# N749SA: 1994 Saab SAAB 2000

- Status: Valid registration
- Airframe: [Saab SAAB 2000](https://openairdocs.org/model/saab-saab-2000) (registry code 7860007, 58 seats)
- Engine: [Rolls-Royce AE-2100A](https://openairdocs.org/engine/rolls-royce-ae-2100a) (registry code 54140)
- Data sheets: [TCDS A47NM](https://openairdocs.org/tcds/A47NM) (Saab AB), [TCDS TE1CH](https://openairdocs.org/tcds/TE1CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 2000-055
- Year built: 1994
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: August 16, 2023
- Certificate issued: March 24, 2025
- Expires: March 31, 2032
- Mode S code: AA158A
- 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=749SA
- Page: https://openairdocs.org/aircraft/N749SA

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): 83 in force

### Matched by airframe (Saab SAAB 2000)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2024-15-12](https://openairdocs.org/ad/2024-15-12): Time Limits/Maintenance Checks · Saab SAAB 2000. Effective Oct 23, 2024
- [AD 2023-25-06](https://openairdocs.org/ad/2023-25-06): Landing gear · Saab AB Support and Services SAAB 2000. Effective Feb 7, 2024
- [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 2021-09-11](https://openairdocs.org/ad/2021-09-11): Landing gear · Saab AB, Saab Aeronautics SAAB 2000. Effective Jul 29, 2021
- [AD 2021-02-02](https://openairdocs.org/ad/2021-02-02): Landing gear · Saab AB, Saab Aeronautics SAAB 2000. Effective Mar 29, 2021
- [AD 2020-25-02](https://openairdocs.org/ad/2020-25-02): Landing Gear · Saab AB, Saab Aeronautics SAAB 2000, 340A (SAAB SF340A) and SAAB 340B. Effective Jan 21, 2021
- [AD 2020-21-02](https://openairdocs.org/ad/2020-21-02): Fire protection · Airbus Canada Limited Partnership BD-500-1A10, BD-500-1A11, A330-201 and 45 more. Effective Nov 19, 2020
- [AD 2019-23-08](https://openairdocs.org/ad/2019-23-08): Fuel · Saab AB, Saab Aeronautics SAAB 2000. Effective Jan 7, 2020
- [AD 2019-21-04](https://openairdocs.org/ad/2019-21-04): Nacelles/ pylons · Saab AB, Saab Aeronautics SAAB 2000. Effective Dec 11, 2019
- [AD 2019-19-04](https://openairdocs.org/ad/2019-19-04): Fuel · Saab AB, Saab Aeronautics SAAB 2000. Effective Oct 31, 2019
- [AD 2019-10-02](https://openairdocs.org/ad/2019-10-02): Auto flight · Saab AB, Saab Aeronautics SAAB 2000. Effective Aug 15, 2019
- [AD 2018-25-10](https://openairdocs.org/ad/2018-25-10): Flight controls · Saab AB, Saab Aeronautics SAAB 2000. Effective Jan 14, 2019
- [AD 2016-25-17](https://openairdocs.org/ad/2016-25-17): Water/waste · Saab AB, Saab Aeronautics SAAB 2000. Effective Jan 25, 2017
- [AD 2016-20-05](https://openairdocs.org/ad/2016-20-05): Nacelles/pylons · Saab AB, Saab Aeronautics SAAB 2000. Effective Oct 13, 2016
- [AD 2016-17-14](https://openairdocs.org/ad/2016-17-14): Standard Practices/Structures · Saab AB, Saab Aeronautics SAAB 2000. Effective Oct 13, 2016
- [AD 2016-12-05](https://openairdocs.org/ad/2016-12-05): Water/Waste · Saab AB, Saab Aeronautics SAAB 2000. Effective Jul 20, 2016
- [AD 2014-18-01](https://openairdocs.org/ad/2014-18-01): Navigation · Bombardier ATR42-200, ATR42-300, ATR42-320 and 23 more. Effective Oct 14, 2014
- [AD 2012-26-01](https://openairdocs.org/ad/2012-26-01): Fuselage · Saab AB, Saab Aerosystems SAAB 2000. Effective Feb 13, 2013
- [AD 2012-10-06](https://openairdocs.org/ad/2012-10-06): Critical system wiring · Saab AB, Saab Aerosystems SAAB 2000. Effective Jun 25, 2012
- [AD 2012-09-03](https://openairdocs.org/ad/2012-09-03): Hydraulic Power · Saab AB, Saab Aerosystems SAAB 2000. Effective Jun 7, 2012
- [AD 2011-18-05](https://openairdocs.org/ad/2011-18-05): Fuselage · Saab AB, Saab Aerosystems SAAB 2000. Effective Sep 30, 2011
- [AD 2011-14-12](https://openairdocs.org/ad/2011-14-12): Landing gear · Saab AB, Saab Aerosystems SAAB 2000. Effective Aug 19, 2011
- [AD 2011-05-13](https://openairdocs.org/ad/2011-05-13): Stabilizers · Saab AB, Saab Aerosystems SAAB 2000. Effective Apr 14, 2011
- [AD 2009-22-07](https://openairdocs.org/ad/2009-22-07): Engine oil. · Saab AB, Saab Aerosystems SAAB 2000. Effective Dec 3, 2009
- [AD 2007-23-05 R1](https://openairdocs.org/ad/2007-23-05-R1): Fuel · Saab AB, Saab Aerosystems SAAB 2000. Effective Oct 30, 2009
- [AD 2008-23-02](https://openairdocs.org/ad/2008-23-02): Aft engine mounting · Saab AB, Saab Aerosystems SAAB 2000. Effective Dec 22, 2008
- [AD 2008-22-07](https://openairdocs.org/ad/2008-22-07): Fuel tank system · Saab AB, Saab Aerosystems SAAB 2000. Effective Dec 5, 2008
- [AD 2008-03-08](https://openairdocs.org/ad/2008-03-08): Fuel tank system · Saab AB, Saab Aerosystems SAAB 2000. Effective Mar 11, 2008
- [AD 2007-20-06](https://openairdocs.org/ad/2007-20-06): Control surface balancing procedure · Saab AB, Saab Aerosystems SAAB 2000. Effective Nov 7, 2007
- [AD 2005-23-04](https://openairdocs.org/ad/2005-23-04): Manual feather-and-unfeather system · Saab AB, Saab Aerosystems SAAB 2000. Effective Dec 19, 2005
- [AD 2005-23-11](https://openairdocs.org/ad/2005-23-11): Compressor impeller assemblies · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 5 more. Effective Dec 14, 2005
- [AD 2005-17-10](https://openairdocs.org/ad/2005-17-10): Front and rear spars · Saab AB, Saab Aerosystems SAAB 2000. Effective Sep 27, 2005
- [AD 2005-07-26](https://openairdocs.org/ad/2005-07-26): Electrical power generator · Saab AB, Saab Aerosystems SAAB 2000. Effective May 16, 2005
- [AD 2004-25-20](https://openairdocs.org/ad/2004-25-20): Drag and shear angles · Saab AB, Saab Aerosystems SAAB 2000. Effective Jan 24, 2005
- [AD 2004-14-11](https://openairdocs.org/ad/2004-14-11): Backup struts in the left and right nacelles · Saab AB, Saab Aerosystems SAAB 2000. Effective Aug 13, 2004
- [AD 2004-09-25](https://openairdocs.org/ad/2004-09-25): Roll and pitch disconnect handles · Saab AB, Saab Aerosystems SAAB 2000. Effective Jun 15, 2004
- [AD 2004-09-21](https://openairdocs.org/ad/2004-09-21): Windshield Wiper Assembly · Saab AB, Saab Aerosystems SAAB 2000. Effective Jun 15, 2004
- [AD 2004-06-14](https://openairdocs.org/ad/2004-06-14): Intermediate strut · Saab AB, Saab Aerosystems SAAB 2000. Effective Apr 30, 2004
- [AD 2004-04-02](https://openairdocs.org/ad/2004-04-02): Dual shuttle valve · Saab AB, Saab Aerosystems SAAB 2000. Effective Mar 24, 2004
- [AD 2003-20-04](https://openairdocs.org/ad/2003-20-04): Electrical wire harnesses · Saab AB, Saab Aerosystems SAAB 2000. Effective Nov 7, 2003
- [AD 2002-26-19](https://openairdocs.org/ad/2002-26-19): Main Pitot Static Tube · Saab AB, Saab Aerosystems SAAB 2000, SAAB 340B and 340A (SAAB SF340A). Effective Feb 10, 2003
- [AD 2001-13-10](https://openairdocs.org/ad/2001-13-10): Emergency Pitch Trim System · Saab AB, Saab Aerosystems SAAB 2000. Effective Aug 1, 2001
- [AD 2001-07-06](https://openairdocs.org/ad/2001-07-06): Rear Spar · Saab AB, Saab Aerosystems SAAB 2000. Effective May 15, 2001
- [AD 2000-23-24](https://openairdocs.org/ad/2000-23-24): Self-Seal Couplings · Saab AB, Saab Aerosystems SAAB 2000. Effective Jan 2, 2001
- [AD 2000-16-09](https://openairdocs.org/ad/2000-16-09): Fluorescent Lamps and Lampholders · Saab AB, Saab Aerosystems SAAB 2000 and SAAB 340B. Effective Sep 20, 2000
- [AD 2000-01-04](https://openairdocs.org/ad/2000-01-04): Aft Exterior Light · Saab AB, Saab Aerosystems SAAB 2000. Effective Feb 16, 2000
- [AD 2000-01-03](https://openairdocs.org/ad/2000-01-03): Retract Actuator of the Main Landing Gear · Saab AB, Saab Aerosystems SAAB 2000. Effective Feb 16, 2000
- [AD 99-24-17](https://openairdocs.org/ad/99-24-17): Lower Spar Cap Of Wing Front And Rear Spar · Saab AB, Saab Aerosystems SAAB 2000. Effective Jan 4, 2000
- [AD 99-19-14](https://openairdocs.org/ad/99-19-14): AFM - Limitations Section - Ice Protection System · Saab AB, Saab Aerosystems SAAB 2000, SAAB 340B and 340A (SAAB SF340A). Effective Dec 27, 1999

### Matched by engine (Rolls-Royce 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 2021-26-05](https://openairdocs.org/ad/2021-26-05) (historical): Time Limits/Maintenance Checks · Saab AB Support and Services SAAB 2000. Effective Feb 15, 2022
- [AD 2020-07-17](https://openairdocs.org/ad/2020-07-17) (historical): Time Limits/Maintenance Checks · Saab AB, Saab Aeronautics SAAB 2000. Effective May 26, 2020
- [AD 2019-03-19](https://openairdocs.org/ad/2019-03-19) (historical): Fuel · Saab AB, Saab Aeronautics SAAB 2000. Effective Apr 2, 2019
- [AD 2018-11-07](https://openairdocs.org/ad/2018-11-07) (historical): Flight controls · Saab AB, Saab Aeronautics SAAB 2000. Effective Jun 13, 2018
- [AD 2014-15-04](https://openairdocs.org/ad/2014-15-04) (historical): Water/Waste · Saab AB, Saab Aerosystems SAAB 2000. Effective Sep 9, 2014
- [AD 2007-23-05](https://openairdocs.org/ad/2007-23-05) (historical): Fuel tank system · Saab AB, Saab Aerosystems SAAB 2000. Effective Dec 11, 2007
- [AD 2000-13-09](https://openairdocs.org/ad/2000-13-09) (historical): Backup Struts in the Left and Right Nacelles · Saab AB, Saab Aerosystems SAAB 2000. Effective Aug 11, 2000
- [AD 97-13-06](https://openairdocs.org/ad/97-13-06) (historical): Inspect Fluorescent Lamps And Lampholders · Saab AB, Saab Aerosystems SAAB 2000 and SAAB 340B. Effective Jul 7, 1997

All 91: https://openairdocs.org/aircraft/N749SA/ads.md

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

- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008

## NTSB investigations

None matched to N749SA.

## FAA accident and incident reports

None matched to N749SA.

## Service difficulty reports (36)

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 4VAA202605270028](https://openairdocs.org/sdr/4VAA202605270028), May 27, 2026: SKIN. CORRODED. DURING INSPECTION, THE LEFT NACELLE INSIDE SKIN WAS FOUND CHAFED AND CORRODED. THE SKIN WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060709.
- [SDR 4VAA202605260040](https://openairdocs.org/sdr/4VAA202605260040), May 26, 2026: DOOR FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OVERWING EMERGENCY EXIT BOTTOM FRAME. THE FRAME WAS REPLACED IN ACCORDANCE WITH SRM 51-40-21/22.
- [SDR 4VAA202605140033](https://openairdocs.org/sdr/4VAA202605140033), May 26, 2026: RIB. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT WING TRAILING EDGE SUPPORT RIB. THE SUPPORT RIB WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060641.
- [SDR 4VAA202605260032](https://openairdocs.org/sdr/4VAA202605260032), May 26, 2026: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD FLOOR SUPPORT FRAME. THE FRAME WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060702.
- [SDR 4VAA202605210024](https://openairdocs.org/sdr/4VAA202605210024), May 21, 2026: BRACKET. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT NACELLE FIRE FLOOR AFT BRACKET. THE BRACKET WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060709.
- [SDR 4VAA202605210022](https://openairdocs.org/sdr/4VAA202605210022), May 21, 2026: DOOR FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FRAME AFT OF THE CARGO DOOR. THE FRAME WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060682.
- [SDR 4VAA202605210010](https://openairdocs.org/sdr/4VAA202605210010), May 21, 2026: BRACKET. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE HYDRAULIC PIPE BRACKET. IT WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060669.
- [SDR 4VAA202605190019](https://openairdocs.org/sdr/4VAA202605190019), May 19, 2026: FRAME. CHAFED. DURING INSPECTION, CHAFE DAMAGE WAS FOUND AT THE FORWARD CARGO DOOR RAIL FRAME. THE FORWARD CARGO DOOR RAIL FRAME WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT
- [SDR 4VAA202605190014](https://openairdocs.org/sdr/4VAA202605190014), May 19, 2026: SKIN. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON RIGHT WING TRAILING EDGE TOP SKIN OUTBOARD OF NACELLE. IT WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060668
- [SDR 4VAA202605180020](https://openairdocs.org/sdr/4VAA202605180020), May 18, 2026: ACCESS PANEL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT THE RIGHT HAND FUEL ACCESS PANEL (624ET) APERTURE FRAME. THE CORROSION WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 
- [SDR 4VAA202605180016](https://openairdocs.org/sdr/4VAA202605180016), May 18, 2026: LUG. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT HAND FLAP LUGS TO HINGE FITTING AND THE RIGHT HAND FLAP HINGE FAIRING BRACKETS. THE FLAP WAS REPLACED.
- [SDR 4VAA202605150039](https://openairdocs.org/sdr/4VAA202605150039), May 15, 2026: BRACKET. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE BRACKET AFT OF ENTRANCE DOOR LEFT WALL. THE BRACKET WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060712.
- [SDR 4VAA202605150038Q](https://openairdocs.org/sdr/4VAA202605150038Q), May 15, 2026: BRACKET. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WING REAR SPAR HYDRAULIC LINE CLAMP BRACKET. THE BRACKET WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000
- [SDR 4VAA202605150037](https://openairdocs.org/sdr/4VAA202605150037), May 15, 2026: BRACKET. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WING REAR SPAR HYDRAULIC LINE CLAMP BRACKET. THE BRACKET WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000
- [SDR 4VAA202605150036](https://openairdocs.org/sdr/4VAA202605150036), May 15, 2026: ANCHOR FITTING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT 5EA C1 CARGO FLOOR NET ANCHOR PLATES. THE ANCHOR PLATES WERE REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060712.
- [SDR 4VAA202605150030](https://openairdocs.org/sdr/4VAA202605150030), May 15, 2026: FLOORBEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE FLOOR BEAM FRAME IN SERVICE (AFT) DOOR AREA. THE FRAME WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS06070
- [SDR 4VAA202605150029](https://openairdocs.org/sdr/4VAA202605150029), May 15, 2026: FLOORBEAM. CRACKED. DURING INSPECTION, CORROSION AND A CRACK WAS FOUND ON THE FLOOR BEAM FORWARD ENTRANCE AREA. THE BEAM WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS06070
- [SDR 4VAA202605150011](https://openairdocs.org/sdr/4VAA202605150011), May 15, 2026: FLOORBEAM. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE FLOORBEAM AT THE ENTRANCE. THE BEAM WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060702.
- [SDR 4VAA202605140027](https://openairdocs.org/sdr/4VAA202605140027), May 14, 2026: SKIN. CORRODED. DURING INSPECTION, CORROSION AND CHAFING WAS FOUND ON THE RIGHT NACELLE INSIDE SKIN. THE SKIN WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060709.
- [SDR 4VAA202605140008](https://openairdocs.org/sdr/4VAA202605140008), May 14, 2026: SPLICE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT HORIZONTAL STAB UPPER FINGER SPLICE AT Y1595B-1500. IT WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SD
- [SDR 4VAA202605130035](https://openairdocs.org/sdr/4VAA202605130035), May 13, 2026: ANGLE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE PRESSURE BULKHEAD AFT ANGLE. THE ANGLE WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060703.
- [SDR 4VAA202605130026](https://openairdocs.org/sdr/4VAA202605130026), May 13, 2026: SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT HAND NACELLE FIRE FLOOR SUPPORT. THE SUPPORT WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060641.
- [SDR 4VAA202605130025](https://openairdocs.org/sdr/4VAA202605130025), May 13, 2026: ANGLE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT HAND NACELLE FIRE FLOOR ANGLE. THE ANGLE WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060704.
- [SDR 4VAA202605130023](https://openairdocs.org/sdr/4VAA202605130023), May 13, 2026: WEB. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE WEB ABOVE THE CARGO DOOR. THE CORROSION WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060682.
- [SDR 4VAA202605120017](https://openairdocs.org/sdr/4VAA202605120017), May 12, 2026: SPAR. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT ELEVATOR FORWARD SPAR AND RIBS, AND THE EMER PITCH TRIM ACTUATOR BRACKET. THE CORROSION WAS REPAIRED IN ACCO
- [SDR 4VAA202605130015](https://openairdocs.org/sdr/4VAA202605130015), May 12, 2026: MOUNT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RUDDER FRONT SPAR LEFT HAND AND RIGHT HAND LEADING EDGE PANEL MOUNT SCREW HOLES. IT WAS REPAIRED IN ACCORDANCE WIT
- [SDR 4VAA202605120013](https://openairdocs.org/sdr/4VAA202605120013), May 12, 2026: BRACKET. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT AIR CYCLE MACHINE BRACKET. THE BRACKET WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060669.
- [SDR 4VAA202605120012`](https://openairdocs.org/sdr/4VAA202605120012%60), May 12, 2026: BRACKET. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT HAND AIR CYCLE MACHINE BRACKET. THE BRACKET WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060669.
- [SDR 4VAA202605120009](https://openairdocs.org/sdr/4VAA202605120009), May 12, 2026: FRAME. CRACKED. DURING INSPECTION, A CRACK WAS FOUND AT LEFT LOWER FRAME FORWARD WING BOX. IT WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060707.
- [SDR 4VAA202605110031](https://openairdocs.org/sdr/4VAA202605110031), May 11, 2026: SKIN. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT ELEVATOR TOP AND LOWER LEADING EDGE. THE ELEVATOR WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS06067
- [SDR 4VAA202605110021](https://openairdocs.org/sdr/4VAA202605110021), May 11, 2026: SPAR CAP. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT THE RIGHT HAND WING TRAILING EDGE TOP SPAR CAP AT HINGE NUMBER 3. THE RIGHT HAND WING TRAILING EDGE SPAR CAP WAS REPAI
- [SDR 4VAA202605090018](https://openairdocs.org/sdr/4VAA202605090018), May 9, 2026: FAIRING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT WING SKIN DOUBLER AILERON ACTUATOR FAIRING. THE LEFT HAND WING SKIN DOUBLER AILERON ACTUATOR FAIRING WAS REPA
- [SDR 4VAA202605070007](https://openairdocs.org/sdr/4VAA202605070007), May 7, 2026: SPAR. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LH FLAP LOWER FRONT SPAR IN TWO PLACES. THE LT FLAP LOWER FRONT SPAR WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMEN
- [SDR 4VAA202605040041](https://openairdocs.org/sdr/4VAA202605040041), May 4, 2026: ANGLE. CORRODED. DURING INSPECTION, CORROSION AND A CRACK WAS FOUND ON THE NOSE LANDING GEAR WHEEL WELL ANGLE AT THE LEFT FORWARD CORNER. THE ANGLE WAS REPLACED IN ACCORDANCE WI
- [SDR 4VAA202604290034](https://openairdocs.org/sdr/4VAA202604290034), Apr 29, 2026: SKIN. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WING LEADING EDGE PNL 612BR UPPER AND LOWER SURFACE AT THE FASTENER HOLES. THE PANEL WAS REPAIRED IN ACCORDA
- [SDR 4VAA202601290002](https://openairdocs.org/sdr/4VAA202601290002), Jan 29, 2026: BATTERY PACK. INOPERATIVE. DURING INSPECTION, THE EMERGENCY LIGHT BATTERY PACK 11LN FAILED A FUNCTIONAL CHECK. THE BATTERY PACK WAS REPLACED IN ACCORDANCE WITH THE SAAB AMM.

## STCs that may be installed (OpenAirDocs) (23)

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 SAAB 2000)

- [STC ST12467CH](https://openairdocs.org/stc/ST12467CH): Installation of Seat Blocker Interior Reconfiguration. STS Engineering Solutions, LLC
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST00807DE](https://openairdocs.org/stc/ST00807DE): Installation of a Panasonic Flight Link System. FLYHT Inc
- [STC ST02586AK](https://openairdocs.org/stc/ST02586AK): Approval of the Thomas Global Systems TFD-4000/4100 Active Matrix Liquid Crystal Display. ADS-B Technologies
- [STC ST01833WI](https://openairdocs.org/stc/ST01833WI): Modification of a Rockwell Collins Global Positioning System (GPS) installation. Rockwell Collins Inc
- [STC ST00144IB](https://openairdocs.org/stc/ST00144IB): Installation of LPV Approach and ADS-B Out capability. TABY AIR MAINTENANCE AB
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04471NY](https://openairdocs.org/stc/ST04471NY): Installation of Standalone ADS-B (Out). Cranfield Aerospace Solutions Ltd
- [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST01836WI](https://openairdocs.org/stc/ST01836WI): Installation of a Reinforced Flightdeck Door. Worldwide Aviation Engineering LLC
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST01431WI-D](https://openairdocs.org/stc/ST01431WI-D): Modification of a Rockwell Collins, Inc. Data Base Unit (DBU) installation. Rockwell Collins Inc
- [STC ST01474WI-D](https://openairdocs.org/stc/ST01474WI-D): Modication of a Rockwell Collins Weather Radar System installation. Rockwell Collins Inc
- [STC ST01433WI-D](https://openairdocs.org/stc/ST01433WI-D): Modification of a Collins GPS-4000 or GPS-4000A. Rockwell Collins Inc
- [STC ST02540AT-D](https://openairdocs.org/stc/ST02540AT-D): Installation of replacement fuel tank sealant system. FFC Manufacturing
- [STC ST00844WI-D](https://openairdocs.org/stc/ST00844WI-D): Modification of Collins TCAS II or TCAS-94 (TCAS II) system installation with Collins TTR-920 Change 7.0 Receiver Transmitter to a Collins TCAS II or TCAS-94 OTCAS II) system installation with Collins TTR-921 or Collins TTR-4000 Change 7.0 TCAS Receiver Transmitter. Rockwell Collins Inc
- [STC ST10433SC](https://openairdocs.org/stc/ST10433SC): Reconfigure aircraft interior from a 36 seat configuration to a 45 seat configuration. Rose Aircraft Interiors, Inc
- [STC SA2983SO](https://openairdocs.org/stc/SA2983SO): Installation of coffee maker/water boiler, P/N 3510-0044-(), and rail assembly, P/N 416-0201-(). B/E Aerospace Inc
- [STC ST408CH](https://openairdocs.org/stc/ST408CH): Installation of Radome. Norton Company

## Earlier aircraft with N749SA

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N749SA before.

- [Cancelled 2012-07-13](https://openairdocs.org/deregistered/N749SA-2012-07-13): Boeing 747-300 SERIES, S/N 24194, built 1988. First renewal notice. Owner: [Southern Air Inc](https://openairdocs.org/faa-owner/SOUTHERN%20AIR%20INC), [Norwalk, CT](https://openairdocs.org/faa-place/CT/Norwalk)

## Related

- Other Saab SAAB 2000 aircraft: https://openairdocs.org/model/saab-saab-2000/aircraft.md
- The Rolls-Royce AE-2100A engine: https://openairdocs.org/engine/rolls-royce-ae-2100a.md

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