# N985AT: 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: 55090
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 18, 2001
- Certificate issued: May 21, 2025
- Expires: May 31, 2032
- Mode S code: ADBDC9
- 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=985AT
- Page: https://openairdocs.org/aircraft/N985AT

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/N985AT/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 N985AT.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20091004049939I](https://openairdocs.org/incident/20091004049939I), Oct 4, 2009: Boeing 717-200 (N985AT), Orlando, FL, No damage. Airtran flight 904/04 oct (mco-atl) on departure from kmco rwy 17R at approximately 300-400 AGL the crew heard a loud bang and experienced a yaw to the left.…

## Service difficulty reports (176, 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 DALA2026072204283](https://openairdocs.org/sdr/DALA2026072204283), Jul 21, 2026: LIGHT. FAULTED. CHEMICAL BURNING ODOR APPEARED THE FIRST FEW MINUTES IN ENTIRE AIRCRAFT, R & R UPPER ANTI COLLISION LIGHT IAW AMM 33-42. (9223935) (AIRCRAFT GROUNDED).
- [SDR DALA2026062103688](https://openairdocs.org/sdr/DALA2026062103688), Jun 21, 2026: BATTERY PACK. INOPERATIVE. TAIL COMP O/H EMERG LIGHTS INOP. REPLACED B5-116 BATTERY PACK IAW AMM 33-51-04. (LP 8290307 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026021901201](https://openairdocs.org/sdr/DALA2026021901201), Feb 18, 2026: STRAP. CRACKED. AIRCRAFT 9585, CRACK ON STRAP BTW UPPER PYLON LH AND Y=1178 AT AFT FUSELAGE AREA. CORRECTIVE ACTION: STRAP BTW UPPER PYLON LH AND Y=1178 AT AFT FUSELAGE AREA WA
- [SDR DALA2026020900905](https://openairdocs.org/sdr/DALA2026020900905), Feb 2, 2026: HINGE FITTING. CORRODED. CORROSION ON LOWER OUTBOARD ATTACH POINT ( STUD) AND MIDDLE FLAP HINGE FITTING STA Y XRS 267 APPROX AT RH WING. REPAIRED PER ER/A 14-631617 (1432236)
- [SDR DALA2026010500064](https://openairdocs.org/sdr/DALA2026010500064), Dec 30, 2025: NONE. NONE. TRACKING FOR ACCOMPLISHMENT OF ER/A 615647-14AD. ACCOMPLISHMENT OF ER/A 615647-14A (1377242)
- [SDR DALA2026020900908](https://openairdocs.org/sdr/DALA2026020900908), Oct 24, 2025: SKIN. DAMAGED. ERA 630089-14, SECTION I, ISSUED FOR BIRD STRIKE DAMAGE TO RT HORIZONTAL STAB LEADING EDGE INBD STRUCTURE. REPAIRED IAW ER/A 630089-14. (1269533)
- [SDR DALA2025102207718](https://openairdocs.org/sdr/DALA2025102207718), Oct 17, 2025: BATTERY PACK. INOPERATIVE. CREW REPORT EXIT SIGN F/C INOP (EMERRGENCY LIGHT). FOUND BATTERY PACK B5-259 INOP, REPLACED BATTERY PACK. OPS CHEC K GOOD, IAW B717AMM 33-51. (7585679)
- [SDR DALA2025100807355](https://openairdocs.org/sdr/DALA2025100807355), Oct 7, 2025: DOOR. OPEN. ATB- PERFORMED AN AIR TURN BACK DUE TO A NOSE GEAR AREA VIBRATION. MAINTENANCE CLOSED THE NOSE GEAR DOORS, CONFIRMED THE SECURITY AND CONDITION OF THE DOORS AND
- [SDR DALA2025051403732](https://openairdocs.org/sdr/DALA2025051403732), May 14, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS OVERWING EXIT AND CEILING LIGHT ARE ALL INOPERATIVE. MAINTENANCE FOUND B5-230 BATTERY PACK NOT WORKING. THE BATTERY PACK B5-230 WAS REPLACED PE
- [SDR DALA2025043003313](https://openairdocs.org/sdr/DALA2025043003313), Apr 29, 2025: BATTERY. INOPERATIVE. THE OVERHEAD CEILING EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 24-28. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY ASSEMBLY B5-231 PER B717 AMM 33-51. OPERAT
- [SDR DALA2025030701776](https://openairdocs.org/sdr/DALA2025030701776), Mar 6, 2025: CONTROLLER. FAULTED. SHIP 9585 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC DUE TO A "TAIL ANTI-ICE MANIFOLD FAIL" MESSAGE ILLUMINATING ABOUT 20 MINUTES FROM LANDING. CO
- [SDR DALA2025021801197](https://openairdocs.org/sdr/DALA2025021801197), Feb 17, 2025: A/C PACK. SMOKE. SHIP 9585 -ATB/SMKE/DE- THE CREW RETURNED THE FLIGHT BACK TO SDF DUE TO VISIBLE SMOKE AND ODOR IN THE MAIN CABIN. CORRECTIVE ACTION: MAINTENANCE ISOLATED THE SO
- [SDR DALA2025021801201](https://openairdocs.org/sdr/DALA2025021801201), Feb 15, 2025: A/C PACK. ODOR. SHIP 9585 -ATB/SMKE/DE- THE FLIGHT CREW AND CABIN CREW BOTH REPORTED SMOKE IN COCKPIT AND CABIN SOON AFTER TAKEOFF. AN EMERGENCY WAS DECLARED WITH ATC AND THE A
- [SDR DALA2024112611223](https://openairdocs.org/sdr/DALA2024112611223), Nov 8, 2024: BULKHEAD. MECHANIC ERROR. -AD- ACCOMPLISH ER/A 551838-14AD REV A SECTION II FUSELAGE / BULKHEADS / CANTED STA 1178 FRAME / MISDRILLED HOLES. ACCOMPLISH ER/A 551838-14AD REV A SECTION II 
- [SDR DALA2024091909182](https://openairdocs.org/sdr/DALA2024091909182), Sep 17, 2024: ACTUATOR. LEAKING. SHIP 9585 -DIV/FUME/DE- ENROUTE TO MDT THE FLIGHT WAS DIVERTED TO IAD FOLLOWING STRONG SULFUR FUMES THROUGHOUT THE COCKPIT AND CABIN. MAINTENANCE FOUND THE NOSE
- [SDR DALA2024031203225](https://openairdocs.org/sdr/DALA2024031203225), Mar 11, 2024: SPAR. CRACKED. CRACK ON REAR SPAR APPROX XRS 145 AT LH WING. ERA 61543-14 REV ORIG SECTION I AND II ACCOMPLISHED ON NRC 628 IN TOMX. NEEDS SECTION III ACCOMPLISHED. SUMMARY OF
- [SDR DALA2024031103219](https://openairdocs.org/sdr/DALA2024031103219), Mar 10, 2024: SPAR CAP. CRACKED. ERA 615647-14AD REV ORIG - LH WING REAR SPAR LOWER CAP AT XRS=159 IS CRACKED. COMPLIED WITH ERA 615647-14AD REV ORIG PRI "0", "1", "2", "3, "4", "5", "6", "7", 
- [SDR DALA2024031103218](https://openairdocs.org/sdr/DALA2024031103218), Mar 10, 2024: SKIN. CRACKED. LOWER WING SKIN AND DOUBLER PER PRI 615647-14AD, REV 1, STEP 23, SHOWS CRACK INDICATIONS (3 EA) COMMON TO LOWER WING SKIN DOUBLER BELOW XRS164, ALONG INBOARD ED
- [SDR DALA2024031103217](https://openairdocs.org/sdr/DALA2024031103217), Mar 10, 2024: SKIN. CRACKED. INSPECTION OF LOWER WING SKIN AND DOUBLER PER PRI 615647-14AD, REV 1, STEP 23, SHOWS CRACK INDICATIONS (4 EA) COMMON TO LOWER WING SKIN DOUBLER AT XRS 164. 1 EA
- [SDR DALA2024031203226](https://openairdocs.org/sdr/DALA2024031203226), Feb 6, 2024: SPAR. CRACKED. CRACK ON REAR SPAR APPROX XRS 145 AT LH WING. ERA 615453-14 AD REV ORIG SECTION I AND SECTION II ACCOMPLISHED ON NRC 7628 IN TOMX. NEEDS SECTION III ACCOMPLISHE
- [SDR DALA2024012901228](https://openairdocs.org/sdr/DALA2024012901228), Jan 28, 2024: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL OVER STRG 29R AND 28R BTW STA Y=927 TO 946 AT AFT CARGO CPMPARMENT. SUMMARY OF NRC 00271: CORROSION LEVEL 2. INTERCOSTALS OVER STRG 29R
- [SDR DALA2024012501109](https://openairdocs.org/sdr/DALA2024012501109), Jan 25, 2024: FINGER DOUBLER. CORRODED. CORROSION ON FINGER DOUBLER STA 944, 972, 1001, AND 1004 BTW STRG 26L/27L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00194: CORROSION LEVEL 2. FINGER DOUBLER BTW S
- [SDR DALA2024012200904](https://openairdocs.org/sdr/DALA2024012200904), Jan 19, 2024: WEB. CORRODED. CORROSION ON WEB BTW STA Y=200/205 AND L 18L AND L 17L AT DOOR JAMB L1. SUMMARY OF NRC 00304: CORROSION LEVEL 2. CORROSION ON WEB BTW STA Y=200/205 AND L 18L AN
- [SDR DALA2024011900809](https://openairdocs.org/sdr/DALA2024011900809), Jan 19, 2024: WEB. CRACKED. CRACK ON WEB STA Y=674 X=55 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00311: WEB STA Y=674 X=55 AT PASSENGER CABIN WAS REPAIRED PER ERA 614715-14 REV ORIGINAL S
- [SDR DALA2024011900808](https://openairdocs.org/sdr/DALA2024011900808), Jan 18, 2024: CUSP WEB. CORRODED. CORROSION ON CUSP WEB (UPPER AREA) BTW STA 579-598, 609-617, 658-678, AND 720-756 AT CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00560: CORROSION LEVEL 2. CORROSION O
- [SDR DALA2024011700680](https://openairdocs.org/sdr/DALA2024011700680), Jan 17, 2024: WEB. CRACKED. CRACKS ON WEBS AT 11 O'CLOCK POSITION STA Y=1200 AT AFT ACC COMPARTMENT. SUMMARY OF NRC 00238: WEB AT 11 O'CLOCK POSITION STA Y=1200 AT AFT ACC COMPARTMENT WAS 
- [SDR DALA2024011700679](https://openairdocs.org/sdr/DALA2024011700679), Jan 17, 2024: WEB. CRACKED. CRACK WAS FOUND ON WEB BTW STA 182 AND X=-6 AT E/E COMPARTMENT. SUMMARY OF NRC 00607: WEB BTW STA 182 AND X=-6 AT E/E COMPARTMENT WAS REPAIRED PER B717-200 SRM 
- [SDR DALA2024011700678](https://openairdocs.org/sdr/DALA2024011700678), Jan 16, 2024: BEAM. CRACKED. CRACKS ON BEAM #1, STA Y=200 AT PAX CABIN DOOR L1. SUMMARY OF NRC 00595: BEAM #1, STA Y=200 AT PAX CABIN DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROC
- [SDR DALA2024011600589](https://openairdocs.org/sdr/DALA2024011600589), Jan 15, 2024: WEB. CRACKED. CRACK ON WEB STA Y=715 X=44 AND X=-44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00312: WEB STA Y=715 X=44 AND X=-44 AT PASSENGER CABIN WERE REPAIRED PER B717-20
- [SDR DALA2024011500573](https://openairdocs.org/sdr/DALA2024011500573), Jan 13, 2024: UNKNOWN. UNKNOWN. CRACK ON CUSP WEB IN STA Y=713 AND X=55 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00596: CUSP WEB IN STA Y=713 AND X=55 AT PASSENGER CABIN STRUCTURE WAS REPA
- [SDR DALA2024011600586](https://openairdocs.org/sdr/DALA2024011600586), Jan 12, 2024: UNKNOWN. UNKNOWN. CRACKS ON BEAM #1, STA Y=160 AND Y=200 AT PAX CABIN DOOR L1. SUMMARY OF NRC 00199: BEAM #1, STA Y=160 AT PAX CABIN DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-0
- [SDR DALA2024011500572](https://openairdocs.org/sdr/DALA2024011500572), Jan 12, 2024: UNKNOWN. UNKNOWN. CUSP WEB AT STA Y=928, BTW STA Y=920 TO STA Y=935, WAS FOUND CRACKED. SUMMARY OF NRC 00581: CUSP WEB AT STA Y=928 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROC
- [SDR DALA2024010500148](https://openairdocs.org/sdr/DALA2024010500148), Jan 5, 2024: UNKNOWN. UNKNOWN. CORROSION ON PREVIOUS REPAIR CUSP WEB LH SIDE STA Y=542. SUMMARY OF NRC 00363: CORROSION LEVEL 2. PREVIOUS REPAIR CUSP WEB LH SIDE STA Y=542 WAS REPLACED PER B7
- [SDR DALA2023122810693](https://openairdocs.org/sdr/DALA2023122810693), Dec 24, 2023: UNKNOWN. UNKNOWN. MAINTENANCE FOUND THE KEVLAR CABLE FOR THE RELEASE MECHANISM INSIDE TAILCONE TO BE TORN. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NO
- [SDR DALA2023031401855](https://openairdocs.org/sdr/DALA2023031401855), Mar 12, 2023: UNKNOWN. UNKNOWN. THE AFT 3 CENTER AISLE CEILING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENACE REPLACED THE EMERGENCY LIGHT BATTERY PACK ROW 24-29 IAW B717 AMM 33-51. OPERATIONAL 
- [SDR DALA2023012600640](https://openairdocs.org/sdr/DALA2023012600640), Jan 20, 2023: OIL SYSTEM. LEAKING. SHIP 9585 -SMKE- DURING BOARDING WITH APU RUNNING PACKS, SMOKE AND ODOR FILLED THE CABIN. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE APU HAD FAILED AND DUMPE
- [SDR DALA2022082905773](https://openairdocs.org/sdr/DALA2022082905773), Aug 28, 2022: UNKNOWN. UNKNOWN. AIRCRAFT 9585, EMERGENCY LIGHT ABOVE FWD F/A SEAT INOP. CORRECTIVE ACTION: REPLACED BATTERY POWER SUPPLY PER B717 AMM 33-51, OPERATIONAL CHECK GOOD. ( LP 905179
- [SDR DALA2022060804012](https://openairdocs.org/sdr/DALA2022060804012), Jun 5, 2022: THERMOSWITCH. MISALIGNED. SPARKS EMITTED FROM CA WINDSHIELD WHEN ANTI-FOG SWITCH TURNED ON. FWD TO B717 MEL 30-41-01A. 'M' PROC C/W. MEL/PLAC INSTALLED. OK FOR SVC. *********************
- [SDR DALA2022050503143](https://openairdocs.org/sdr/DALA2022050503143), May 5, 2022: COMPRESSOR. STALLED. SHIP 9585 - THE CREW ABORTED THE TAKE-OFF AT 103 KNOTS FOLLOWING THE #2 ENGINE COMPRESSOR STALL AFTER INGESTING A MYLAR BALLOON FLOATING OVER THE RUNWAY. CORREC
- [SDR DALA2022041202527](https://openairdocs.org/sdr/DALA2022041202527), Apr 8, 2022: NONE. NONE. SHIP 9585 - THE FLIGHT CREW SAFELY ABORTED THE TAKEOFF ROLL AT 100 KTS. DUE TO A "STAB TRIM" MESSAGE WITH AN AURAL WARNING. CORRECTIVE ACTION: MAINTENANCE FOUND
- [SDR DALA2022040602320](https://openairdocs.org/sdr/DALA2022040602320), Apr 1, 2022: DOOR. CRACKED. FOUND FWD CARGO DOOR CRACKED/ DAMAGED DURING PRESSURIZATION CHECK. SUMMARY SEE NRC 001-0051:5230-2004/004 00500: REPLACED CARGO DOOR PER B717 AMM 52-31-01. REMO
- [SDR DALA2022040602324](https://openairdocs.org/sdr/DALA2022040602324), Mar 31, 2022: STIFFENER. CORRODED. AFT CARGO COMPARTMENT STA 1053, VERTICAL STIFFENER, AFT SIDE OF BULKHEAD AT STRINGER 29L CORRODED AT LOWER TIP. MARKED. CORROSION LEVEL 2, REPLACED STIFFENER PE
- [SDR DALA2022040602323](https://openairdocs.org/sdr/DALA2022040602323), Mar 31, 2022: STRINGER. CRACKED. AFT CARGO COMPARTMENT, STRINGER 28L CORRODED FROM STATION 1010 - 1022. WORK WITH NRC 357: CORROSION LEVEL 2, REPLACED STRINGER 28L, SPLICE (1) AND CLIP (1) FROM
- [SDR DALA2022040202241](https://openairdocs.org/sdr/DALA2022040202241), Mar 30, 2022: NONE. NONE. AFT CARGO COMPARTMENT, SHEAR TIE, LOWER LEG AT STA 1002 CORRODED. SUMMARY SEE NRC 046-0008:5331-2001/014 00358: CORROSION LEVEL 2, INSTALLED REPAIR SHEAR TIE PE
- [SDR DALA2022040202240](https://openairdocs.org/sdr/DALA2022040202240), Mar 30, 2022: NONE. NONE. AFT CARGO STA 1002, OUTBAORD OF STRINGER 28L, INTERCOSTAL CORRODED NEAR SKIN. SUMMARY SEE NRC 046-0008:5331-2001/037 00435: CORROSION LEVEL 2, REPLACED INTERCOS
- [SDR DALA2022040202239](https://openairdocs.org/sdr/DALA2022040202239), Mar 30, 2022: NONE. NONE. AFT CARGO STRINGER 30 BETWEEN STATIONS 1022-1037 CORRODED. SUMMARY SEE NRC 046-0008:5331-2001/017 00363: CORROSION LEVEL 2, REPLACED INTERCOSTAL AT STA 1022-103
- [SDR DALA2022040202238](https://openairdocs.org/sdr/DALA2022040202238), Mar 30, 2022: NONE. NONE. AFT CARGO COMPARTMENT, 3 EACH SKIN SPLICE PLATES BETWEEN STATIONS 1015 - 1037 BETWEEN STRINGERS 29R - 29L CORRODED. SUMMARY SEE NRC 046-0008:5331-2001/015 00359
- [SDR DALA2022040202237](https://openairdocs.org/sdr/DALA2022040202237), Mar 30, 2022: NONE. NONE. AFT CARGO COMPARTMENT, SHEAR TIE AT STA 1022 (AFT BULKHEAD) CORRODED BETWEEN STRINGERS 29R - 29L. SUMMARY SEE NRC 046-0008:5331-2001/016 00360: CORROSION LEVEL 
- [SDR DALA2022040202236](https://openairdocs.org/sdr/DALA2022040202236), Mar 30, 2022: NONE. NONE. AFT CARGO STA 1022 AFT SIDE OF FRAME CORRODED BETWEEN 29RT AND 29LT. SUMMARY SEE NRC 046-0008:5331-2001/027 00424: INSTALLED REPAIR PARTS PER B717 SRM 53-20-07-
- [SDR DALA2022040202235](https://openairdocs.org/sdr/DALA2022040202235), Mar 30, 2022: NONE. NONE. AFT CARGO COMPARTMENT, STRINGER 28L CORRODED FROM STATION 994-1010. SUMMARY SEE NRC 046-0008:5331-2001/013 00357: CORROSION LEVEL 2, REPAIRED PER B717 SRM 53-00

All 176: https://openairdocs.org/aircraft/N985AT/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/N985AT/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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