# N994AT: 2002 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [Rolls-Royce BR-700 series](https://openairdocs.org/engine/rolls-royce-br-700-series) (registry code 54565)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55138
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 11, 2002
- Certificate issued: December 17, 2024
- Expires: December 31, 2031
- Mode S code: ADE191
- 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=994AT
- Page: https://openairdocs.org/aircraft/N994AT

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 Rolls-Royce 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 (Rolls-Royce 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/N994AT/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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ERA09LA488](https://openairdocs.org/ntsb/ERA09LA488), Aug 27, 2009: Boeing 717-200 (N994AT), Inverness, FL, no damage. Probable cause: The flight crew's encounter with convective turbulence. Contributing to the accident was the failure of the operator's dispatch department to provide the flightcrew with current adverse weather…

## 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.

- [Accident 20090827049429A](https://openairdocs.org/incident/20090827049429A), Aug 27, 2009: Boeing 717-200 (N994AT), Inverness, FL, No damage. Airtran airways flight 163, a Boeing 717-200, N994AT, encountered turbulence while in climb near Inverness, Florida, during which one flight attendant…

## Service difficulty reports (192, 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 DALA2026092105262](https://openairdocs.org/sdr/DALA2026092105262), Sep 21, 2026: ANNUNCIATOR. INOPERATIVE. R1 DOOR WARNING ANNUNCIATION INOP. T/S PER B717 FRMFIM 52-70-00-810-809, PERFORMED PSEU BITE TEST, TEST PASSED, NO DEFECTS NOTED. PSEU SENSOR READOUT OK. (18237
- [SDR DALA2026082604840](https://openairdocs.org/sdr/DALA2026082604840), Aug 26, 2026: SKIN. CRACKED. CRACKED ON EXTERNAL FUSELAGE SKIN ON BS 1086 BTW LONG 13L AND 14L, COMPLIED WITH ER/A 636457-14. (1777167) (AIRCRAFT GROUNDED).
- [SDR DALA2026082604839](https://openairdocs.org/sdr/DALA2026082604839), Aug 26, 2026: SKIN. CRACKED. CRACKS ON EXTERNAL FUSELAGE SKIN ON BS 1076 BTW LONG 13L AND 14L, COMPLIED WITH ER/A 636463-14. (1777154) (AIRCRAFT GROUNDED).
- [SDR DALA2026082604842](https://openairdocs.org/sdr/DALA2026082604842), Aug 25, 2026: SKIN. CRACKED. CRACKS WERE FOUND AFFECTING THE FUSELAGE SKIN AT APPROXIMATELY BS 1087.060, BTW LONGERONS 13 & 14, COMPLIED WITH ER/A 636457-14. (1776557) (AIRCRAFT GROUNDED).
- [SDR DALA2026082604841](https://openairdocs.org/sdr/DALA2026082604841), Aug 25, 2026: SKIN. CRACKED. CRACKS WERE FOUND AFFECTING THE FUSELAGE SKIN AT APPROX BS 1076, BTW LONGERONS 13L & 14L, COMPLIED WITH ER/A 636463-14. (1776432) (AIRCRAFT GROUNDED).
- [SDR DALA2026082404792](https://openairdocs.org/sdr/DALA2026082404792), Aug 23, 2026: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN STA Y= 1037 BTW LONG 13L AND 14L, COMPLIED WITH ER/A 636303-14. (1773110) (AIRCRAFT GROUNDED).
- [SDR DALA2026082404790](https://openairdocs.org/sdr/DALA2026082404790), Aug 23, 2026: LANYARD. TORN. TORN LANYARD OF R1 DOOR EMERGENCY SLIDE. R & R LANYARD OF R1 DOOR EMERGENCY SLIDE IAW AIPC 25-61- 03-01. (1771710) (AIRCRAFT GROUNDED).
- [SDR DALA2026082404794](https://openairdocs.org/sdr/DALA2026082404794), Aug 21, 2026: SKIN. CRACKED. CRACKS WERE FOUND AFFECTING THE FUSELAGE SKIN AT BS Y=1037, BETWEEN THE L-13L AND L-14L, COMPLIED WITH ER/A 636303-14. (1772642) (AIRCRAFT GROUNDED).
- [SDR DALA2026082404789](https://openairdocs.org/sdr/DALA2026082404789), Aug 21, 2026: DOOR FRAME. CRACKED. CRACK ON LOWER JAMB AT Y=391 APPROX. ON FWD CARGO DOOR CUTOUT, R & R LOWER JAMB IAW SRM 51-41-02-0G AND SRM 51-41-05-0G. (1769464) (AIRCRAFT GROUNDED).
- [SDR DALA2026082104769](https://openairdocs.org/sdr/DALA2026082104769), Aug 20, 2026: FRAME. CRACKED. CRACK ON CAP STA Y=1178 CANT AND LONG 17L AT AFT FUSELAGE COMPARTMENT, COMPLIED WITH ER/A 636312-14. (1767796) (AIRCRAFT GROUNDED).
- [SDR DALA2026082004758](https://openairdocs.org/sdr/DALA2026082004758), Aug 20, 2026: CHANNEL. CRACKED. CRACKED CORNER OF AFT ZEE CHANNELS Y=799, -X=10.5 AT THE RT MLG INBD DOOR, COMPLIED WITH ER/A 619191-14TR. (1766358) (AIRCRAFT GROUNDED).
- [SDR DALA2026082004756](https://openairdocs.org/sdr/DALA2026082004756), Aug 19, 2026: SCUFF PLATE. CORRODED. FOUND CORROSION LVL 2 ON ANGLE (2EAS) AT FWD CARGO SCUFF PLATE, R & R THE SCUFF PLATE IAW SRM 53-20- 15-2R. (1765931) (AIRCRAFT GROUNDED).
- [SDR DALA2026081704699](https://openairdocs.org/sdr/DALA2026081704699), Aug 16, 2026: FERRULE. CRACKED. CRACK AND MISSING FERRULES ON CARGO COMPARTMENT FLOOR PANEL, COMPLIED WITH ER/A 591778-14TR. (1759040) (AIRCRAFT GROUNDED).
- [SDR DALA2026081704698](https://openairdocs.org/sdr/DALA2026081704698), Aug 16, 2026: FLOOR PANEL. CRACKED. CRACKED FLOOR PANEL 121RF ON FWD CARGO COMPARTMENT, CORRECTIVE ACTION: COMPLIED WITH ER/A 00-591778. (1759039) (AIRCRAFT GROUNDED).
- [SDR DALA2026081704696](https://openairdocs.org/sdr/DALA2026081704696), Aug 16, 2026: VANE. DEBONDED. DISBOND WAS FOUND OF 6.500IN X 3.500IN (LENGTH / WIDTH) ON RT FWD MOVABLE FLAP VANE AT 20IN OF IB AND 5IN TE, RT FWD MOVABLE FLAP VANE WAS REPAIRED IAW SRM 51-7
- [SDR DALA2025092406976](https://openairdocs.org/sdr/DALA2025092406976), Sep 23, 2025: LIMITER. DAMAGED. ON WAKEUP FOUND SPEED TAPE ON RH VORTILON. DAMAGE WITHIN LIMITER PER EAA 570743-14MA REV B APPLIED TEMP REPAIR. WILL NEED PERMINENT REPAIR WITHIN 100 FLIGHT HOU
- [SDR DALA2024112611222](https://openairdocs.org/sdr/DALA2024112611222), Nov 22, 2024: PAN. CRACKED. CRACK ON FWD INNER PAN BTW STA 954 BEAM 3 APPROX AT AFT CARGO DOOR. SUMMARY OF NRC 00086: AFT CARGO DOOR WAS REPLACED WITH A SERVICEABLE AFT CARGO DOOR AND PART
- [SDR DALA2024112211134](https://openairdocs.org/sdr/DALA2024112211134), Nov 22, 2024: PAN. CRACKED. CRACK ON INNER PAN FWD EDGE IN BEAM #5 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00325: INNER PAN FWD EDGE IN BEAM #5 AT AFT CARGO COMPARTMENT DOOR WAS REPA
- [SDR DALA2024111911024](https://openairdocs.org/sdr/DALA2024111911024), Nov 15, 2024: SKIN. CRACKED. CRACK ON FUS SKIN BTW STA 1037 AND 1053 LONGERON 15R. SUMMARY OF NRC 0053: FUS SKIN BTW STA 1037 AND 1053 LONGERON 15R WAS REPAIRED PER ER/A 621624-14 REV ORIGI
- [SDR DALA2024111210889](https://openairdocs.org/sdr/DALA2024111210889), Nov 12, 2024: DOOR FRAME. CORRODED. CORROSION ON DOOR JAM BTW STA Y-954 TO 994 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00076: CORROSION LEVEL 2. CORROSION ON DOOR JAM BTW STA Y-954 TO 994 AT AFT C
- [SDR DALA2024111210886](https://openairdocs.org/sdr/DALA2024111210886), Nov 11, 2024: VANE. DENTED. DENTS: 2, 3, 4, 5, AND 6 BTW XF89 AND XF95 (10 TO 13.5 INCHES FROM T.E.) ON RH AFT MOVABLE FLAP VANE WERE FOUND OUT OF LIMITS BY DISTANCE BTWN OTHER DAMAGES. SU
- [SDR DALA2024111110805](https://openairdocs.org/sdr/DALA2024111110805), Nov 10, 2024: ACCESS PANEL. CORRODED. CORROSION ON ACCESS PANEL 5971074 -1 BTW STA Y=636 TO STA Y=655 L29L TO L29R AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00616: CORROSION LEVEL 2. ACCESS PANEL 597
- [SDR DALA2024111110804](https://openairdocs.org/sdr/DALA2024111110804), Nov 10, 2024: DOUBLER. CORRODED. CORROSION WAS FOUND ON DOUBLER AT E/E COMPARTMENT ON INTERNAL FUSELAGE SKIN PANEL STA Y=215 TO STA Y=221 BTW LONGERON 28R AND 29R. SUMMARY OF NRC 00626: CORROSI
- [SDR DALA2024111110803](https://openairdocs.org/sdr/DALA2024111110803), Nov 9, 2024: VANE. DENTED. DENTS OUT OF LIMITS: 8, 12, 19, 22, AND 24 BTW STA XF95 AND XF103 (4 TO 7 INCHES FROM T.E.) ON UPPER SURFACE AT LH AFT MOVABLE VANE AT LH WING. SUMMARY OF NRC 0
- [SDR DALA2024111110802](https://openairdocs.org/sdr/DALA2024111110802), Nov 9, 2024: VANE. DENTED. DENT #1 (1EA) OUT OF LIMITS UPPER SURFACE RH FWD MOVEABLE FLAP VANE. DISTANCE TO AFT EDGE 6.650, DISTANCE OF OUTER EDGE 34.900 RH WING. SUMMARY OF NRC 00620: ON
- [SDR DALA2024110810727](https://openairdocs.org/sdr/DALA2024110810727), Nov 8, 2024: SKIN. GOUGED. GOUGE ON EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE. SUMMARY OF NRC 00092: EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE WAS REPAIRED PER
- [SDR DALA2024110410591](https://openairdocs.org/sdr/DALA2024110410591), Nov 4, 2024: HINGE. WORN. WEAR ON DOBLER AND FLIGHT ATTENDANT SEAT HINGES OF AFT CABIN BULKHEAD VENTRAL DOOR. AND WEAR ON UPPER / LWR SIDE FITTING (7 EA) 0F AFT CABIN BULKHEAD VENTRAL DO
- [SDR DALA2024110410590](https://openairdocs.org/sdr/DALA2024110410590), Nov 3, 2024: SKIN. GOUGED. GOUGE ON EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE. SUMMARY OF NRC 00092: EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE WAS REPAIRED PER
- [SDR DALA2024110410589](https://openairdocs.org/sdr/DALA2024110410589), Nov 1, 2024: FRAME. CRACKED. CRACK ON MAIN FRAME BTW STA Y=1037 AND L17L AT AFT CABIN PASSENGER. SUMMARY OF NRC 00433: MAIN FRAME BTW STA Y=1037 AND L17L AT AFT CABIN PASSENGER WAS REPAIRED
- [SDR DALA2024110110567](https://openairdocs.org/sdr/DALA2024110110567), Oct 31, 2024: WEB. CRACKED. CRACK ON WEB BTW STA Y=674 AND -X=45 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00380: WEB BTW STA Y=674 AND -X=45 AT PASSENGER CABIN STRUCTURE WAS REPAIRED P
- [SDR DALA2024110110566](https://openairdocs.org/sdr/DALA2024110110566), Oct 31, 2024: LONGERON. CRACKED. CRACK ON LONGERON BTW STA Y=1022 AND L6L AT AFT CABIN PASSENGER. SUMMARY OF NRC 00434: LONGERON BTW STA Y=1022 AND L6L AT AFT CABIN PASSENGER WAS REPAIRED PER B
- [SDR DALA2024103110527](https://openairdocs.org/sdr/DALA2024103110527), Oct 30, 2024: PAN. CRACKED. CRACK WAS FOUND ON INNER PAN AFT EDGE BTW BEAM 1 AND BEAM 2 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00486: INNER PAN AFT EDGE BTW BEAM 1 AND BEAM 2 AT AFT
- [SDR DALA2024103110526](https://openairdocs.org/sdr/DALA2024103110526), Oct 30, 2024: SKIN. CRACKED. CRACK ON SKIN ON CUTOUT OF RH SLIDING WINDOW AT COCKPIT (UPPER AFT CORNER). SUMMARY OF NRC 00355: SKIN ON CUTOUT OF RH SLIDING WINDOW AT COCKPIT (UPPER AFT CORN
- [SDR DALA2024103010504](https://openairdocs.org/sdr/DALA2024103010504), Oct 29, 2024: WEB. CRACKED. CRACKED WEB BTW STA Y=696 AND X=45 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00432: WEB BTW STA Y=696 AND X=45 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER 
- [SDR DALA2024103010503](https://openairdocs.org/sdr/DALA2024103010503), Oct 29, 2024: BEAM. CRACKED. CRACK ON BEAM #1 AFT SECTION AT FWD PASSENGER DOOR. SUMMARY OF NRC 00266: BEAM #1 AFT SECTION AT FWD PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PR
- [SDR DALA2024103010499](https://openairdocs.org/sdr/DALA2024103010499), Oct 25, 2024: WEB. CRACKED. CRACK ON WEB BTW STA Y=674 AND X=45 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00378: WEB BTW STA Y=674 AND X=45 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER
- [SDR DALA2024031203222](https://openairdocs.org/sdr/DALA2024031203222), Mar 8, 2024: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL LH STA Y=1224 CANT 12 O'CLOCK AT AFT ACCESORY COMPARMENT. SUMMARY OF NRC 00078: INTERCOSTAL LH STA Y=1224 CANT 12 O'CLOCK AT AFT ACCESSORY 
- [SDR DALA2024030503008](https://openairdocs.org/sdr/DALA2024030503008), Mar 5, 2024: FRAME. CRACKED. CRACK ON CLIP FRAME STA 1116 BTW LONG 15RH AND 16 RH AT AFT ACCESSORY COMPARMENT. SUMMARY OF NRC 00087: CLIP FRAME STA 1116 BTW LONG 15RH AND 16 RH AT AFT ACCES
- [SDR DALA2024030503007](https://openairdocs.org/sdr/DALA2024030503007), Mar 5, 2024: FRAME. CRACKED. CRACK ON CLIP FRAME STA 1116 BTW LONG 15LH AND 16LH AT AFT ACCESSORY COMPARMENT. SUMMARY OF NRC 00084: CLIP FRAME STA 1116 BTW LONG 15LH AND 16LH AT AFT ACCESSO
- [SDR DALA2023120810062](https://openairdocs.org/sdr/DALA2023120810062), Dec 7, 2023: UNKNOWN. UNKNOWN. RAMP REPORTS DENT ON LOWER LEFT CORNER OF L1 DOOR OUTER SKIN. INSPECTED IAW B717 SRM 53-01-01-1A PROC 3, DENT MEASURES 2 X 0.125 X 0.342. DENT IS OUT OF LIMITS 
- [SDR DALA2023090507199](https://openairdocs.org/sdr/DALA2023090507199), Sep 4, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT JUST AFT OF GALLEY. MAINTENANCE INSTALLED THE EMERGENCY EXIT SIGN COVER BETWEEN ROW 1 SEATS REF B717 AIPC 3
- [SDR DALA2023022201328](https://openairdocs.org/sdr/DALA2023022201328), Dec 2, 2022: NONE. NONE. PDA. LH WING SKIN ASSY STA XFS 70.812-196.236 MISSING. FWD TO MON PER ER/A 604219-14 REV ORIGINAL. C/W SECTION 1. PERMANENT REPAIR TO BE ACCOMPLISHED IN 90 DAYS
- [SDR DALA2022021500948](https://openairdocs.org/sdr/DALA2022021500948), Feb 11, 2022: NONE. NONE. LH VERTICAL STAB LE, CRACK INDICATION IN 4TH HOLE UP FROM SLICE AT STA ZFS 52.267. FOUND DURING OPEN HOLE INSPECTION REF AMDS 5530-01048-02-ET STEP 8 AND AD 201
- [SDR DALA2022021500947](https://openairdocs.org/sdr/DALA2022021500947), Feb 9, 2022: NONE. NONE. TAILCONE EMERGENCY RELEASE; LEFT LOWER LATCH LEVER CABLE IS FRAYED AT UPPER PULLY AREA. -M- SUMMARY SEE NRC 001-0317:5353-2001/001 00453: REPLACED, RIGGED, AND 
- [SDR DALA2022021500946](https://openairdocs.org/sdr/DALA2022021500946), Feb 9, 2022: NONE. NONE. TAILCONE R/H SIDE LATCH LEVER REQUIRES RIG ADJUSTMENT TO TOP OF SLOT PER B717 AMM 53-52-01 830-802 STEP E.1.AG. THIS COULD PREVENT PROPER OPERATION OF THE ESCAP
- [SDR DALA2019091205278](https://openairdocs.org/sdr/DALA2019091205278), Sep 11, 2019: DOOR FRAME. CORRODED. AFT CARGO LOWER DOOR JAMB CORRODED (MARKED). NRC 001-0302:5231-2002/001 00013: REPAIRED REF SRM 53-20-15-2R PROC 7. (LP #1266353)
- [SDR DALA2018112706854](https://openairdocs.org/sdr/DALA2018112706854), Nov 26, 2018: TRANSCEIVER. MALFUNCTIONED. SHIP 9539 - ATO - AT 105 KNOTS DUE TO PREDICTIVE WINDSHEAR WARNING AT 95-100KNOTS. SUSPECT A FALSE WARNING AS OTHER DEPARTURES AND ARRIVALS REPORTED GOOD FLIGHT
- [SDR DALA2018111906671](https://openairdocs.org/sdr/DALA2018111906671), Nov 19, 2018: BATTERY PACK. INOPERATIVE. DURING THE SERVICE CHECK, MAINTENANCE FOUND THE AFT LEFT LOWER EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY FOR THE AFT LEFT LOWER EMER
- [SDR DALA2017111508130](https://openairdocs.org/sdr/DALA2017111508130), Nov 14, 2017: LONGERON. CRACKED. CRACKED LONGERON 16L, BS 1022. THE LONGERON WAS REPAIRED IAW ER/A 562376-14, REV ORIGINAL, AND ETI-17-17-223, REV 3.
- [SDR DALA2017111408092](https://openairdocs.org/sdr/DALA2017111408092), Nov 14, 2017: ANGLE. CORRODED. CORROSION ON RT CUSP ANGLE BELOW OF R1 DOOR JAMB BTW Y=168-207 AT PAX CABIN. CORROSION LEVEL 2. RT CUSP ANGLE BELOW OF R1 DOOR JAMB BTW Y=168-207 AT PAX CABIN W

All 192: https://openairdocs.org/aircraft/N994AT/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/N994AT/stcs.md

## Related

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

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