# N986AT: 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: 55089
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 11, 2001
- Certificate issued: May 15, 2025
- Expires: May 31, 2032
- Mode S code: ADC180
- 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=986AT
- Page: https://openairdocs.org/aircraft/N986AT

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/N986AT/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 N986AT.

## FAA accident and incident reports

None matched to N986AT.

## Service difficulty reports (184, 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 DALA2026102205831](https://openairdocs.org/sdr/DALA2026102205831), Oct 22, 2026: FUEL CELL. LEAKING. DURING REAR SPAR AND LWR SKIN INSPECTION FOUND FUEL LEAKING AT THE LOWER SKIN DOUBLER ON THE FWD EDGE, COMPLIED WITH ER/A 621136-14AD. (9191047) (AIRCRAFT GROUN
- [SDR DALA2026092805397](https://openairdocs.org/sdr/DALA2026092805397), Sep 26, 2026: BATTERY PACK. INOPERATIVE. E-LIGHTS POWER BY B5-230 AND B5-119 INOP DURING SVC CHECK. R/R BATTERY TRAY FOR B5-230 AND R/R BATTERY AND BATTERY TRAY FOR B5-119 REF B717 AMM 33-51. CHECKS GO
- [SDR DALA2026071404142](https://openairdocs.org/sdr/DALA2026071404142), Jul 13, 2026: DAMPENER. FAULTED. ATB- PERFORMED AN AIR TURN BACK DUE TO SPLIT ELEVATOR INDICATION. REPLACED RT ELEVATOR DAMPER IAW AMM 27-31 OPS CHK GOOD. (8424292) (AIRCRAFT GROUNDED).
- [SDR DALA2026070803993](https://openairdocs.org/sdr/DALA2026070803993), Jul 8, 2026: FUEL CELL. LEAKING. FOUND FUEL LEAK AT RT WING LOWER XRS164 AFT OTBD 2 LOWER BOLTS, COMPLIED WITH ER/A 621136-14AD. (8424279) (AIRCRAFT GROUNDED).
- [SDR DALA2026061603617](https://openairdocs.org/sdr/DALA2026061603617), Jun 15, 2026: DISPLAY. FAULTED. ATB- RETURNED FROM FLIGHT DUE TO RECEIVING ENGINE SYSTEM FAIL MESSAGES ON BOTH ENGINES. REPLACED CAPTAIN'S AND FIRST OFFICER'S MCDU, AND FCC 1 AND 2, AND GCP. (
- [SDR DALA2026051102946](https://openairdocs.org/sdr/DALA2026051102946), May 6, 2026: SKIN. GROUND DAMAGE. AIRCRAFT STRUCK BY BAG LOADER AND KNOCKED OFF COMM 1 ANTENNA. REPAIRED PER ERA 634130-14 (6545520) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402366](https://openairdocs.org/sdr/DALA2026041402366), Apr 12, 2026: POWER SUPPLY. NO TEST. EMERGENCY LIGHTS AT OVERWING EMERGENCY DOORS AND CEILING PANEL DON'T TURN ON. SERVICEABLE EMERGENCY POWER SUPPLIES (2EA) AND SERVICEABLE EMERGENCY BATTERIES ASS
- [SDR DALA2026041402363](https://openairdocs.org/sdr/DALA2026041402363), Apr 11, 2026: FRAME ANGLE. CRACKED. CRACK ON ANGLE CAP OF FRAME BTW L16L AND L17L STA Y= 1178 CANT AT AFT ACCESORIES COMPARTMENT. REPAIRED PER PRI 633430-14 (1538578) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402362](https://openairdocs.org/sdr/DALA2026041402362), Apr 11, 2026: FRAME ANGLE. CRACKED. CRACK ON ANGLE CAP OF FRAME BTW L16R AND L17R STA Y= 1178 CANT AT AFT ACCESORY COMPARTMENT. REPAIRED PER PRI 633462-14 (1538572) (AIRCRAFT GROUNDED)
- [SDR DALA2026031901910](https://openairdocs.org/sdr/DALA2026031901910), Mar 18, 2026: TEE FITTING. OUT OF POSITION. LEFT WING T/E RIB 3 TEE HAS A .030 GAP AT SKIN. SPLICE REPAIR OF WING REAR SPAR LOWER CAP BETWEEN PRODUCTION SPLICE AT XRS 111.5 AND REPAIR SPLICE AT XRS 192 BA
- [SDR DALA2026031901913](https://openairdocs.org/sdr/DALA2026031901913), Mar 14, 2026: HINGE FITTING. WORN. AIRCRAFT 9584, LH FLAP IDLER HINGE FITTING WORN. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FLANGED BUSHING SIMILAR TO PRODUCTION BUSHING P/N 4913570-1. 
- [SDR DALA2026031001648](https://openairdocs.org/sdr/DALA2026031001648), Mar 4, 2026: NOT REPORTED. NOT REPORTED. ER/A 627199-14AD REV F REQUIRES STAGE 2 DTA APPROVAL. REPAIRED PER ER/A 00-627199. (1478991)
- [SDR DALA2026020200756](https://openairdocs.org/sdr/DALA2026020200756), Jan 27, 2026: HINGE FITTING. WORN. THE LEFT WING FLAP IDLER HINGE FITTING INBD AND OTBD LUG INNER FACES WERE FOUND WORN AND ELONGATED BEYOND THE LIMITS OF CMM 27- 50-5. REPAIRED IAW ER/A 14-62996
- [SDR DALA2025090906664](https://openairdocs.org/sdr/DALA2025090906664), Sep 2, 2025: BATTERY PACK. INOPERATIVE. EMERGENCEY LIGHTS ROW 20-21 EXIT LIGHTS INOP. R & R BATTERY PACK B5-119 AND BATTERY POWER SUPPLY PER B717 AMM 33 -51. (7556762)
- [SDR DALA2025090906663](https://openairdocs.org/sdr/DALA2025090906663), Sep 2, 2025: BATTERY PACK. INOPERATIVE. EMERGENCEY PATH LIGHTS ROW 1-13 INOP. R & R BATTERY PACK P5-227 PER B717 AMM 33-51 (7556761)
- [SDR DALA2025082606326](https://openairdocs.org/sdr/DALA2025082606326), Aug 21, 2025: SPAR CAP. CRACKED. LEFT WING REAR SPAR LOWER CAP AFT FLANGE CRACKED NEAR XRS = 164. ACCOMPLISH ER/A 627199-14AD REV D (1156482)
- [SDR DALA2025070805070](https://openairdocs.org/sdr/DALA2025070805070), Jul 2, 2025: FUEL SYS. LEAKING. SHIP 9584 C/W ERA 621136-14AD REV A - RH WING / REAR SPAR LOWER CAP / FUEL LEAK. CORRECTIVE ACTION: C/W ERA 621136-14AD REV A (1058308)
- [SDR DALA2025063004850](https://openairdocs.org/sdr/DALA2025063004850), Jun 25, 2025: FUEL SYS. LEAKING. SHIP 9584 PER ERA 621136-14AD WORKING CARD 5720-01103-01B. FUEL LEAK FOUND DURING INSPECTION OF RH WING AFT LOWER SKIN DOUBLER AT XRS=164. CORRECTIVE ACTION: CO
- [SDR DALA2025062604796](https://openairdocs.org/sdr/DALA2025062604796), Jun 25, 2025: SPAR CAP. CRACKED. SHIP 9584 CRACKS FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP AFT LEG. CORRECTIVE ACTION: COMPLIED WITH 627199-14 REV A LH WING REAR SPAR LOWER CAP CR
- [SDR DALA2025062504751](https://openairdocs.org/sdr/DALA2025062504751), Jun 24, 2025: NONE. NONE. ER/A 627199-14AD REV A REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. CORRECTIVE ACTION: C/W ERA 627199.
- [SDR DALA2025060604327](https://openairdocs.org/sdr/DALA2025060604327), May 24, 2025: REPAIR. NOT REPORTED. SHIP 9584 EXISTING REPAIRS FOUND ON RH AFT REAR SPAR FC 5720-01103. REPAIRED PER ER/A 621136-14AD (7125256)
- [SDR DALA2025043003315](https://openairdocs.org/sdr/DALA2025043003315), Apr 29, 2025: REPAIR. NOT REPORTED. -AD- EXISTING REPAIR FOUND, CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURE PRIOR TO FURTHUR FLIGHT REF. FC5720-01103. AMOC 24-160 TO AD 2024-21-01 PARA(G) W/C
- [SDR DALA2025020600922](https://openairdocs.org/sdr/DALA2025020600922), Feb 1, 2025: NONE. NONE. -AD- EXISTING REPAIR FOUND. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURE PRIOR TO FURTHER FLIGHT REF FC5720-01103. AMOC 24-160 TO AD 2024-21-01 PARA(G) W/C 
- [SDR DALA2025012800654](https://openairdocs.org/sdr/DALA2025012800654), Jan 27, 2025: BATTERY PACK. INOPERATIVE. THE EMERGENCY LIGHTS AT ROW 20 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK AT B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. 
- [SDR DALA2025012800655](https://openairdocs.org/sdr/DALA2025012800655), Jan 23, 2025: LENS. DETACHED. THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT LOCATION 600. THE EXIT SIGN COVER FELL OFF. MAINTENANCE RESECURRED THE LENS COVER. OPERATIONAL CHECK WAS NO
- [SDR DALA2024111410952](https://openairdocs.org/sdr/DALA2024111410952), Nov 13, 2024: POWER SUPPLY. INOPERATIVE. THE AFT OVER WING EXIT DOOR EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY (B5-230) AND THE LIGHT OPERATIONALLY CHECKED GOOD 
- [SDR DALA2024111110800](https://openairdocs.org/sdr/DALA2024111110800), Nov 9, 2024: UNKNOWN. UNKNOWN. -AD- EXISTING REPAIRS FOUND. PERFORMED ALL REPAIRS PER PRI 621136-14, REV 13. REPAIR LEAK CHECK WAS GOOD. REPAIRS COMPLETED IAW ER/A 621136-14AD, REV O, SECTION
- [SDR DALA2024111110799](https://openairdocs.org/sdr/DALA2024111110799), Nov 9, 2024: FUEL CELL. LEAKING. -AD- FOUND FUEL SEEPING FROM FWD FLAP CARRIAGE MOUNT AND DOUBLER ON RT WING INBOARD FLAP AT XRS 164. (FC 5720-01103) PERFORMED ALL REPAIRS PER PRI 621136-14, RE
- [SDR DALA2024082708492](https://openairdocs.org/sdr/DALA2024082708492), Aug 26, 2024: LENS. MISSING. AIRCRAFT 9584, EMERGENCY LENS COVER AT 26CDE IS MISSING. CEILING EMERGENCY LIGHT. CORRECTIVE ACTION: INSTALLED EMERGENCY CEILING LENS COVER PER B717 AMM 33-51. 
- [SDR DALA2024082608452](https://openairdocs.org/sdr/DALA2024082608452), Aug 26, 2024: BATTERY. INOPERATIVE. BOTH EMERGENCY LIGHTS IN CABIN ABOVE AFT OVERWING EXITS ARE INOP. CORRECTIVE ACTION: REPLACED BATTERY AT STA 426.
- [SDR DALA2024080107659](https://openairdocs.org/sdr/DALA2024080107659), Jul 31, 2024: BATTERY. NO TEST. FOUND OVERWING EMERGENCY EXIT LIGHTS OVERHEAD EXIT LIGHTS IN ROW 20 TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY FOR ROW 20 LIGHT PER B717 AMM 
- [SDR DALA2024032303707](https://openairdocs.org/sdr/DALA2024032303707), Mar 23, 2024: CYLINDER. FAULTED. SHIP 9584 -ATB/GEAR/DE- FOLLOWING TAKEOFF AND LANDING GEAR RETRACTION, THE CREW RECEIVED A "LEFT MAIN GEAR UNSAFE" MESSAGE. AN EMERGENCY WAS DECLARED, AND THE C
- [SDR DALA2024020101443](https://openairdocs.org/sdr/DALA2024020101443), Jan 31, 2024: PAN. CRACKED. CRACK ON INTERNAL PAN ON UPPER FWD CORNER AT AFT CARGO DOOR. SUMMARY OF NRC 00087: INTERNAL PAN ON UPPER FWD CORNER AT AFT CARGO DOOR WAS REPAIRED PER ERA 61520
- [SDR DALA2024013001357](https://openairdocs.org/sdr/DALA2024013001357), Jan 29, 2024: SKIN. CORRODED. CORROSION ON INNER SKIN NEXT TO HINGE AT FORWARD AIR STAIRWELL DOOR. SUMMARY OF NRC 00127: STAIRWELL DOOR WAS REPLACED PER BOEING 717-200 AMM 52-63-01. (LP #017
- [SDR DALA2024012901229](https://openairdocs.org/sdr/DALA2024012901229), Jan 28, 2024: DOUBLER. CORRODED. CORROSION ON DOUBLER STA=908 BTW LONGERON 29LH TO 29RH AT CARGO COMPARTMENT. SUMMARY OF NRC 00535: CORROSION LEVEL 2. DOUBLER STA=908 BTW LONGERON 29LH TO 29RH 
- [SDR DALA2024012901218](https://openairdocs.org/sdr/DALA2024012901218), Jan 25, 2024: PAN. CRACKED. CRACK ON INTERNAL PAN FWD EDGE BTW BEAM #2 AND BEAM #4 AT FWD CARGO DOOR. SUMMARY OF NRC 00069: INTERNAL PAN FWD EDGE BTW BEAM #2 AND BEAM #4 AT FWD CARGO DOOR 
- [SDR DALA2024011600590](https://openairdocs.org/sdr/DALA2024011600590), Jan 15, 2024: UNKNOWN. UNKNOWN. CRACK INTERCOSTAL AT X=0, BTWEEN STA Y=1002 TO Y=1022, CABIN FLOOR SUPPORT STRUCTURE. SUMMARY OF NRC 00511: TRIMMED OUT INTERCOSTAL AT X=0, BT STA Y=1002 TO STA
- [SDR DALA2024011200537](https://openairdocs.org/sdr/DALA2024011200537), Jan 11, 2024: UNKNOWN. UNKNOWN. SCRATCH ON WEB BTW APROX STA Y199/Y197 AND -X54 AT PAX CABIN. SUMMARY OF NRC 00327: SCRATCH ON WEB BTW APROX STA Y199/Y197 AND -X54 AT PAX CABIN WAS REPAIRED PE
- [SDR DALA2024010900323](https://openairdocs.org/sdr/DALA2024010900323), Jan 7, 2024: UNKNOWN. UNKNOWN. CRACKS ON LOWER SURFACE OF CUSP WEB MEMBRANE RH ON STA Y=655, 674, 890, 694, AND 697 AT CPAX. SUMMARY OF NRC 00316: CRACKS ON LOWER SURFACE OF CUSP WEB MEMBRANE
- [SDR DALA2024010300073](https://openairdocs.org/sdr/DALA2024010300073), Jan 3, 2024: CUSP WEB. UNKNOWN. CRACK ON CUSP WEB LH SIDE BTW STA Y=655 X=49, Y=653 X=57.5, Y=675 X=46, AND Y=717 X=46 AT PAX CABIN. SUMMARY OF NRC 00366: CUSP WEB LH SIDE BTW STA Y=655 X=49, 
- [SDR DALA2024010300072](https://openairdocs.org/sdr/DALA2024010300072), Jan 3, 2024: UNKNOWN. UNKNOWN. CORROSION OUT OF LIMITS ON RH CUP WEB MEMBRANE ON STA Y=527 AND STA Y=608 PER B717-200 SRM 53-00-55-1A PROCEDURE 1. AD. 1 PAR 4. FIG 101. SUMMARY OF NRC 00457: 
- [SDR DALA2024010200013](https://openairdocs.org/sdr/DALA2024010200013), Dec 31, 2023: UNKNOWN. UNKNOWN. CRACK ON INTERCOSTAL (CEILING AREA) BTW SAT 851 AND X=0 AT AFT CARGO. SUMMARY OF NRC 00137: INTERCOSTAL (CEILING AREA) BTW SAT 851 AND X=0 AT AFT CARGO WAS REPA
- [SDR DALA2023062005004](https://openairdocs.org/sdr/DALA2023062005004), Jun 20, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY LIGHTS WERE DISCOVERED TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERIES PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. THE A
- [SDR DALA2023060604554](https://openairdocs.org/sdr/DALA2023060604554), May 29, 2023: UNKNOWN. UNKNOWN. FLAP HINGE ATTACH FITTING INSIDE WING AT XRS 164.00 BOTTOM LUG HORIZONTAL FASTENER HOLES, 3 EA OUTBOARD SIDE - MARKED. COMPLIED WITH ON ERA 6071561-14 AD STEP 3
- [SDR DALA2023060604553](https://openairdocs.org/sdr/DALA2023060604553), May 29, 2023: UNKNOWN. UNKNOWN. 3 EA HOLES MISDRILLED IN SKIN BELOW XRS 140.00 - MARKED. COMPLIED WITH ON ERA 607151-14AD STEP 23. (LP #2790419)
- [SDR DALA2023060604552](https://openairdocs.org/sdr/DALA2023060604552), May 29, 2023: UNKNOWN. UNKNOWN. THREE EA HOLES WITH CRACK INDICATION IN SKIN LAYER, IB EDGE OF LOWER WING SKIN DOUBLER IB OF XRS 164.00. MARKED. COMPLIED WITH ON ERA 607151-14AD STEP 27. (LP #
- [SDR DALA2023021501185](https://openairdocs.org/sdr/DALA2023021501185), Feb 13, 2023: UNKNOWN. UNKNOWN. CORROSION AT LWR FLAP FITTING ATTACH POINTS ON FWD INBD DRIVE FITTING ASSY RH SIDE. REMOVED HINGE FLAP FITTING NONROUTINE CARDS #09 & 01. REMOVED DAMAGE AT HOLE
- [SDR DALA2023011600309](https://openairdocs.org/sdr/DALA2023011600309), Jan 12, 2023: SKIN. DENTED. DENT AFT CARGO DOOR, QTY 2. 1) 12" FROM TOP EDGE, 18" FROM T/E. 2) FWD EDGE IAW B717 SRM 53-01-01 AD 3 COND 1B DENT ORIGINALLY DOCUMENED, INSPECTED, MEASURED BY
- [SDR DALA2023011600310](https://openairdocs.org/sdr/DALA2023011600310), Jan 11, 2023: SKIN. DAMAGED. THE AFT CARGO DOOR HAS SKIN DAMAGED ALONG AFT EDGE OF DOOR. MARKED. REF NRC 74: MAINTENANCE REPLACED THE CARGO DOOR PER B717 AMM 52-31-01. (LP #2577273)
- [SDR DALA2023011000172](https://openairdocs.org/sdr/DALA2023011000172), Jan 8, 2023: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT AT RBL 7 STA 194-200 (C-CHECK N/R CARD 343). REPLACED FLOOR SUPPORT REF B717 DWG 9936534. (LP #2573682)

All 184: https://openairdocs.org/aircraft/N986AT/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/N986AT/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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