# N26974: 1986 Fairchild SA227-AC, registration cancelled 2012-05-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 30, 2012
- Exported to: Bolivia
- Status when cancelled: Valid registration
- Airframe: [Fairchild SA227-AC](https://openairdocs.org/model/fairchild-sa227-ac) (registry code 3377509)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A8SW](https://openairdocs.org/tcds/A8SW) (OpenAirDocs)
- Serial number: AC-664
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, normal
- Airworthiness date: December 8, 1986
- Certificate issued: January 23, 2009
- Last registry action: April 29, 2010
- Mode S code: A2A3D6
- Owner when cancelled: [Coast Aviation Credit LLC](https://openairdocs.org/faa-owner/COAST%20AVIATION%20CREDIT%20LLC)
- Location: [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas)
- Owner type: Corporation
- Owner's area on the map: 36.0602° N, 115.2623° W: Placed by OpenAirDocs at the center of ZIP code 89113, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N26974
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=26974
- Page: https://openairdocs.org/deregistered/N26974-2012-05-30

From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Fairchild SA227-AC: https://openairdocs.org/model/fairchild-sa227-ac.md

## Service difficulty reports (6)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR LY02011F00001](https://openairdocs.org/sdr/LY02011F00001), Apr 22, 2011: ACCUMULATOR. CRACKED. DURING FLIGHT, THE ACFT HAD HYD LEAK DUE TO A CRACKING ON THE ACCUMULATOR. THE ACFT RETURNED TO DEPARTURE AND PERFORMED EMERGENCY PROCEDURES WITHOUT ANY PROBLEM
- [SDR LY02011F00000](https://openairdocs.org/sdr/LY02011F00000), Feb 14, 2011: PACKING. LEAKING. ACFT DURING ASCENT WITH ALTITUDE OF 6500 FT WAS EVIDENCE THE LOW OIL PRESSURE LIGHT ENG RT "TURN ON", AND THE OIL QTY INDICATOR TO ZERO. CABIN CREW AGREES TO SH
- [SDR SWIA95752](https://openairdocs.org/sdr/SWIA95752), Jul 24, 1996: STRUT. WORN. LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. INSPECTION OF AIRCRAFT DETECTED A FAULTY OUTBOARD GEAR SWITCH. REPLACED AND ADJUSTED PER 32-00-00, THE LEFT MAIN L
- [SDR SWIA95692](https://openairdocs.org/sdr/SWIA95692), Dec 12, 1995: POTENTIOMETER. DIRTY. AFTER TAKEOFF, GEAR HORN SOUNDED UPON RETRACTION. AT THIS POINT, IT WAS NOTICED THAT THE FLAP INDICATOR SHOWED FULL DOWN DEFLECTION, HOWEVER, FLAPS WERE RETRACT
- [SDR SWIA95628](https://openairdocs.org/sdr/SWIA95628), Sep 28, 1995: CONTL CABLES. OUT OF ADJUST. DURING PREFLIGHT CONTROL CHECK, FOUND EXCESSIVE PLAY IN CONTROLS, COPILOT WOULD MOVE WHILE CAPT WOULD REMAIN STATIONARY. INSPECTED AILERON CABLES FROM CONTROL C
- [SDR SWIA95607](https://openairdocs.org/sdr/SWIA95607), Jul 21, 1995: AWI SYST. MALFUNCTIONED. DURING TAKEOFF, AWI WAS TURNED ON, GOT BOTH LIGHTS BUT NO TORQUE RISE ON EITHER ENGINE. OPS CKS AWI SYSTEM ON GROUND, FOUND TO BE OPS NORMALLY AT THIS TIME.

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