# N959AT: 2001 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [BMW Rolls BR-700 series](https://openairdocs.org/engine/bmw-rolls-br-700-series) (registry code 09500)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55021
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Experimental, operating kit built
- Airworthiness date: February 16, 2026
- Certificate issued: December 18, 2023
- Expires: December 31, 2030
- Mode S code: AD5628
- Registered owner: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC)
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Corporation
- Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, 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=959AT
- Page: https://openairdocs.org/aircraft/N959AT

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. The registry lists only the engine series, so ADs for every BMW Rolls BR-700 model are included.

## ADs that may apply (OpenAirDocs): 78 in force

### Matched by airframe (Boeing 717-200)

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [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 2025-21-05](https://openairdocs.org/ad/2025-21-05): Landing Gear · Boeing 717-200. Effective Jan 2, 2026
- [AD 2025-02-07](https://openairdocs.org/ad/2025-02-07): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Mar 17, 2025
- [AD 2024-21-01](https://openairdocs.org/ad/2024-21-01): Wings · Boeing 717-200. Effective Nov 7, 2024
- [AD 2024-20-02](https://openairdocs.org/ad/2024-20-02): Fuselage · Boeing 717-200, DC-9-11, DC-9-12 and 16 more. Effective Oct 21, 2024
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 2023
- [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 2021-12-12](https://openairdocs.org/ad/2021-12-12): Wings · Boeing 717-200. Effective Jul 29, 2021
- [AD 2021-02-16](https://openairdocs.org/ad/2021-02-16): Ice and rain protection · Boeing 717-200. Effective Mar 30, 2021
- [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018
- [AD 2018-10-08](https://openairdocs.org/ad/2018-10-08): Stabilizers · Boeing 717-200. Effective May 31, 2018
- [AD 2018-03-04](https://openairdocs.org/ad/2018-03-04): Airspeed/Mach Indicator · Boeing 717-200, DC-9-11, DC-9-12 and 23 more. Effective Mar 16, 2018
- [AD 2017-09-09](https://openairdocs.org/ad/2017-09-09): Passenger Compartment Equipment · Boeing 717-200, MD-90-30, CL-600-2C10 (Regional Jet Series 700) and 17 more. Effective Jun 28, 2017
- [AD 2017-01-03](https://openairdocs.org/ad/2017-01-03): Standard practices/structures · Boeing 717-200. Effective Mar 14, 2017
- [AD 2015-02-05](https://openairdocs.org/ad/2015-02-05): Navigation · Boeing 717-200, DC-10-10, DC-10-10F and 13 more. Effective Mar 5, 2015
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2014-05-22](https://openairdocs.org/ad/2014-05-22): Fuselage · Boeing 717-200. Effective Apr 15, 2014
- [AD 2013-19-22](https://openairdocs.org/ad/2013-19-22): JASC Code 53, Fuselage · Boeing 717-200. Effective Nov 6, 2013
- [AD 2012-12-09](https://openairdocs.org/ad/2012-12-09): Horizontal Stabilizer Structure · Boeing 717-200. Effective Jul 23, 2012
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2009-07-07](https://openairdocs.org/ad/2009-07-07): Main landing gear (MLG) · Boeing 717-200. Effective May 5, 2009
- [AD 2008-18-05](https://openairdocs.org/ad/2008-18-05): Elevator standby cable system · Boeing 717-200. Effective Oct 14, 2008
- [AD 2008-11-15](https://openairdocs.org/ad/2008-11-15): Fuel tank systems · Boeing 717-200, DC-9-11, DC-9-12 and 21 more. Effective Jul 3, 2008
- [AD 2008-11-06](https://openairdocs.org/ad/2008-11-06): Gray water drain hose · Boeing 717-200. Effective Jul 3, 2008
- [AD 2008-02-12](https://openairdocs.org/ad/2008-02-12): Center fuel tank · Boeing 717-200. Effective Feb 28, 2008
- [AD 2008-02-08](https://openairdocs.org/ad/2008-02-08): Main fuel tanks · Boeing 717-200. Effective Feb 26, 2008
- [AD 2007-19-15](https://openairdocs.org/ad/2007-19-15): Flight management system (FMS) · Boeing 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Oct 26, 2007
- [AD 2007-19-03](https://openairdocs.org/ad/2007-19-03): Power conversion distribution unit (PCDU) · Boeing 717-200. Effective Oct 17, 2007
- [AD 2007-17-11](https://openairdocs.org/ad/2007-17-11): In-line fuel float switch fuses · Boeing 717-200. Effective Oct 2, 2007
- [AD 2007-13-09](https://openairdocs.org/ad/2007-13-09): Fuel boost pump container · Boeing 717-200. Effective Aug 3, 2007
- [AD 2007-13-01](https://openairdocs.org/ad/2007-13-01): Wiring of the first officer's pitot static heater system · Boeing 717-200. Effective Jul 25, 2007
- [AD 2007-05-06](https://openairdocs.org/ad/2007-05-06): Bulkhead nipple assemblies of the left and right wing vent boxes · Boeing 717-200. Effective Apr 9, 2007
- [AD 2006-20-12](https://openairdocs.org/ad/2006-20-12): Replaces clamp bases on fuel tank vent systems. · Boeing 717-200. Effective Nov 8, 2006
- [AD 2006-10-14](https://openairdocs.org/ad/2006-10-14): Stop pad support fittings · Boeing 717-200, DC-9-11, DC-9-12 and 22 more. Effective Jun 21, 2006
- [AD 2005-16-08](https://openairdocs.org/ad/2005-16-08): Oxygen release system in the forward cabin · Boeing 717-200. Effective Sep 13, 2005
- [AD 2005-11-03](https://openairdocs.org/ad/2005-11-03): Brake fuses. · Boeing 717-200. Effective Jul 1, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-08-02](https://openairdocs.org/ad/2004-08-02): Left and right hand horizontal stabilizer hinge fitting bolts · Boeing 717-200. Effective May 19, 2004
- [AD 2004-03-21](https://openairdocs.org/ad/2004-03-21): Inboard Ends of Outer Skin Panels of Horizontal Stabilizer at Station Xh=7.234 · Boeing 717-200. Effective Mar 17, 2004
- [AD 2004-01-15](https://openairdocs.org/ad/2004-01-15): Auxiliary hydraulic pump · Boeing 717-200. Effective Feb 17, 2004
- [AD 2003-14-05](https://openairdocs.org/ad/2003-14-05): Main spoiler actuators · Boeing 717-200. Effective Jul 31, 2003
- [AD 2003-10-10](https://openairdocs.org/ad/2003-10-10): Rear spar · Boeing 717-200. Effective Jul 1, 2003
- [AD 2003-10-08](https://openairdocs.org/ad/2003-10-08): Upper center fuselage · Boeing 717-200. Effective Jul 1, 2003
- [AD 2003-04-24](https://openairdocs.org/ad/2003-04-24): Support Fitting Assemblies and Stop Pads of Main Spoiler Actuators · Boeing 717-200. Effective Mar 17, 2003
- [AD 2002-21-01](https://openairdocs.org/ad/2002-21-01): Electrical terminal contact pins · Airbus A319-111, A319-112, A319-113 and 66 more. Effective Nov 27, 2002
- [AD 2002-16-09](https://openairdocs.org/ad/2002-16-09): Solenoid operated shut-off valve (SOV) · Boeing 717-200. Effective Sep 3, 2002
- [AD 2002-14-16](https://openairdocs.org/ad/2002-14-16): Spoiler Hold-Down Actuator Supports on Left and Right Wing Rear Spar · Boeing 717-200. Effective Aug 16, 2002
- [AD 2001-18-11](https://openairdocs.org/ad/2001-18-11): Rudder Trim · Boeing 717-200. Effective Oct 1, 2001

### Matched by engine (BMW Rolls BR-700 series)

- [AD 2026-21-04](https://openairdocs.org/ad/2026-21-04): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Nov 23, 2026
- [AD 2025-06-03](https://openairdocs.org/ad/2025-06-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 23, 2025
- [AD 2023-17-11](https://openairdocs.org/ad/2023-17-11): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Sep 20, 2023
- [AD 2022-26-02](https://openairdocs.org/ad/2022-26-02): Accessory Gearboxes · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20, BR700-710C4-11 and 1 more. Effective Jan 27, 2023
- [AD 2021-21-12](https://openairdocs.org/ad/2021-21-12): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A2-20. Effective Dec 13, 2021
- [AD 2021-14-03](https://openairdocs.org/ad/2021-14-03): Turbine Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 19, 2021
- [AD 2021-12-07](https://openairdocs.org/ad/2021-12-07): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 12, 2021
- [AD 2018-18-14](https://openairdocs.org/ad/2018-18-14): Engine Controls · Rolls-Royce Deutschland BR700-710A2-20 and BR700-710C4-11. Effective Oct 12, 2018
- [AD 2016-13-12](https://openairdocs.org/ad/2016-13-12): Pawl carrier pivot pins · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 5, 2016
- [AD 2014-12-03](https://openairdocs.org/ad/2014-12-03): Fuel metering units (FMUs) · Rolls-Royce Deutschland BR700-725A1-12. Effective Jul 17, 2014
- [AD 2014-08-05](https://openairdocs.org/ad/2014-08-05): Low-pressure compressor (LPC) case ice impact panels · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 23, 2014
- [AD 2014-07-02](https://openairdocs.org/ad/2014-07-02): High-pressure (HP) compressor stages 1 to 6 rotor disc assemblies · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 8, 2014
- [AD 2013-12-03](https://openairdocs.org/ad/2013-12-03): Fuel pump tube · Rolls-Royce Deutschland BR700-725A1-12. Effective Jun 14, 2013
- [AD 2013-03-17](https://openairdocs.org/ad/2013-03-17): High-pressure turbine (HPT) stage 1 and stage 2 discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Mar 21, 2013
- [AD 2012-14-01](https://openairdocs.org/ad/2012-14-01): LP compressor booster rotor · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Oct 19, 2012
- [AD 2009-07-01 R1](https://openairdocs.org/ad/2009-07-01-R1): High-pressure (HP) turbine stage 1 discs, and HP turbine stage 2 discs · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 6, 2012
- [AD 2011-22-01](https://openairdocs.org/ad/2011-22-01): Touch-and-go and overshoot on life cycle counting · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Nov 23, 2011
- [AD 2010-25-05](https://openairdocs.org/ad/2010-25-05): Turbine Discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 13, 2011
- [AD 2009-21-04](https://openairdocs.org/ad/2009-21-04): Engine Failure · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Dec 3, 2009
- [AD 2009-04-13](https://openairdocs.org/ad/2009-04-13): Low pressure (LP) compressor (fan) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Mar 26, 2009
- [AD 2005-21-05](https://openairdocs.org/ad/2005-21-05): Fan discs and fan blades · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Nov 25, 2005
- [AD 2005-16-12](https://openairdocs.org/ad/2005-16-12): Independent Overspeed Protection (IOP) unit. · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 26, 2005
- [AD 2000-25-51](https://openairdocs.org/ad/2000-25-51): High Pressure Turbine Disks · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Feb 20, 2001
- [AD 2001-01-01](https://openairdocs.org/ad/2001-01-01): Oil Filter · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Jan 31, 2001
- [AD 98-24-03 R1](https://openairdocs.org/ad/98-24-03-R1): Combustion Core Fairings · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Dec 27, 1999

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

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2020-03-20](https://openairdocs.org/ad/2020-03-20) (historical): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Feb 18, 2020
- [AD 2016-09-05](https://openairdocs.org/ad/2016-09-05) (historical): Stabilizers · Boeing 717-200. Effective Jun 8, 2016
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2007-11-13](https://openairdocs.org/ad/2007-11-13) (historical): Principal structural elements (PSEs) · Boeing 717-200. Effective Jun 29, 2007
- [AD 2004-18-04](https://openairdocs.org/ad/2004-18-04) (historical): Airplane Flight Manual (AFM) · McDonnell Douglas 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Sep 20, 2004
- [AD 2003-17-01](https://openairdocs.org/ad/2003-17-01) (historical): Flap system · McDonnell Douglas 717-200. Effective Sep 23, 2003
- [AD 2000-03-51](https://openairdocs.org/ad/2000-03-51) (historical): Jackscrew Assembly · McDonnell Douglas 717-200, DC-9 Series (all), MD-88 and 1 more. Effective Mar 6, 2000
- [AD 2022-24-06](https://openairdocs.org/ad/2022-24-06) (historical): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 6, 2023
- [AD 2013-05-13](https://openairdocs.org/ad/2013-05-13) (historical): Fuel pump splined couplings · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 24, 2013
- [AD 2012-26-14](https://openairdocs.org/ad/2012-26-14) (historical): High-pressure (HP) compressor stages 1 to 6 rotor disc assembly · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Jan 10, 2013
- [AD 2009-07-01](https://openairdocs.org/ad/2009-07-01) (historical): High Pressure (HP) Turbine · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Apr 27, 2009
- [AD 2003-07-11](https://openairdocs.org/ad/2003-07-11) (historical): Fan discs · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Apr 28, 2003
- [AD 2001-05-06](https://openairdocs.org/ad/2001-05-06) (historical): Fan Disk · BMW Rolls-Royce BR700-710A1-10 and BR700-710A2-20. Effective Mar 29, 2001

All 92: https://openairdocs.org/aircraft/N959AT/ads.md

## Information bulletins (advisory) (4 in force)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-18-33](https://openairdocs.org/saib/NM-18-33): Engine Fuel and Control. Issued Dec 17, 2018
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006

## NTSB investigations

None matched to N959AT.

## FAA accident and incident reports

None matched to N959AT.

## Reports on N959AT not matched to an aircraft (1)

They name N959AT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19800105013409I](https://openairdocs.org/incident/19800105013409I), Jan 5, 1980: Lear 35LEAR (N959AT), Las Vegas, NV, Minor damage. On takeoff roll, left tire blew and during aborted takeoff other left tire blew. Wheels and gear door damage.

## Service difficulty reports (213, newest 50)

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 DALA2026080604548](https://openairdocs.org/sdr/DALA2026080604548), Aug 5, 2026: LANYARD. BROKEN. L1 DOOR SLIDE BUSTLE TO GIRT BAR LANYARD BROKEN, REPLACED L1 DOOR SLIDE LANYARD IAW AMM 25-61. (8497882) (AIRCRAFT GROUNDED).
- [SDR DALA2026062103689](https://openairdocs.org/sdr/DALA2026062103689), Jun 20, 2026: LIGHT. DETACHED. EMERGENCY FLOOR LIGHT STRIP EXTENDING FROM ROW 14-17 ON THE RIGHT SIDE CAME OFF. SECURED EMERGENCY FLOOR LIGHT STRIP. OK FOR SVC. (LP 8878887 - AIRCRAFT WAS GRO
- [SDR DALA2026051102945](https://openairdocs.org/sdr/DALA2026051102945), May 6, 2026: NONE. NONE. INSTALL ESA ANTENNA, REPAIRED REF B717 ERA 681787-14. (8673211) (AIRCRAFT GROUNDED)
- [SDR DALA2026031901912](https://openairdocs.org/sdr/DALA2026031901912), Mar 16, 2026: CARBON SEAL. LEAKING. AIRCRAFT 9518, STRONG DIRTY SOCK ODOR COMING FROM PACK 2. FOUND APU TO BE LEAKING THROUGH CARBON SEAL PER B717 AMM 49-00. REPLACED APU. (LP 8237910)
- [SDR DALA2025091606818](https://openairdocs.org/sdr/DALA2025091606818), Sep 11, 2025: HINGE FITTING. CORRODED. RT ELEVATOR GEARED TAB INBD CRANK FITTING-HINGE HAS SIGNS OF CORROSION ON HARDWARE AND PUSH ROD END HAS SIDE TO SIDE PLAY. REPLACED HARDWARE REF B717 AMM 27-31-
- [SDR DALA2025060704357](https://openairdocs.org/sdr/DALA2025060704357), Jun 2, 2025: LIGHT. DETACHED. AIRCRAFT 9518, EMERGENCY EXIT LIGHT HANGING DOWN ROW 19. CORRECTIVE ACTION: SECURED LIGHT ASSY REF B717 AMM 33-51. (LP 7263518)
- [SDR DALA2025060604337](https://openairdocs.org/sdr/DALA2025060604337), May 29, 2025: REPAIR. NOT REPORTED. SHIP 9518 EXISTING REPAIR FOUND. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. CORRECTIVE ACTION: REPAIRED PER ER/A 14-621443 (0994
- [SDR DALA2025060604336](https://openairdocs.org/sdr/DALA2025060604336), May 29, 2025: REPAIR. NOT REPORTED. SHIP 9518 EXISTING REPAIRS FOUND. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. CORRECTIVE ACTION: REPAIRED PER ERA 621388-14AD (09
- [SDR DALA2025052203934](https://openairdocs.org/sdr/DALA2025052203934), May 16, 2025: NONE. NONE. SHIP 9518 ACCOMPLISH ERA 624994-14 KA1717 STRUCTURAL SHIMMING FOR HUGHES WIFI INSTALLATION, CORRECTIVE ACTION: COMPLIED WITH ERA 624994-14 REV. (0969673)
- [SDR DALA2025051403727](https://openairdocs.org/sdr/DALA2025051403727), May 9, 2025: SPAR CAP. CRACKED. DUE TO CRACK IN RH WING REAR AFT SPAR LOWER CAP, COMPLY WITH PRI 621388-14. CRACKED SPAR CAP REPLACED ON PRI 621388-14 REVS 0 THRU 22. COMPARED PRI 621388-14 RE
- [SDR DALA2025051203682](https://openairdocs.org/sdr/DALA2025051203682), May 9, 2025: BATTERY. NO TEST. DURING TESTING FOUND 1EA LIGHT IN CEILING AT AFT EXIT / FA SEAT AREA TO BE INOPERATIVE. REPLACED BATTERY AT B5-116. NOW LIGHT TEST GOOD REF B717 AMM 33-51-00. (
- [SDR DALA2025051403726](https://openairdocs.org/sdr/DALA2025051403726), May 8, 2025: SPAR CAP. CRACKED. DUE TO CRACK IN LH WING LOWER SPAR CAP, COMPLY WITH PRI 621443-14. CRACKED SPAR CAP REPLACED ON PRI 621443-14 REVS 0 THRU 24. COMPARED PRI 621443-14 REVS 0 THRU
- [SDR DALA2024040504130](https://openairdocs.org/sdr/DALA2024040504130), Apr 3, 2024: NUT. OUT OF LIMITS. AD -- DURING FUNCTIONAL TEST OF THE TRIM ACME SCREW AND NUT FOUND DIMENSION BG IS OUT OF LIMIT. UNSAFTIED TURNBUCKLE CONNECTING CABLES 130B TO 130A AND CABLE TU
- [SDR DALA2024040504131](https://openairdocs.org/sdr/DALA2024040504131), Apr 1, 2024: SUPPORT. CRACKED. AD -- DURING JACK SCREW LUBE, CYCLED HORIZ STAB FULL NOSE UP, SUPPORT ASSY CONTACTED STOP AND CRACKED. REMOVED HORIZONTAL STABILIZER ACTUATOR ASSEMBLY AND REPLA
- [SDR DALA2024020801685](https://openairdocs.org/sdr/DALA2024020801685), Feb 7, 2024: COVER. MISALIGNED. DURING SERVICE CHECK, THE CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE WITH C/B A11 PULLED. MAINTENANCE FOUND F/A PANEL SWITCH COVER MISALIGNED, CAUSING SWITCH T
- [SDR DALA2024020601581](https://openairdocs.org/sdr/DALA2024020601581), Feb 4, 2024: HOLDER. SHORTED. SHIP 9518 -SMKE- THE FLIGHT CREW REPORTED VISIBLE SMOKE FROM THE CAPTAIN SIDE CLIPBOARD LIGHT. THE SMOKE STOPPED AFTER ABOUT 10 SECONDS. THE QRH WAS COMPLIED WI
- [SDR DALA2024012601172](https://openairdocs.org/sdr/DALA2024012601172), Jan 24, 2024: LIGHT. SPARKS. AFTER TAKEOFF ON RWY 6 IN BHM, AT APPROX 600 FT, CAPTAIN SIDE MAP LIGHT SPARKED AND BEGAN TO SMOKE. THE CIRCUIT BREAKER W29 TRIPPED AND FLIGHT CONTINUED WITHOUT
- [SDR DALA2023100408162](https://openairdocs.org/sdr/DALA2023100408162), Sep 29, 2023: UNKNOWN. UNKNOWN. SHIP 9518 -DE- THE CREW DECLARED AN EMERGENCY DUE TO INTERMITTENT RIGHT HYDRAULIC PUMP FAIL MESSAGE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT ENGINE DR
- [SDR DALA2023081606668](https://openairdocs.org/sdr/DALA2023081606668), Aug 12, 2023: UNKNOWN. UNKNOWN. AD RELATED, MISSING TO PERFORM STEP 14 A (2) AND 22 A (2) OF 2521-01701-01B-TRIPLE TOURIST CLASS SEATS, B717 - MODIFY; SECTION 01. SUMMARY OF NRC 00520: STEP 14
- [SDR DALA2023081606667](https://openairdocs.org/sdr/DALA2023081606667), Aug 12, 2023: UNKNOWN. UNKNOWN. AD RELATED, MISSING TO PERFORM TORQUE OF TRIPLE TOURIST CLASS SEATS. SUMMARY OF NRC 00518: STEP 8J OF 2521-01701-01B-TRIPLE TOURIST CLASS SEATS, B717 - MODIFY; 
- [SDR DALA2023081606666](https://openairdocs.org/sdr/DALA2023081606666), Aug 12, 2023: UNKNOWN. UNKNOWN. AD RELATED, MISSING TO PERFORM STEP 14 A (2), 21 A (2) AND 34 A (2) OF 2521-01701-01A-SINGLE AND DOUBLE TOURIST CLASS SEATS, B717 - MODIFY; SECTION 01. SUMMARY 
- [SDR DALA2023080706365](https://openairdocs.org/sdr/DALA2023080706365), Aug 4, 2023: UNKNOWN. UNKNOWN. NICKS ON DOUBLER REPAIR BTW STA Y=996 TO Y=1002. SUMMARY OF NRC 099: 2ND. DOUBLER WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 10 FIGURE 202. PERFORM VIS
- [SDR DALA2023080706364](https://openairdocs.org/sdr/DALA2023080706364), Aug 4, 2023: UNKNOWN. UNKNOWN. CRACK ON WEB INSIDE STRUCTURE AFT EMERGENCY DOOR AT CABIN PAX. SUMMARY OF NRC 0170: WEB INSIDE STRUCTURE AFT EMERGENCY DOOR AT CABIN PAX WAS REPAIRED PER B-717-
- [SDR DALA2023080306278](https://openairdocs.org/sdr/DALA2023080306278), Aug 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON WEB ON X=-44 STA Y=160 AND X=54 BTW STA Y=160 AND STA Y=180 AT FWD PAX CABIN FLOOR. SUMMARY OF NRC 00179: CORROSION LEVEL 2. WEB ON X=-44 STA Y=160
- [SDR DALA2023080106211](https://openairdocs.org/sdr/DALA2023080106211), Jul 31, 2023: UNKNOWN. UNKNOWN. CORROSION ON GENERATION FLOOR ACCESS PANELS 221SF, 222EF, 221NF, 222AWF, AND 222SF. SUMMARY OF NRC 00283: CORROSION LEVEL 2. FLOOR ACCESS PANELS 222EF AND 222SF
- [SDR DALA2023080106210](https://openairdocs.org/sdr/DALA2023080106210), Jul 31, 2023: UNKNOWN. UNKNOWN. DISBOND ON RH CENTER FIXED VANE, UPPER SURFACE OF 0.700IN LENGTH X 0.600IN WIDTH AT DENT #1, (53.25" FROM IB EDGE, 5" FROM TE) IN REF MON JOB 032-0001 LOG 15493
- [SDR DALA2023080106201](https://openairdocs.org/sdr/DALA2023080106201), Jul 29, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR PANEL 211AMF AT COCKPIT. SUMMARY OF NRC 00299: CORROSION LEVEL 2. PANEL (SKIN) OF FLOOR PANEL 211AMF AT COCKPIT WAS FABRICATED AND REPLACED P
- [SDR DALA2023080106200](https://openairdocs.org/sdr/DALA2023080106200), Jul 28, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME BTW STA Y=1037 AND LONG 17LH AT AFT PAX CABIN. SUMMARY OF NRC 00289: FRAME BTW STA Y=1037 AND LONG 17LH AT AFT PAX CABIN WAS REPAIRED PER B717 SR
- [SDR DALA2023072806113](https://openairdocs.org/sdr/DALA2023072806113), Jul 28, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH CTR SEAT TRACK FROM STA Y=216 TO STA Y=245 AT FWD PAX CABIN FLOOR. SUMMARY OF NRC 0174: CORROSION LEVEL 2. SECTION SEAT TRACK FROM STA Y=200 TO 
- [SDR DALA2023072806110](https://openairdocs.org/sdr/DALA2023072806110), Jul 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON FITTINGS (2 EA) OF FWD SERVICE DOOR JAMB AT FWD PAX CABIN FLOOR. SUMMARY OF NRC 0180: CORROSION LEVEL 2. FITTINGS (2 EA) WERE REPLACED PER B717-200
- [SDR DALA2023072606037](https://openairdocs.org/sdr/DALA2023072606037), Jul 24, 2023: UNKNOWN. UNKNOWN. CORROSION ON LH CUSP MEMBRANE (WEB) STA 832 TO STA 870. SUMMARY OF NRC 0438: CORROSION LEVEL 2. CUSP MEMBRANE WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4
- [SDR DALA2023072505981](https://openairdocs.org/sdr/DALA2023072505981), Jul 23, 2023: UNKNOWN. UNKNOWN. CRACKED FRAME CLIP STA Y=715 LH SIDE AT UNDERWING CANTED KEEL INTERNAL STRUCTURE. SUMMARY OF NRC 0197: FRAME CLIP STA Y=715 LH SIDE AT UNDERWING CANTED KEEL INT
- [SDR DALA2023072105923](https://openairdocs.org/sdr/DALA2023072105923), Jul 20, 2023: UNKNOWN. UNKNOWN. CRACKS ON RH WINDOW PANS ON STA Y=238 FWD UP CORNER, STA Y=294 FWD UP CORNER, STA Y=370 FWD UPPER CORNER, STA Y=636 FWD LOWER CORNER, STA Y=851 AFT LOWER CORNER
- [SDR DALA2023071705781](https://openairdocs.org/sdr/DALA2023071705781), Jul 16, 2023: UNKNOWN. UNKNOWN. CORROSION ON PLATE IN STA Y=1053 BTW LONGERONS 29R-29L AT AFT BULKHEAD AT AFT CARGO COMPARMENT. SUMMARY OF NRC 203: LEVEL CORROSION 2. DOUBLER (PLATE) WAS REPLA
- [SDR DALA2023071705780](https://openairdocs.org/sdr/DALA2023071705780), Jul 16, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP MEMBRANE LOWER SURFACE ON STA Y=645 AND X=-44 AT CPAX. SUMMARY OF NRC 421: CUSP MEMBRANE LOWER SURFACE ON STA Y=645 AND X=-44 AT CPAX WAS REPAIRED
- [SDR DALA2020022601416](https://openairdocs.org/sdr/DALA2020022601416), Feb 25, 2020: BATTERY PACK. INOPERATIVE. REAR AIRCRAFT, ABOVE JUMPSEAT, THE EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND POWER SUPPLY PER AMM 33-51-03. OPERATIONAL CHECK IS GOOD
- [SDR DALA2020011400239](https://openairdocs.org/sdr/DALA2020011400239), Jan 13, 2020: POWER SUPPLY. INOPERATIVE. EMERGENCY OVER WING EXIT SIGN IS INOPERATIVE AT B20DC. MAINTENANCE REPLACED THE POWER SUPPLY, EMERGENCY BATTERY AT 20DC, RIGHT HAND AFT EMERGENCY EXIT PER AMM 3
- [SDR DALA2019120507056](https://openairdocs.org/sdr/DALA2019120507056), Dec 5, 2019: BATTERY PACK. INOPERATIVE. OVERHEAD EMERGENCY LIGHTS IN REAR TAIL CONE ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK, B5-116, IN THE AFT RIGHT LAVATORY. THE OVERHEAD EMERGENCY LI
- [SDR DALA2019120206971](https://openairdocs.org/sdr/DALA2019120206971), Nov 27, 2019: POWER SUPPLY. MALFUNCTIONED. THE AFT CATWALK AND AFT EMERGENCY EXIT DOORWAY LIGHTS ARE FLICKERING ON AND OFF. MAINTENANCE REPLACED THE AFT CATWALK EMERGENCY POWER SUPPLY IAW B717 AMM 33-51-
- [SDR DALA2019092305439](https://openairdocs.org/sdr/DALA2019092305439), Sep 21, 2019: BATTERY. DISCHARGED. UPON ARRIVAL AT THE GATE IN ATL, THE AFT EMERGENCY EXIT LIGHT WAS FLASHING. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY. OPERATIONAL CHECK WAS GOOD PER AM
- [SDR DALA2019091805389](https://openairdocs.org/sdr/DALA2019091805389), Sep 18, 2019: LUG. CORRODED. CORROSION FOUND ON RT FWD AND AFT FACES OF THE RHS FIXED BRACE ATTACH LUG. REPAIRED PER ER/A 581446-14 REV ORIGINAL. ASSOCIATED ER/A 14-581446 ADDED FOR AC 9518
- [SDR DALA2019091805387](https://openairdocs.org/sdr/DALA2019091805387), Sep 18, 2019: LUG. CORRODED. CORROSION FOUND ON LT FWD AND AFT FACES OF THE LHS FIXED BRACE ATTACH LUG. REPAIRED PER ER/A 581445-14 REV ORIGINAL. ASSOCIATED ER/A 14-581445 ADDED FOR AC 9518
- [SDR DALA2019060603431](https://openairdocs.org/sdr/DALA2019060603431), Jun 5, 2019: POWER SUPPLY. MALFUNCTIONED. EXIT LIGHT OVER TAILCONE EXIT AND AIRCRAFT RIGHT STANDBY EMERGENCY LIGHT FLICKER INTERMITTENTLY DURING ALL PHASES OF FLIGHT. MAINTENANCE RE-SET AFT POWER PACK A
- [SDR DALA20190221082](https://openairdocs.org/sdr/DALA20190221082), Feb 20, 2019: POWER SUPPLY. INOPERATIVE. THE EMERGENCY EXIT SIGN IS INOPERATIVE AT LOCATIONS:102. MAINTENANCE FOUND THE AFT LIGHT AND ESCAPE SECTION EMERGENCY LIGHT POWER PACK TO BE INOPERATIVE. THE PO
- [SDR DALA2019020410715](https://openairdocs.org/sdr/DALA2019020410715), Jan 31, 2019: COVER. DAMAGED. THE TAIL-CONE SLIDE COVER HAS A BROKEN CLIP FOR THE RELEASE CABLE. MAINTENANCE INSTALLED A NEW CLIP. (LP #0926413)
- [SDR DALA2018100305847](https://openairdocs.org/sdr/DALA2018100305847), Oct 3, 2018: POWER SUPPLY. DEFECTIVE. THE EMERGENCY EXIT SIGN ABOVE THE DOOR TO THE AFT ACCESSORY COMPARTMENT IS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY BASE AND THE LIGHT RETURNED TO NOR
- [SDR DALA2016081906087](https://openairdocs.org/sdr/DALA2016081906087), Aug 18, 2016: SKIN. DAMAGED. VERTICAL STAB RIGHT SIDE BELOW AND FORWARD OF LOWER RIGHT VOR ANTENNA SEVERAL SCREWS PULLED THROUGH SKIN. REPAIR WAS ACCOMPLISHED IAW ER/A 549263-14AD REV. ORIG
- [SDR DALA2016081806070](https://openairdocs.org/sdr/DALA2016081806070), Aug 17, 2016: SKIN. GOUGED. GOUGES ON RIGHT WING FIXED LE BETWEEN XIS 83.5, XIS 90 AND XIS 120. GOUGES WERE BLENDED IAW SRM 57-00-00 FIG 103. BHEC INSPECTION WAS ACCOMPLISHED ON DRILLED HO
- [SDR DALA2016081706042](https://openairdocs.org/sdr/DALA2016081706042), Aug 17, 2016: ACCESS PANEL. CORRODED. CORROSION ON COUTERSINKS AT FUEL TANK ACCESS NR 520JB, SM. CORROSION OF COUNTERSINK WAS REMOVED IAW SRM 51-10-04. REWORKED AREAS WERE MEASURED AND MAX DIAMETER 
- [SDR DALA2016081706041](https://openairdocs.org/sdr/DALA2016081706041), Aug 17, 2016: ACCESS PANEL. CORRODED. CORROSION ON COURTERSINKS AT FUEL TANK ACCESS NR 520EB, SM. CORROSION OF COUNTERSINKS WAS REMOVED IAW SRM 51-10-04. REWORKED AREAS WERE MEASURED AND MAX DIAMETE

All 213: https://openairdocs.org/aircraft/N959AT/reports.md

## STCs that may be installed (OpenAirDocs) (71, first 50)

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 (Boeing 717-200)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST02463AT](https://openairdocs.org/stc/ST02463AT): Installation of an Intrusion/Penetration Resistance Flightdeck Door and Reinforced Flightdeck Door Surround. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST04122AT](https://openairdocs.org/stc/ST04122AT): Installation of an oven. AIRCRAFT RECONFIG TECHNOLOGIES, 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 ST04816NY](https://openairdocs.org/stc/ST04816NY): Installation of Electronically Steerable (ESA) Antenna and Power Supply. ALOFT AeroArchitects
- [STC ST12026AT](https://openairdocs.org/stc/ST12026AT): Installation of Portable Emergency Locator Transmitter. Delta Flight Products LLC
- [STC ST02478NY](https://openairdocs.org/stc/ST02478NY): Installation of an advertisement container on the bottom of a seat back tray table on Weber Model 5300 passenger seats (Weber Part Numbers 852454, 852455, 852456, 852457, 852458, and 852459). Atin OOH, LLC
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST04813NY](https://openairdocs.org/stc/ST04813NY): Installation of Hughes Satellite Connectivity and Wifi Cabin Distribution System. ALOFT AeroArchitects
- [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 ST03682AT](https://openairdocs.org/stc/ST03682AT): Installation of an Aircell Broadband Service (ABS) Passenger Cabin Air-To-Ground (ATG) Voice/Data Communication System. Amphenol Cable and Interconnect Technologies Inc
- [STC ST11388DS](https://openairdocs.org/stc/ST11388DS): Expansion of the Delta Comfort+® Passenger Seating Section. Aircraft Systems and Manufacturing Inc
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST02637AT](https://openairdocs.org/stc/ST02637AT): Installation of SafTGlo Inc. photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC SA9024NM-D](https://openairdocs.org/stc/SA9024NM-D): Installation of Scandinavian Bellyloading Company, sliding carpet loading system. SBC-America LLC
- [STC ST04416AT](https://openairdocs.org/stc/ST04416AT): Installation of the Rockwell Collins Multi-Mode Receiver (MMR). Woven Electronics LLC
- [STC ST04418AT](https://openairdocs.org/stc/ST04418AT): Installation of the Rockwell Collins Automatic Dependent Surveillance - Broadcast (ADS-B) Out System. Woven Electronics LLC
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC ST01465LA-D](https://openairdocs.org/stc/ST01465LA-D): Installation of B/E Aerospace, Inc. Air Chiller Part Number 374-8. B/E Aerospace Inc
- [STC ST01023SE](https://openairdocs.org/stc/ST01023SE): Installation of a the TPA-81A Traffic Alert and Collision Avoidance System (TCAS) Processor in accordance with Master Drawing List 756-0119-001, Revision D, dated November 21, 2003, or later FAA approved revisions. Honeywell International Inc
- [STC ST01096SE](https://openairdocs.org/stc/ST01096SE): Installation of the Mark III Aircraft Communications Addressing and Reporting System (ACARS). Honeywell International Inc
- [STC ST01640SE](https://openairdocs.org/stc/ST01640SE): Installation of the Mark III Aircraft Communications Addressing and Reporting System (ACARS). Honeywell International Inc
- [STC ST03418NY](https://openairdocs.org/stc/ST03418NY): Installation of a UTC Electronic Flight Bags. Rockwell Collins Inc
- [STC ST03574AT](https://openairdocs.org/stc/ST03574AT): Installation of a Talon Aerospace Anti-Collision Light. Aaxico Technical Services Inc
- [STC ST04002AT](https://openairdocs.org/stc/ST04002AT): Installation of a Talon LED Replacement Wing and Tail Mounted Anti-Collision Lights. Aaxico Technical Services Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04029CH](https://openairdocs.org/stc/ST04029CH): Modification of an existing Aircell Broadband Services (ABS) System with ATG4 Enhancements. Intelsat Inflight LLC
- [STC ST02532LA](https://openairdocs.org/stc/ST02532LA): Modify the wing fuel tanks access cover installation by replacing the existing rubstrip and seal with a new encapsulated wire mesh gasket and a new seal. Aviation Devices & Electronic Components LLC
- [STC ST04425CH](https://openairdocs.org/stc/ST04425CH): Installation of a Honeywell One Aero Edge Node (1AEN) in accordance with StandardAero Master Data List 1037081, Revision (B), dated June 9, 2020 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST04424CH](https://openairdocs.org/stc/ST04424CH): TPED Compatibility Test in accordance with StandardAero Master Data List 1037140, Revision (B), dated June 1, 2020 or later FAA approved revision. Standard Aero Business Aviation Services LLC
- [STC ST04468NY](https://openairdocs.org/stc/ST04468NY): Installation of Honeywell ADS-B Transponder Upgrade. H4 Aerospace (UK) Ltd
- [STC ST02152LA](https://openairdocs.org/stc/ST02152LA): Installation of AmSafe Aviation Inflatable Restraint (AAIR) System. AMSAFE Inc
- [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 SA8339SW](https://openairdocs.org/stc/SA8339SW): Installation of a fuselage nose radome shell. The NORDAM Group LLC
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST04229NY](https://openairdocs.org/stc/ST04229NY): Introduction of a 16G New Generation Stretcher XL P/N 1120030-Series. Bucher Leichtbau AG
- [STC ST04167NY](https://openairdocs.org/stc/ST04167NY): Installation of TCAS System upgrade to Change 7.1. H4 Aerospace (UK) Ltd
- [STC ST03846NY](https://openairdocs.org/stc/ST03846NY): Installation of SuperSeal UltraLite (SSUL) PHOTOLUMINESCENT AISLE PATH MARKING SYSTEM. STG Aerospace Ltd
- [STC ST04242CH](https://openairdocs.org/stc/ST04242CH): Installation of ACSS Automatic Dependent Surveillance-Broadcast (ADS-B) compliant Mode S Transponders. Canard Aerospace Corporation
- [STC ST04186CH](https://openairdocs.org/stc/ST04186CH): Retrofit installation of Rosemount Aerospace Model 0861EW2 Angle of Attack (AOA) Sensors. Rosemount Aerospace Inc
- [STC ST02479SE](https://openairdocs.org/stc/ST02479SE): Installation of class dividers and cross aisle curtain headers. Northwest Aerospace Technologies Inc
- [STC SA7076NM](https://openairdocs.org/stc/SA7076NM): Installation of Stretcher Carrier. Air Medic LLC
- [STC ST02991AT](https://openairdocs.org/stc/ST02991AT): Installation of LiveTV XM Satellite Radio System. Thales Avionics Inc
- [STC ST03449CH](https://openairdocs.org/stc/ST03449CH): Installation of LH and RH Passenger Window - STA 218 to STA 237. AAR Aircraft Services
- [STC ST04206AT](https://openairdocs.org/stc/ST04206AT): Interior reconfiguration. Delta Air Lines Inc
- [STC ST03442CH](https://openairdocs.org/stc/ST03442CH): Installation of New Interior Arrangement. AAR Aircraft Services
- [STC ST03817AT](https://openairdocs.org/stc/ST03817AT): Installation of a Thales-KANNAD Emergency Locator Transmitter. Avionics Support Group Inc

All 71: https://openairdocs.org/aircraft/N959AT/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md
- The BMW Rolls BR-700 series engine: https://openairdocs.org/engine/bmw-rolls-br-700-series.md

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