# N993AT: 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: 55137
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 21, 2002
- Certificate issued: August 5, 2024
- Expires: August 31, 2031
- Mode S code: ADDDDA
- 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=993AT
- Page: https://openairdocs.org/aircraft/N993AT

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/N993AT/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 N993AT.

## FAA accident and incident reports

None matched to N993AT.

## Service difficulty reports (210, 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 DALA2026090805037](https://openairdocs.org/sdr/DALA2026090805037), Sep 7, 2026: SLAT. DAMAGED. DAMAGE TO LEFT WING SLAT DUE TO BIRD STRIKE. PERFORMED A BIRD STRIKE INSP PER B717 AMM 05-62 FOUND NO OTHER DAMAGE. REPLACED #3 WING SLAT IAW AMDS JOB CARD 2780
- [SDR DALA2026060903438](https://openairdocs.org/sdr/DALA2026060903438), Jun 2, 2026: WING. NO DISCREPANCY. ACFT DUE LT AND RT WING INSPECTIONS AD 2024-21-01. C/W WORKCARDS 5720-01103-01A, AND 5720-01103-01B, FCN'S 95-0557- 8-0032, AND 95-0557-8-0035. OK FOR SVC. (835
- [SDR DALA2026060203339](https://openairdocs.org/sdr/DALA2026060203339), May 30, 2026: SKIN. CRACKED. CRACKS ON FUSELAGE OUTER SKIN, BS 1095 BTW LONGERON 3R AND 4R & BS 1095 BTW LONGERON 2R AND 3R. REPAIRED IAW PRI 634353-14 (1621163) (AIRCRAFT GROUNDED)
- [SDR DALA2026052903260](https://openairdocs.org/sdr/DALA2026052903260), May 28, 2026: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1037 BTW. REPAIRED PER ER/A NO. 634335-14 (1618251) (AIRCRAFT GROUNDED)
- [SDR DALA2026052903258](https://openairdocs.org/sdr/DALA2026052903258), May 28, 2026: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN STA Y= 1022 BTW. REPAIRED PER ER/A 634381 (1616802) (AIRCRAFT GROUNDED)
- [SDR DALA2026052903257](https://openairdocs.org/sdr/DALA2026052903257), May 28, 2026: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN STA Y= 1022 BTW LONG 13RH & 14RH. REPAIRED IAW PRI 634340 (1616686) (AIRCRAFT GROUNDED)
- [SDR DALA2026060203342](https://openairdocs.org/sdr/DALA2026060203342), May 26, 2026: SKIN. DAMAGED. ERA 634353-14 ISSUED FOR REPAIR TO FUSELAGE SKIN AT STA 1152, L2 TO L4. ACCOMPLISH ERA 634353-14 (1616414) (AIRCRAFT GROUNDED)
- [SDR DALA2026052903255](https://openairdocs.org/sdr/DALA2026052903255), May 26, 2026: DOOR FRAME. CORRODED. CORROSION AROUND LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. REPAIRED IAW SRM 51-41-02-0G AND SRM 51-41-05-0G AND PER B717-200 SRM 53-20-15. (1614443) (AIRCRAFT G
- [SDR DALA2026052903253](https://openairdocs.org/sdr/DALA2026052903253), May 26, 2026: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN STA Y=1076 BTW LONG 13LH & 14LH. REPAIR AND PRI 634388-14 (1613658) (AIRCRAFT GROUNDED)
- [SDR DALA2026052903252](https://openairdocs.org/sdr/DALA2026052903252), May 25, 2026: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN STA Y= 1087 BTW LONG 13RH & 14RH. REPAIRED PER ER/A NO. 634338-14 (1612208) (AIRCRAFT GROUNDED)
- [SDR DALA2026052803221](https://openairdocs.org/sdr/DALA2026052803221), May 22, 2026: CUSP WEB. CRACKED. IAW TASK 310-01436-01 STEP 5 AFTER REMOVAL CUSP MEMBRENE CRACK WAS FOUND AT CUSP WEB. FUSELAGE STA 674 LH SIDE. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-
- [SDR DALA2026052903261](https://openairdocs.org/sdr/DALA2026052903261), May 21, 2026: SKIN. CRACKED. CRACK AND WEAR EXTERNAL SKIN ON AFT CARGO DOOR CUTOUT AFT EDGE BTW LONG 24RH TO LONG 26RH AT LOWER FUSELAGE SECTION. REPAIRED PER B717-200 SRM 53-20-15 (1605105
- [SDR DALA2025120808961](https://openairdocs.org/sdr/DALA2025120808961), Nov 30, 2025: UNKNOWN. ODOR. FWD FAS SAYS THAT GOT A GOOD WIFT OF THE DIRTY SOCK SMELL ON CLIMB OUT. NO OTHER COMPLAINTS ON ACFT. FUME WAS SHORT TERM MAYBE A MINUTE OR TWO. TROUBLESHOT ODOR
- [SDR DALA2025120508917](https://openairdocs.org/sdr/DALA2025120508917), Nov 30, 2025: PIN. BROKEN. ATO- APPROX 80KTS DUE TO PREDICTIVE WINDSHEAR WARNING. FOUND COAXIAL CABLE PIN BROKEN. REPLACED SAME. OPS NORMAL.(7952152)
- [SDR DALA2025091606813](https://openairdocs.org/sdr/DALA2025091606813), Sep 6, 2025: LANYARD. UNSECURE. DOOR 1R EMERGENCY SLIDE ARMING BAR DETACHED AND BROKEN. MEM DELTA MX NOTIFIED. REINSTALLED GIRT BAR LANYARD ON 1R EMERGENCY SLIDE IAW AMM 25-61 (7587364)
- [SDR DALA2025030601744](https://openairdocs.org/sdr/DALA2025030601744), Mar 5, 2025: BATTERY PACK. NO TEST. THE EMERGENCY LIGHT SERVICE CHECK FOUND THE LIGHTED SIGNS ABOVE THE AFT OVERWING EXITS ON LEFT & RIGHT SIDES TO BE INOPERATIVE. MAINTENANCE TROUBLESHOT IN REF W
- [SDR DALA2025021801200](https://openairdocs.org/sdr/DALA2025021801200), Feb 13, 2025: OVEN. CONTAMINATED. SHIP 9538 -DIV/SMK/DE- THE FLIGHT CREW NOTED SMOKE IN COCKPIT WHILE ENROUTE TO MCI. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT WAS DIVERTED TO A NORMAL SAFE LA
- [SDR DALA2024121811803](https://openairdocs.org/sdr/DALA2024121811803), Dec 18, 2024: UNION. LEAKING. SHIP 9538 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC FOLLOWING THE RIGHT HYDRAULIC SYSTEM SHOWING A LOSS IN QUANTITY. THE QRH WAS COMPLIED WITH, B
- [SDR DALA2024120911541](https://openairdocs.org/sdr/DALA2024120911541), Dec 8, 2024: BATTERY PACK. INOPERATIVE. DURING THE SERVICE CHECK THE FWD OVERWING EMERGENCY EXIT UPPER DOOR LIGHTS ON BOTH LT & RT SIDE WERE FOUND NOT ILLUMINATED. MAINTENANCE REPLACED THE B5-121 BATT
- [SDR DALA2024120911531](https://openairdocs.org/sdr/DALA2024120911531), Nov 12, 2024: NONE. NONE. -AD- ACCOMPLISH ER/A 622306-14AD SECTION I B717 FUSELAGE STA 1178.558 ALTERNATIVE INSPECTION FOR PREVIOUS REPAIR. ACCOMPLISH ER/A 622306-14AD SECTION I FOR THE 
- [SDR DALA2024062706579](https://openairdocs.org/sdr/DALA2024062706579), Jun 25, 2024: HPC. DAMAGED. SHIP 9538 -ATO- ABORTED TAKEOFF AT APPROXIMATELY 80 KNOTS DUE TO SUSPECTED RIGHT ENGINE SUSPECTED COMPRESSOR STALL. CORRECTIVE ACTION: PERFORMED BORESCOPE INSPE
- [SDR DALA2024052105381](https://openairdocs.org/sdr/DALA2024052105381), May 20, 2024: POWER SUPPLY. INOPERATIVE. THE AFT ACCESORY COMPARTMENT EMERGENCY LIGHTS ARE INOPERATIVE. THE EMERGENCY LIGHT BATTERY POWER SUPPLY WAS REPLACED PER B717 AMM 33-51-03. OPERATIONAL TESTS AR
- [SDR DALA2024052105376](https://openairdocs.org/sdr/DALA2024052105376), May 19, 2024: RELEASE CABLE. MISROUTED. IMPROPER ROUTING OF MANUAL RELEASE CABLE FOR SLIDE AT FORWARD SERVICE DOOR. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIAN
- [SDR DALA2024052005345](https://openairdocs.org/sdr/DALA2024052005345), May 18, 2024: PAN. CRACKED. CRACK ON PAN LOWER EDGE INTERNAL STRUCTURE BTW STA 403 TO 413 FWD CARGO DOOR. SUMMARY OF NRC 00212: INNER AND OUTER PAN ON LOWER EDGE INTERNAL STRUCTURE BTW STA
- [SDR DALA2024052005342](https://openairdocs.org/sdr/DALA2024052005342), May 17, 2024: SLIDE. DAMAGED. DURING FWD PASSENGER SLIDE DOOR COVER INSTALLATION, THE SLIDE PACKAGE WAS FOUND UNSAFE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT
- [SDR DALA2024052005340](https://openairdocs.org/sdr/DALA2024052005340), May 17, 2024: SLIDE. DAMAGED. DURING FWD PASSENGER SLIDE DOOR COVER INSTALLATION, THE SLIDE PACKAGE WAS FOUND UNSAFE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT
- [SDR DALA2024051705296](https://openairdocs.org/sdr/DALA2024051705296), May 16, 2024: STRAP. CORRODED. CORROSION ON WEB STRAP BTW STA Y=200/208 AND LONGERON 18L. (PAX CAB). SUMMARY OF NRC 00409: CORROSION LEVEL 2. WEB STRAP BTW STA Y=200/208 AND LONGERON 18L WAS 
- [SDR DALA2024051705294](https://openairdocs.org/sdr/DALA2024051705294), May 16, 2024: HINGE. EXCESS PLAY. FREEPLAY ON JOINT BTW FLAP AND FLAP OUTBD HINGE AT LH WING. LT WING FLAP OUTBD HINGE WAS REPAIRED IN ACCORDANCE WITH PRI 617504-14 REV 2 AND ER/A 617504-14 REV 
- [SDR DALA2024051605253](https://openairdocs.org/sdr/DALA2024051605253), May 16, 2024: STRUCTURE. CORRODED. CORROSION WAS FOUND ON HSTB HOLE #27 RH. SUMMARY OF NRC 00650: RH HORIZONTAL STABILIZER BARREL NUT HOLE #27 WAS REPAIRED IN ACCORDANCE WITH ER/A 617762-14 REV O
- [SDR DALA2024051505224](https://openairdocs.org/sdr/DALA2024051505224), May 15, 2024: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL BTW STA Y=636 AND X=0 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00679: CRACK ON INTERCOSTAL BTW STA Y=636 AND X=0 AT FWD CARGO COMPARTMENT W
- [SDR DALA2024051505223](https://openairdocs.org/sdr/DALA2024051505223), May 14, 2024: VANE. DENTED. DENTS ON AFT MOVEABLE VANE LOWER SKIN AT RIGHT WING. SUMMARY OF NRC 00238: AFT MOVEABLE VANE LOWER SKIN AT RIGHT WING WAS REPAIRED PER ER/A 617597-14 REV ORIGIN
- [SDR DALA2024051505221](https://openairdocs.org/sdr/DALA2024051505221), May 14, 2024: DOUBLER. CORRODED. CORROSION ON INTERNAL DOUBLER BTW STA Y 617-636 AND LONG L27L TO L28L AT FWD CARGO COMPARTEMENT. SUMMARY OF NRC 00631: CORROSION LEVEL 2. CORROSION ON INTERNAL 
- [SDR DALA2024051405175](https://openairdocs.org/sdr/DALA2024051405175), May 13, 2024: SUPPORT ANGLE. CRACKED. CRACKS (2 EA) ON ANGLE STRUCTURE SUPPORT BULKHEAD BTW LONGERON 5L AND 6L ALSO 7L STA=Y 1022 AT AFT LAVATORY ENGINE PYLON AREA. SUMMARY OF NRC 00400: CRACK ON AN
- [SDR DALA2024051405172](https://openairdocs.org/sdr/DALA2024051405172), May 12, 2024: SCUFF PLATE. CRACKED. CRACK ON AFT SCUFF PLATE AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0002: SCUFF PLATE AT AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 542149-14TR REV B, SECTION I:
- [SDR DALA2024051405171](https://openairdocs.org/sdr/DALA2024051405171), May 10, 2024: PAN. CRACKED. CRACKS ON PAN FWD EDGE AND AFT EDGE BETWEEN BEAM #2 AND #3 AT AFT CARGO DOOR. SUMMARY OF NRC 00366: AFT CARGO DOOR ASSY WAS REMOVED PER AMDS 5231-4002, WAS REPL
- [SDR DALA2024051305131](https://openairdocs.org/sdr/DALA2024051305131), May 9, 2024: FRAME. CORRODED. CORROSION ON PREVIOUS REPAIR DOUBLER ON FRAME Y=870 BTW LONGERONS 29L AND 29R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00299: CORROSION LEVEL 2. PREVIOUS REPAIR
- [SDR DALA2024050905041](https://openairdocs.org/sdr/DALA2024050905041), May 8, 2024: ANGLE. CORRODED. CORROSION ON CUSP ANGLE AT FORWARD GALLEY SERVICE DOOR JAMB STA Y=157-200. SUMMARY OF NRC 00345: CORROSION LEVEL 2. CUSP ANGLE AT FORWARD GALLEY SERVICE DOOR JA
- [SDR DALA2024050805022](https://openairdocs.org/sdr/DALA2024050805022), May 7, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BTW STA Y 157 TO 200 AND X=-43 AT PAX CABIN. SUMMARY OF NRC 00407: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y 157 TO 200 AND X=-43 AT
- [SDR DALA2024050704974](https://openairdocs.org/sdr/DALA2024050704974), May 7, 2024: FLOORBEAM. CORRODED. CORROSION ON FLOOR SUPPORT STA 180 FROM X=-7 TO X=-44 AT PAX CABIN. SUMMARY OF NRC 00415: CORROSION LEVEL 2. FLOOR SUPPORT STA 180 FROM X=-7 TO X=-44 AT PAX CAB
- [SDR DALA2024050604954](https://openairdocs.org/sdr/DALA2024050604954), May 3, 2024: FRAME. CRACKED. CRACK ON FRAME STA=Y 1178 APPROX BTW LONGERON 1L AND 2L AT AFT ACCESORY COMPARTMENT AREA. SUMMARY OF NRC 00401: FRAME STA=Y 1178 APPROX BTW LONGERON 1L AND 2L A
- [SDR DALA2024050304920](https://openairdocs.org/sdr/DALA2024050304920), May 2, 2024: SKIN. CRACKED. CRACK INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW AREA. CPIL. SUMMARY OF NRC 00524: FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WIND
- [SDR DALA2024050204890](https://openairdocs.org/sdr/DALA2024050204890), May 1, 2024: BULKHEAD WEB. CRACKED. CRACKED BULKHEAD WEB STA Y=218, X=-8 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00647: BULKHEAD WEB STA Y=218, X=-8 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717
- [SDR DALA2024050204887](https://openairdocs.org/sdr/DALA2024050204887), Apr 30, 2024: CUSP WEB. CORRODED. CORROSION ON RH CUSP WEB UPPER AND LOWER BTW STA 217-237 AT PAX CAB. SUMMARY OF NRC 00346: CORROSION LEVEL 2. RH CUSP WEB UPPER AND LOWER BTW STA 217-237 AT PAX
- [SDR DALA2024043004795](https://openairdocs.org/sdr/DALA2024043004795), Apr 27, 2024: CUSP WEB. CORRODED. CORROSION ON LH CUSP WEB ALSO WITH OIL SCAN ON THE SAME CUSP WEB BTW STA 889 TO STA 908 X=58 AT PAX CABIN. SUMMARY OF NRC 00396: CORROSION LEVEL 2. LH CUSP WEB 
- [SDR DALA2024043004792](https://openairdocs.org/sdr/DALA2024043004792), Apr 27, 2024: SKIN. DAMAGED. ELONGATED HOLE ON VERTICAL STABILIZER LEADING EDGE LEFT SIDE, JUST ON THE CORNER WAS FOUND STA ZFS=52.267 IN REF NRC 0525. SUMMARY OF NRC 00611: HOLE ON VERTICA
- [SDR DALA2024042304669](https://openairdocs.org/sdr/DALA2024042304669), Apr 23, 2024: CUSP WEB. CRACKED. CRACK LH CUSP WEB STA 657 TO 663 X=55 AT PAX CABIN. SUMMARY OF NRC 00394: CRACK LH CUSP WEB STA 657 TO 663 X=55 AT PAX CABIN WAS REPAIRED PER B717 SRM-53-00-55-
- [SDR DALA2024042304665](https://openairdocs.org/sdr/DALA2024042304665), Apr 22, 2024: LONGERON. CRACKED. CRACKS ON LONGERON (3 EA) 5L, 5R, AND 17L STA=Y 1022 AT AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD AREA. SUMMARY OF NRC 0245: LONGERON (2 EA) 5L & 5R AT AFT LAV
- [SDR DALA2024041904571](https://openairdocs.org/sdr/DALA2024041904571), Apr 19, 2024: MEMBRANE. CORRODED. CORROSION ON LEFT MEMBRANE STA 200 TO 207 X=54 AT PAX CABIN IN REFERENCE NRC 00391. SUMMARY OF NRC 00591: CORROSION LEVEL 2. LEFT MEMBRANE STA 200 TO 207 X=54 A
- [SDR DALA2024041904567](https://openairdocs.org/sdr/DALA2024041904567), Apr 18, 2024: CUSP WEB. CRACKED. CRACK LH CUSP WEB STA 606 X=59 AT PAX CABIN PAX. SUMMARY OF NRC 00393: CRACK LH CUSP WEB STA 606 X=59 AT PAX CABIN, WAS REPAIRED PER B717 SRM-53-00-55-2R-4. (LP
- [SDR DALA2024041504424](https://openairdocs.org/sdr/DALA2024041504424), Apr 12, 2024: BULKHEAD WEB. CRACKED. CRACKED BULKHEAD WEB SYA Y=218, X=-8 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00283: BULKHEAD WEB STA Y=218, X=-8 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717

All 210: https://openairdocs.org/aircraft/N993AT/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/N993AT/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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