# N893AT: 2004 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: 55045
- Year built: 2004
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 13, 2004
- Certificate issued: August 28, 2024
- Expires: August 31, 2031
- Mode S code: AC508B
- 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=893AT
- Page: https://openairdocs.org/aircraft/N893AT

From the FAA registry file of October 22, 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/N893AT/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 N893AT.

## FAA accident and incident reports

None matched to N893AT.

## Service difficulty reports (171, 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 DALA2026101605700](https://openairdocs.org/sdr/DALA2026101605700), Oct 15, 2026: LANYARD. UNSECURE. WIRE HANGING OFF GIRT BAR R1 SERVICE DOOR, REINSTALLED 1R DOOR SLIDE LANYARD ASSY PER AMM 25-61. (9539936) (AIRCRAFT GROUNDED).
- [SDR DALA2026091405131](https://openairdocs.org/sdr/DALA2026091405131), Sep 12, 2026: LIGHT. INOPERATIVE. FWD UPPER EMERGENCY EXIT LIGHT INOP. REPAIRED PER B717 AMM 33-51. (9539800) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026050502828](https://openairdocs.org/sdr/DALA2026050502828), Apr 30, 2026: DOOR FRAME. GROUND DAMAGE. BELT LOADER DAMAGE TO AFT CARGO DOOR JAM FWD EDGE. REPAIRED DOOR JAM SEAL DEPRESSOR ON AFT CARGON FORWARD CARGO DOOR JAM IAW B717 SRM 53-20-15 (1571106) (AIRCRA
- [SDR DALA2026050502817](https://openairdocs.org/sdr/DALA2026050502817), Apr 30, 2026: SKIN. GROUND DAMAGE. BELT LOADER DMG TO AFT CARGO DOOR JAMB, AFT EDGE. CORRECTIVE ACTION: REPAIRED PER PRI 634141-14. (1571522) (AIRCRAFT GROUNDED)
- [SDR DALA2026020900919](https://openairdocs.org/sdr/DALA2026020900919), Feb 2, 2026: FMU. FAULTED. ON TAKEOFF AROUND 700 - 1000 FT, HEARD A BANG AND RECEIVED LT ENG COMP STALL MESSAGE. MSG CLEARED 30 SECONDS LATER, RAN QRH AND ALL ENGINE INDICATIONS APPEARED 
- [SDR DALA2026012700606](https://openairdocs.org/sdr/DALA2026012700606), Jan 24, 2026: COMPRESSOR. STALLED. RETURNED TO BDL DUE TO LEFT ENGINE COMPRESSOR STALL. PERFORMED BORESCOPE INSPECTION OF THE ENTIRE LT ENGINE, NO DEFECTS FOUND. REPLACED N2 SPEED PROBE AND RETUR
- [SDR DALA2026010500069](https://openairdocs.org/sdr/DALA2026010500069), Jan 1, 2026: EEC. FAULTED. ATB TO DTW DUE TO LEFT ENGINE COMPRESSOR STALL ON CLIMB OUT. PERFORMED BORO INSP NO DAMAGED FOUND. REPLACED EEC, OPS CHECK NORMAL. (8071484)
- [SDR DALA2025121009010](https://openairdocs.org/sdr/DALA2025121009010), Dec 7, 2025: RELAY. FAULTED. EMERGENCY LIGHTS FLICKER ON AND OFF DURING FLGHT. REMOVED AND REPLACED RELAY R2-5133 PER B717 WDM 24-51-01. (8071400)
- [SDR DALA2025121009017](https://openairdocs.org/sdr/DALA2025121009017), Dec 6, 2025: BATTERY PACK. FAULTED. SEAT ROWS 23-29 CEILING EMER LIGHTS GO OFF AFTER SHORT TIME. REMOVED AND REPLACED BATTERY FOR PACK B5-231 PER B717 AMM 33-51. (8071402)
- [SDR DALA2025121009016](https://openairdocs.org/sdr/DALA2025121009016), Dec 5, 2025: RELAY. FAULTED. EMERGENCY LIGHTS FLICKER ON & OFF. REMOVED & REPLACED RELAY R2-5133 REF AIPC 24-50-22-01 ITEM 40, WDM 33-51-11. OPS CHECK NORMAL AT THIS NORMAL AT THIS TIME. (7
- [SDR DALA2025121009014](https://openairdocs.org/sdr/DALA2025121009014), Dec 4, 2025: LIGHT. NO DISCREPANCY. ONCE AIRBORNE, ALL EMERGENCY LIGHTS CAME OM AND WOULD NOT RESET ROW 25/22 EMER LIGHTS ARE OUT & EXIT LIGHT OUT AT EMER EXIT. EMER LIGHTD WENT OUT WHEN LDG GEAR 
- [SDR DALA2025111808417](https://openairdocs.org/sdr/DALA2025111808417), Nov 12, 2025: SLIDE. DEFLATED. SLIDE IN TAIL CONE FOUND DEFLATED IN TAIL COMPARTMENT. REMOVED TAIL CONE SLIDE IAW AMM 25-61-02. INSTALLED NEW TAIL CONE SLIDE IAW WC 2561-9006 (7585377)
- [SDR DALA2025111208303](https://openairdocs.org/sdr/DALA2025111208303), Nov 11, 2025: WARNING MESSAGE. FALSE ACTIVATION. ATO- APPROX 85KTS DUE TO RUDDER RESTRICTED MESSAGE. PERFORMED RUDDER THROW LIMIT FUNCTIONAL TESTS AND RUDDER INSPECTIONS. NO DEFECTS NOTED, OPS NORMAL. (7585374
- [SDR DALA2025041502918](https://openairdocs.org/sdr/DALA2025041502918), Apr 12, 2025: PSEU. FAILED. SHIP 9553 -MISC/DE- THE CREW DECLARED AN EMERGENCY WITH ATC DUE TO THE "PROXIMITY SWITCH ELECTRONIC UNIT FAIL" MESSAGE ILLUMINATING. THE FLIGHT LANDED WITHOUT F
- [SDR DALA2025020500881](https://openairdocs.org/sdr/DALA2025020500881), Feb 5, 2025: DOOR FRAME. CORRODED. CORROSION ON AFT CARGO DOOR JAMB AT AFT CARGO BIN. SUMMARY OF NRC 00064: CORROSION LEVEL 2. THE AFT CARGO DOOR JAMB AT AFT CARGO BIN WAS REPAIRED PER B717-200 S
- [SDR DALA2025020300802](https://openairdocs.org/sdr/DALA2025020300802), Feb 1, 2025: CARGO TRACK. CORRODED. CORROSION WAS FOUND ON THE AFT CARGO COMP TIE TRACK LOCATED BETWEEN Y=995 TO Y=1022. SUMMARY OF NRC 00133: CORROSION LEVEL 2. THE TIE TRACK LOCATED BETWEEN Y=99
- [SDR DALA2024021201856](https://openairdocs.org/sdr/DALA2024021201856), Feb 12, 2024: BATTERY PACK. INOPERATIVE. DOOR 1L & 1R EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT STA B5-118 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #9376629)
- [SDR DALA2023031601913](https://openairdocs.org/sdr/DALA2023031601913), Mar 15, 2023: UNKNOWN. UNKNOWN. DAMAGE T: HOLE CAUSED BY TOOLING DAMAGE ON ELEVATOR RH BTW XHR 214 AND XHR 218.762, AND 13 INCHES FWD APROX OF ELEVATOR TRAILING EDGE. SUMMARY OF NRC 00680: ELE
- [SDR DALA2023031401848](https://openairdocs.org/sdr/DALA2023031401848), Mar 12, 2023: UNKNOWN. UNKNOWN. DENT ON ELEVATOR RH BTW XHS 55 AND XHS 76, AND 12.5 INCHES FWD APROX OF ELEVATOR TRAILING EDGE. SUMMARY OF NRC 00679: DENT ON ELEVATOR RH BTW XHS 55 AND XHS 76,
- [SDR DALA2023031401847](https://openairdocs.org/sdr/DALA2023031401847), Mar 11, 2023: UNKNOWN. UNKNOWN. CORROSION ON LONGERON 18RH AT R1 PASSENGER DOOR (AFT EDGE). SUMMARY OF NRC 00479: CORROSION LEVEL: 2. LONGERON 18RH AT R1 PASSENGER DOOR (AFT EDGE) WAS REPAIRED
- [SDR DALA2023030701659](https://openairdocs.org/sdr/DALA2023030701659), Mar 5, 2023: NONE. NONE. CORROSION ON RH/LH TRACKS (RH) FROM STA Y=813 TO STA Y=896 AND (LH) TRACK FROM STA Y=813 TO STA Y=947 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00682: CORROSION 
- [SDR DALA2023030801719](https://openairdocs.org/sdr/DALA2023030801719), Mar 3, 2023: NONE. NONE. FOUR (4) CRACKS WERE DISCOVERED ON THE FUSELAGE SKIN. SUMMARY OF NRC 00157: PERMANENT REPAIR ON FUSELAGE SKIN WAS ACCOMPLISHED PER ER/A 566828-14 REV. B SECTION
- [SDR DALA2023030701657](https://openairdocs.org/sdr/DALA2023030701657), Mar 3, 2023: NONE. NONE. CORROSION ON FINGER DOUBLER ADJACENT TO L-26LH, STA Y=1010 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00673: CORROSION LEVEL 2. FINGER DOUBLER ADJACENT TO L-26LH,
- [SDR DALA2023030201556](https://openairdocs.org/sdr/DALA2023030201556), Mar 1, 2023: NONE. NONE. CORROSION ON LONGERON 30, BTW STA Y:946 AND STA Y:974 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00255: CORROSION LEVEL 2: LONGERON 30 BTW STA Y:946 AND STA Y:974 
- [SDR DALA2023022501419](https://openairdocs.org/sdr/DALA2023022501419), Feb 23, 2023: NONE. NONE. RE-WRITE TO NRC #00493: DUE TO INADEQUATE STEERING OF THE RELATED STATIONS. THIS NRC IS TO CLARIFY THE CORRECT LOCATION FOR EACH STRUCTURAL ELEMENT. CORROSION O
- [SDR DALA2023022501418](https://openairdocs.org/sdr/DALA2023022501418), Feb 23, 2023: NONE. NONE. AFTER REMOVAL OF FORWARD JAM PAN SEALS,CRACK WAS FOUND ON THE FWD SEAL. SUMMARY OF NRC 00626: REPAIR DOUBLER WAS INSTALLED PER B717-200 SRM 53-00-00-2R PROCEDUR
- [SDR DALA2023022501417](https://openairdocs.org/sdr/DALA2023022501417), Feb 23, 2023: NONE. NONE. CORROSION ON FLOOR STRUCTURE SUPPORTS ALONG FWD DIAPHRAGM AT CPAX, BTW STA Y=200 TO Y=237 AND BL (-X)=55. SUMMARY OF NRC 00518: CORROSION LEVEL 2. FLOOR STRUCTU
- [SDR DALA2023022401416](https://openairdocs.org/sdr/DALA2023022401416), Feb 23, 2023: NONE. NONE. CRACKS (3 EA) ON FRAMES AT LH CANTED KEEL STA Y=674, Y=696, AND Y=715, (-X)=27. SUMMARY OF NRC 00319; FRAMES (3 EA) AT LH CANTED KEEL STA Y=674, Y=696, AND Y=71
- [SDR DALA2023022401413](https://openairdocs.org/sdr/DALA2023022401413), Feb 23, 2023: NONE. NONE. CRACKS (2 EA) ON FRAMES AT RH CANTED KEEL STA Y=696 AND Y=715, (X)=27. SUMMARY OF NRC 00320: FRAMES (2 EA) AT RH CANTED KEEL STA Y=696 AND Y=715, (X)=27. WERE R
- [SDR DALA2023022201323](https://openairdocs.org/sdr/DALA2023022201323), Feb 20, 2023: NONE. NONE. CORROSION ON CUSP WEB BETWEEN STA Y=200 TO STA Y=218 AND BL (-X)=55. SUMMARY OF NRC 00519: CUSP WEB WAS FABRICATED PER DWG 9936535 REV CS AND CUSP WEB BETWEEN S
- [SDR DALA2023022201322](https://openairdocs.org/sdr/DALA2023022201322), Feb 19, 2023: NONE. NONE. CORROSION ON L-22LH, Y STA 845 AT FILLET FAIRING STRUCTURE. SUMMARY OF NRC 00277: CORROSION LEVEL 2. LONGERON STA 845 STR 22LH WAS REPLACED PER DWG 5911420 REV:
- [SDR DALA2023022201321](https://openairdocs.org/sdr/DALA2023022201321), Feb 19, 2023: NONE. NONE. SECONDARY NRC, IN REF NRC 00618: CORROSION ON MEMBRANE ON WEB BTW STA Y=180 - 200 UNDER OF FLOOR SUPPORT RH. SUMMARY OF NRC 00650: CORROSION LEVEL 2. REPAIR OF 
- [SDR DALA2023022001259](https://openairdocs.org/sdr/DALA2023022001259), Feb 19, 2023: NONE. NONE. SECONDARY NRC IN REF NRC #00493: SEVERAL DINGS ON DIAPHRAGM AT STA Y=176, BTW (-X)=15 TO (-X)=42. SUMMARY OF NRC 00660: DINGS ON DIAPHRAGM AT STA Y=176, BTW (-X
- [SDR DALA2023022001257](https://openairdocs.org/sdr/DALA2023022001257), Feb 18, 2023: NONE. NONE. A.A. A.D. CRACK WAS FOUND OF 0.437" LENGTH ON FRAME STA Y=715 RH SIDE IN REF CARD 5310-01436-04D JOB #074-0004 STEP: 13. SUMMARY OF NRC 00329: FRAME STA Y=715 R
- [SDR DALA2023022001256](https://openairdocs.org/sdr/DALA2023022001256), Feb 18, 2023: NONE. NONE. CORROSION ON FLOOR SUPPORT X=20 STA Y=236 PASSENGER CABIN (W1). SUMMARY OF NRC 00531: CORROSION LEVEL 2. FLOOR SUPPORT X=20 STA Y=236 PASSENGER CABIN (W1) WAS R
- [SDR DALA2023022001255](https://openairdocs.org/sdr/DALA2023022001255), Feb 17, 2023: NONE. NONE. WEAR ON CABLE TAIL CONE ASSEMBLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY NRC 00290
- [SDR DALA2023021701233](https://openairdocs.org/sdr/DALA2023021701233), Feb 16, 2023: NONE. NONE. CORROSION ON RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 AT CPAX. SUMMARY OF NRC 00649: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 W
- [SDR DALA2023021701232](https://openairdocs.org/sdr/DALA2023021701232), Feb 16, 2023: NONE. NONE. IN REF NRC #00492: CORROSION ON RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 AT CPAX. SUMMARY OF NRC 00649: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=385 AND 
- [SDR DALA2023021701230](https://openairdocs.org/sdr/DALA2023021701230), Feb 16, 2023: NONE. NONE. CRACK ON INTERCOSTAL FROM STA Y=1002 TO Y=1022 ON PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00584: INTERCOSTAL FROM STA Y=1002 TO Y=1022 ON PASSENGER CABI
- [SDR DALA2023021501184](https://openairdocs.org/sdr/DALA2023021501184), Feb 15, 2023: UNKNOWN. UNKNOWN. CORROSION ON SUPPORT WEB AT STA 579 TO 598 L17 RH FWD CARGO COMPARTMENT. SUMMARY OF NRC 00331: CORROSION LEVEL 2. SUPPORT WEB AT STA 579 TO 598 L17 RH FWD CARGO
- [SDR DALA2023021501183](https://openairdocs.org/sdr/DALA2023021501183), Feb 14, 2023: UNKNOWN. UNKNOWN. CORROSION ON LH CENTER SEAT TRACK X=44 FROM STA Y=200 TO Y=256. SUMMARY OF NRC 00523: CORROSION LEVEL 2. LH CENTER SEAT TRACK AND SPLICE WAS REPLACED ON X=44 FR
- [SDR DALA2023021501181](https://openairdocs.org/sdr/DALA2023021501181), Feb 13, 2023: NONE. NONE. SECONDARY NRC, IN REF NRC 00488 CORROSION ON LH CUSP WEB BTW STA Y=560 - 579 AND BTW Y=609 TO 617. SUMMARY OF NRC 00612: CUSP WEB LH BTW STA Y=560 TO 579 AND BT
- [SDR DALA2023021501177](https://openairdocs.org/sdr/DALA2023021501177), Feb 12, 2023: NONE. NONE. CORROSION ON RH INBD SEAT TRACK -X=22 FROM STA Y=200 TO Y=256. SUMMARY OF NRC 00524: CORROSION LEVEL 2. RH INBD SEAT TRACK -X=22 FROM STA Y=200 TO Y=256 WAS REP
- [SDR DALA2023021401128](https://openairdocs.org/sdr/DALA2023021401128), Feb 10, 2023: UNKNOWN. UNKNOWN. CORROSION ON ANGLE AT L1 DOOR JAMB (LWR SIDE) BTW STA Y=157 TO 186, BL -X=55 AT CPAX. SUMMARY OF NRC 00476: CORROSION LEVEL 2. ANGLE AT L1 DOOR JAMB (LWR SIDE) 
- [SDR DALA2023021401124](https://openairdocs.org/sdr/DALA2023021401124), Feb 9, 2023: UNKNOWN. UNKNOWN. CRACK ON FWD PAN OF FWD CARGO DOOR BTW BEAM 2 AND 3. SUMMARY OF NRC 00294: FWD PAN OF FWD CARGO DOOR BTW BEAM 2 AND 3 WAS REPAIRED PER B717-200 SRM 52-30-02-2R 
- [SDR DALA2023021401123](https://openairdocs.org/sdr/DALA2023021401123), Feb 9, 2023: UNKNOWN. UNKNOWN. CRACK ON INTERCOSTAL ON L1 DOOR INTERNAL STRUCTURE (BEHIND OPEN/CLOSURE HANDLE). SUMMARY OF NRC 00315: INTERCOSTAL ON L1 DOOR INTERNAL STRUCTURE (BEHIND OPEN/CL
- [SDR DALA2023021401122](https://openairdocs.org/sdr/DALA2023021401122), Feb 9, 2023: UNKNOWN. UNKNOWN. IN REF NRC 00294: CRACK ON FWD PAN OF FWD CARGO DOOR ON BEAM 5. SUMMARY OF NRC 00628: FWD PAN OF FWD CARGO DOOR ON BEAM 5 WAS REPAIRED PER B717-200 SRM 52-30-02
- [SDR DALA2023021401133](https://openairdocs.org/sdr/DALA2023021401133), Feb 7, 2023: UNKNOWN. UNKNOWN. WORN ON PREVIOUS REPAIR (2EA) OF FWD CARGO DOOR BARRIER LATCHES. SUMMARY OF NRC 00547: REPAIR DOUBLERS WERE REPLACED PER ER/A 559579-14MA REV ORIGINAL, SECTION 
- [SDR DALA2023020700926](https://openairdocs.org/sdr/DALA2023020700926), Feb 7, 2023: NOT REPORTED. NOT REPORTED. IN REF TO NRC 00497: FABRICATE CUSP WEB. SUMMARY OF NRC 00497: CUSP WEB WAS FABRICATED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #2618064)
- [SDR DALA2023020600882](https://openairdocs.org/sdr/DALA2023020600882), Feb 5, 2023: NOT REPORTED. NOT REPORTED. CRACK WAS FOUND AT AFT BRACKET OF LOWER LINNER SUPPORT BRACKETS. SUMMARY OF NRC 00619: AFT BRACKET (ANGLE) OF PASSENGER DOOR L1 IN LOWER INTERNAL STRUCTURE WAS 

All 171: https://openairdocs.org/aircraft/N893AT/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/N893AT/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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