY 
- [SDR IMJ2004F00002](https://openairdocs.org/sdr/IMJ2004F00002), Jul 21, 2003: INVERTER. FAILED. NR 2 INVERTER FAILED INTERMITTNETLY IN FLIGHT.
- [SDR 2003F00357](https://openairdocs.org/sdr/2003F00357), Apr 24, 2003: PACKING. LEAKING. ON FINAL APPROACH TO KTEB, BOTH THE POEWR BRAKE AND ANTI-SKID LIGHTS ILLUMINATED. DIVERTED TO KEWR, TO TAKE ADVANTAGE OF GREATER RUNWAY LENGTH. AFTER LANDING MA
- [SDR 2003F00329](https://openairdocs.org/sdr/2003F00329), Mar 30, 2003: PACKING. LEAKING. ON TAXI OUT, PILOTS AND CO-PILOTS BRAKES FAILED. FOUND HYDRAULIC FLUID LEAK AT THE HYDRAULIC POWER PACK FILTER BOWL. (M)
- [SDR IMJ2002F00001](https://openairdocs.org/sdr/IMJ2002F00001), Sep 23, 2002: FIRE LOOP. CHAFED. FIVE MINUTES AFTER DEPARTURE, LT FIRE LIGHT ILLUMINATED. DECLARED EMERGENCY, ACCOMPLISHED CHECKLIST, (DISCHARGED BOTH FIRE BOTTLES AND SECURED NR 1 ENGINE). DIV
- [SDR BV92001F00000](https://openairdocs.org/sdr/BV92001F00000), Nov 27, 2001: WIRE. CHAFED. AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. FOUND WIRE BUNDLE IN LEFT WHEEL WELL CHAFED ON HYDRAULIC LINE.

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Autogyro Certification CALIDUS aircraft: https://openairdocs.org/model/autogyro-certification-calidus/aircraft.md

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