# N681SA: 1995 Saab 2000

- Status: Valid registration
- Airframe: [Saab 2000](https://openairdocs.org/model/saab-2000) (registry code 7860202, 60 seats)
- Engine: [Allison AE-2100A](https://openairdocs.org/engine/allison-ae-2100a) (registry code 03042)
- Data sheets: [TCDS A38CE](https://openairdocs.org/tcds/A38CE) (Textron Aviation Inc.), [TCDS TE1CH](https://openairdocs.org/tcds/TE1CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 2000-021
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: March 14, 2008
- Certificate issued: April 22, 2025
- Expires: April 30, 2032
- Mode S code: A9087F
- Registered owner: [Aleutian Airways LLC](https://openairdocs.org/faa-owner/ALEUTIAN%20AIRWAYS%20LLC)
- Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage)
- Owner type: LLC
- Owner's area on the map: 61.1637° N, 149.9966° W: Placed by OpenAirDocs at the center of ZIP code 99502, 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=681SA
- Page: https://openairdocs.org/aircraft/N681SA

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): 13 in force

### Matched by airframe (Saab 2000)

- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2003-02-03](https://openairdocs.org/ad/2003-02-03): Airstair door and emergency exits · Textron 100, 200, 2000 and 46 more. Effective Mar 7, 2003
- [AD 99-10-06](https://openairdocs.org/ad/99-10-06): Wing Cove Skin · Textron 2000. Effective Jun 3, 1999
- [AD 99-02-14](https://openairdocs.org/ad/99-02-14): Inspect Engine Stainless Steel Fuel Line · Textron 2000. Effective Mar 5, 1999
- [AD 98-04-25](https://openairdocs.org/ad/98-04-25): Airplane Flight Manual - Icing · Textron 2000. Effective Mar 13, 1998
- [AD 97-25-03](https://openairdocs.org/ad/97-25-03): AFM - Limitations - Power Levers · Textron 100, 1900, 1900C and 44 more. Effective Jan 21, 1998
- [AD 97-25-01](https://openairdocs.org/ad/97-25-01): Outflow/Safety Valve · Textron 100, 200, 2000 and 38 more. Effective Jan 11, 1998
- [AD 96-22-12](https://openairdocs.org/ad/96-22-12): Inspect fuel filter assembly · Textron 1900C, 1900C (C-12J), 1900D and 1 more. Effective Dec 13, 1996

### Matched by engine (Allison AE-2100A)

- [AD 2020-22-18](https://openairdocs.org/ad/2020-22-18): Turbine Engine Reduction Gear · Rolls-Royce AE 2100A, AE 2100D2, AE 2100D2A and 1 more. Effective Dec 15, 2020
- [AD 2001-17-31](https://openairdocs.org/ad/2001-17-31): Second Stage High Pressure Turbine Wheel · Rolls-Royce AE 2100A, AE 2100C, AE 2100D3 and 2 more. Effective Oct 5, 2001
- [AD 99-17-09](https://openairdocs.org/ad/99-17-09): Propeller Gearbox (PGB) and Power Section (P/S) Strut Fittings · Rolls-Royce AE 2100A and AE 2100C. Effective Sep 7, 1999
- [AD 99-03-09](https://openairdocs.org/ad/99-03-09): Turbine wheel failure · Rolls-Royce AE 2100A, AE 2100C and AE 2100D3. Effective Feb 19, 1999

### Historical (superseded or no longer in force)

- [AD 96-17-10](https://openairdocs.org/ad/96-17-10) (historical): Outflow/Safety Valve · Raytheon 200 Model or Series (all), 2000, 300 and 5 more. Effective Sep 24, 1996

## Information bulletins (advisory) (1 in force)

- [SAIB CE-02-19](https://openairdocs.org/saib/CE-02-19): . Issued Mar 11, 2002

## NTSB investigations

None matched to N681SA.

## FAA accident and incident reports

None matched to N681SA.

## Service difficulty reports (6)

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

- [SDR 4VAA202603310005](https://openairdocs.org/sdr/4VAA202603310005), Mar 31, 2026: LIGHT. FAILED. DURING INSPECTION, THE EMERGENCY LIGHTING FORWARD FLOOR STRIP DID NOT COME ON WHEN COCKPIT OR THE FLIGHT ATTENDANT SWITCH WAS SELECTED ON. THE FORWARD FLOOR PRO
- [SDR 4VAA202603310004](https://openairdocs.org/sdr/4VAA202603310004), Mar 31, 2026: POWER SUPPLY. FAILED. DURING INSPECTION, THE EMERGENCY LIGHT POWER SUPPLY 11LB FAILED A FUNCTIONAL CHECK. THE POWER SUPPLY WAS REPLACED IN ACCORADANCE WITH THE SAAB AMM. OPERATIONAL 
- [SDR 4VAA202604020003](https://openairdocs.org/sdr/4VAA202604020003), Mar 31, 2026: POWER SUPPLY. FAILED. DURING INSPECTION, THE EMERGENCY LIGHT LOWER LEFT HAND FAILED A FUNCTIONAL CHECK. FURTHER, THE EMERGENCY LIGHT POWER SUPPLY 15LN FAILED A FUNCTIONAL CHECK. THE 
- [SDR 4VAA20241015007](https://openairdocs.org/sdr/4VAA20241015007), Oct 15, 2024: SUPPORT BRACKET. CORRODED. R/H NACELLE ENGINE FIRE EXTINGUISHER BOTTLE SUPPORT BRACKET HAS CORROSION. REPLACED PER WORLDWIDE AIRCRAFT SERVICES ENGINEERING ORDER
- [SDR 4VAA20241015006](https://openairdocs.org/sdr/4VAA20241015006), Oct 15, 2024: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTING POWER SUPPLY BATTERY 17LN FAILED FUNCTION TEST. REPLACED WITH SERVICEABLE UNIT.
- [SDR 4VAA202407291003](https://openairdocs.org/sdr/4VAA202407291003), Jul 21, 2024: RELAY. FAILED. DURING INSPECTION, THE CREW NOTED CIRCUIT BREAKER E9 WAS OUT. THE CIRCUIT BREAKER WAS RESET. DURING THE RESET THE FA PANEL EMERGENCY PUSH BUTTON LIGHT FLASHED A

## STCs that may be installed (OpenAirDocs) (22)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Saab 2000)

- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA00292AT](https://openairdocs.org/stc/SA00292AT): Installation of an aircraft security system. (Starship I). Textron Aviation Inc
- [STC SA00300AT](https://openairdocs.org/stc/SA00300AT): Installation of a side facing lavatory seat. Textron Aviation Inc
- [STC SA00358AT](https://openairdocs.org/stc/SA00358AT): Installation of a Collins HF-9000system. Textron Aviation Inc
- [STC SA01681AT](https://openairdocs.org/stc/SA01681AT): Replacement of nickel cadnium battery with a Concorde model RG380E/60L. Textron Aviation Inc
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation
- [STC SA00243BO](https://openairdocs.org/stc/SA00243BO): Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200). Icarus Avionics, LLC
- [STC SA02110CH](https://openairdocs.org/stc/SA02110CH): Installation of a Time Trac Data Recorder. P2 Incorporated
- [STC SA01917SE](https://openairdocs.org/stc/SA01917SE): ONE ONLY STC, NC-51: Non-group aircraft approval for Reduced Vertical Separation Minimum (RVSM). AeroMech Incorporated
- [STC SA01846SE](https://openairdocs.org/stc/SA01846SE): Non-group aircraft approval for Reduced Vertical Separation Minimum (RVSM). AeroMech Incorporated
- [STC SA01847SE](https://openairdocs.org/stc/SA01847SE): Non-group aircraft approval for Reduced Vertical Separation Minimum (RVSM). AeroMech Incorporated
- [STC SA01473SE](https://openairdocs.org/stc/SA01473SE): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc
- [STC SA01814SE](https://openairdocs.org/stc/SA01814SE): One Only STC-Serial Number NC-50: Non-group (individual) aircraft approval for Reduced Vertical Separation Minimum (RVSM). AeroMech Incorporated
- [STC SA01487SE](https://openairdocs.org/stc/SA01487SE): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision. Garmin AT Inc
- [STC SA00937WI-D](https://openairdocs.org/stc/SA00937WI-D): Modification of Collins GPS-4000 Global Positioning Sensor installation to a Collins GPS-4000A Global Positioning Sensor installation. Rockwell Collins Inc
- [STC SA00749AT](https://openairdocs.org/stc/SA00749AT): Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent). Aero Trim, Inc
- [STC ST00791AT](https://openairdocs.org/stc/ST00791AT): Modification to the right hand engine start circuit to keep the cockpit instrumentation from dropping out during engine start. Piedmont Avn Services, Inc
- [STC SA01933LA](https://openairdocs.org/stc/SA01933LA) (historical): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin AT Inc

## Earlier aircraft with N681SA

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N681SA before.

- [Cancelled 2012-09-28](https://openairdocs.org/deregistered/N681SA-2012-09-28): Bombardier CL-600-2B19, S/N 7653. Exported to Canada. Owner: [Canoga Capital Corp Trustee](https://openairdocs.org/faa-owner/CANOGA%20CAPITAL%20CORP%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)

## Related

- Other Saab 2000 aircraft: https://openairdocs.org/model/saab-2000/aircraft.md
- The Allison AE-2100A engine: https://openairdocs.org/engine/allison-ae-2100a.md

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