# N943AT: 1999 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [BMW Rolls BR-700 series](https://openairdocs.org/engine/bmw-rolls-br-700-series) (registry code 09500)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55006
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 23, 1999
- Certificate issued: December 31, 2019
- Expires: December 31, 2029
- Mode S code: AD185F
- 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=943AT
- Page: https://openairdocs.org/aircraft/N943AT

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every BMW Rolls BR-700 model are included.

## ADs that may apply (OpenAirDocs): 78 in force

### Matched by airframe (Boeing 717-200)

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-21-05](https://openairdocs.org/ad/2025-21-05): Landing Gear · Boeing 717-200. Effective Jan 2, 2026
- [AD 2025-02-07](https://openairdocs.org/ad/2025-02-07): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Mar 17, 2025
- [AD 2024-21-01](https://openairdocs.org/ad/2024-21-01): Wings · Boeing 717-200. Effective Nov 7, 2024
- [AD 2024-20-02](https://openairdocs.org/ad/2024-20-02): Fuselage · Boeing 717-200, DC-9-11, DC-9-12 and 16 more. Effective Oct 21, 2024
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2021-12-12](https://openairdocs.org/ad/2021-12-12): Wings · Boeing 717-200. Effective Jul 29, 2021
- [AD 2021-02-16](https://openairdocs.org/ad/2021-02-16): Ice and rain protection · Boeing 717-200. Effective Mar 30, 2021
- [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018
- [AD 2018-10-08](https://openairdocs.org/ad/2018-10-08): Stabilizers · Boeing 717-200. Effective May 31, 2018
- [AD 2018-03-04](https://openairdocs.org/ad/2018-03-04): Airspeed/Mach Indicator · Boeing 717-200, DC-9-11, DC-9-12 and 23 more. Effective Mar 16, 2018
- [AD 2017-09-09](https://openairdocs.org/ad/2017-09-09): Passenger Compartment Equipment · Boeing 717-200, MD-90-30, CL-600-2C10 (Regional Jet Series 700) and 17 more. Effective Jun 28, 2017
- [AD 2017-01-03](https://openairdocs.org/ad/2017-01-03): Standard practices/structures · Boeing 717-200. Effective Mar 14, 2017
- [AD 2015-02-05](https://openairdocs.org/ad/2015-02-05): Navigation · Boeing 717-200, DC-10-10, DC-10-10F and 13 more. Effective Mar 5, 2015
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2014-05-22](https://openairdocs.org/ad/2014-05-22): Fuselage · Boeing 717-200. Effective Apr 15, 2014
- [AD 2013-19-22](https://openairdocs.org/ad/2013-19-22): JASC Code 53, Fuselage · Boeing 717-200. Effective Nov 6, 2013
- [AD 2012-12-09](https://openairdocs.org/ad/2012-12-09): Horizontal Stabilizer Structure · Boeing 717-200. Effective Jul 23, 2012
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2009-07-07](https://openairdocs.org/ad/2009-07-07): Main landing gear (MLG) · Boeing 717-200. Effective May 5, 2009
- [AD 2008-18-05](https://openairdocs.org/ad/2008-18-05): Elevator standby cable system · Boeing 717-200. Effective Oct 14, 2008
- [AD 2008-11-15](https://openairdocs.org/ad/2008-11-15): Fuel tank systems · Boeing 717-200, DC-9-11, DC-9-12 and 21 more. Effective Jul 3, 2008
- [AD 2008-11-06](https://openairdocs.org/ad/2008-11-06): Gray water drain hose · Boeing 717-200. Effective Jul 3, 2008
- [AD 2008-02-12](https://openairdocs.org/ad/2008-02-12): Center fuel tank · Boeing 717-200. Effective Feb 28, 2008
- [AD 2008-02-08](https://openairdocs.org/ad/2008-02-08): Main fuel tanks · Boeing 717-200. Effective Feb 26, 2008
- [AD 2007-19-15](https://openairdocs.org/ad/2007-19-15): Flight management system (FMS) · Boeing 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Oct 26, 2007
- [AD 2007-19-03](https://openairdocs.org/ad/2007-19-03): Power conversion distribution unit (PCDU) · Boeing 717-200. Effective Oct 17, 2007
- [AD 2007-17-11](https://openairdocs.org/ad/2007-17-11): In-line fuel float switch fuses · Boeing 717-200. Effective Oct 2, 2007
- [AD 2007-13-09](https://openairdocs.org/ad/2007-13-09): Fuel boost pump container · Boeing 717-200. Effective Aug 3, 2007
- [AD 2007-13-01](https://openairdocs.org/ad/2007-13-01): Wiring of the first officer's pitot static heater system · Boeing 717-200. Effective Jul 25, 2007
- [AD 2007-05-06](https://openairdocs.org/ad/2007-05-06): Bulkhead nipple assemblies of the left and right wing vent boxes · Boeing 717-200. Effective Apr 9, 2007
- [AD 2006-20-12](https://openairdocs.org/ad/2006-20-12): Replaces clamp bases on fuel tank vent systems. · Boeing 717-200. Effective Nov 8, 2006
- [AD 2006-10-14](https://openairdocs.org/ad/2006-10-14): Stop pad support fittings · Boeing 717-200, DC-9-11, DC-9-12 and 22 more. Effective Jun 21, 2006
- [AD 2005-16-08](https://openairdocs.org/ad/2005-16-08): Oxygen release system in the forward cabin · Boeing 717-200. Effective Sep 13, 2005
- [AD 2005-11-03](https://openairdocs.org/ad/2005-11-03): Brake fuses. · Boeing 717-200. Effective Jul 1, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-08-02](https://openairdocs.org/ad/2004-08-02): Left and right hand horizontal stabilizer hinge fitting bolts · Boeing 717-200. Effective May 19, 2004
- [AD 2004-03-21](https://openairdocs.org/ad/2004-03-21): Inboard Ends of Outer Skin Panels of Horizontal Stabilizer at Station Xh=7.234 · Boeing 717-200. Effective Mar 17, 2004
- [AD 2004-01-15](https://openairdocs.org/ad/2004-01-15): Auxiliary hydraulic pump · Boeing 717-200. Effective Feb 17, 2004
- [AD 2003-14-05](https://openairdocs.org/ad/2003-14-05): Main spoiler actuators · Boeing 717-200. Effective Jul 31, 2003
- [AD 2003-10-10](https://openairdocs.org/ad/2003-10-10): Rear spar · Boeing 717-200. Effective Jul 1, 2003
- [AD 2003-10-08](https://openairdocs.org/ad/2003-10-08): Upper center fuselage · Boeing 717-200. Effective Jul 1, 2003
- [AD 2003-04-24](https://openairdocs.org/ad/2003-04-24): Support Fitting Assemblies and Stop Pads of Main Spoiler Actuators · Boeing 717-200. Effective Mar 17, 2003
- [AD 2002-21-01](https://openairdocs.org/ad/2002-21-01): Electrical terminal contact pins · Airbus A319-111, A319-112, A319-113 and 66 more. Effective Nov 27, 2002
- [AD 2002-16-09](https://openairdocs.org/ad/2002-16-09): Solenoid operated shut-off valve (SOV) · Boeing 717-200. Effective Sep 3, 2002
- [AD 2002-14-16](https://openairdocs.org/ad/2002-14-16): Spoiler Hold-Down Actuator Supports on Left and Right Wing Rear Spar · Boeing 717-200. Effective Aug 16, 2002
- [AD 2001-18-11](https://openairdocs.org/ad/2001-18-11): Rudder Trim · Boeing 717-200. Effective Oct 1, 2001

### Matched by engine (BMW Rolls BR-700 series)

- [AD 2026-21-04](https://openairdocs.org/ad/2026-21-04): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Nov 23, 2026
- [AD 2025-06-03](https://openairdocs.org/ad/2025-06-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 23, 2025
- [AD 2023-17-11](https://openairdocs.org/ad/2023-17-11): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Sep 20, 2023
- [AD 2022-26-02](https://openairdocs.org/ad/2022-26-02): Accessory Gearboxes · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20, BR700-710C4-11 and 1 more. Effective Jan 27, 2023
- [AD 2021-21-12](https://openairdocs.org/ad/2021-21-12): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A2-20. Effective Dec 13, 2021
- [AD 2021-14-03](https://openairdocs.org/ad/2021-14-03): Turbine Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 19, 2021
- [AD 2021-12-07](https://openairdocs.org/ad/2021-12-07): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 12, 2021
- [AD 2018-18-14](https://openairdocs.org/ad/2018-18-14): Engine Controls · Rolls-Royce Deutschland BR700-710A2-20 and BR700-710C4-11. Effective Oct 12, 2018
- [AD 2016-13-12](https://openairdocs.org/ad/2016-13-12): Pawl carrier pivot pins · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 5, 2016
- [AD 2014-12-03](https://openairdocs.org/ad/2014-12-03): Fuel metering units (FMUs) · Rolls-Royce Deutschland BR700-725A1-12. Effective Jul 17, 2014
- [AD 2014-08-05](https://openairdocs.org/ad/2014-08-05): Low-pressure compressor (LPC) case ice impact panels · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 23, 2014
- [AD 2014-07-02](https://openairdocs.org/ad/2014-07-02): High-pressure (HP) compressor stages 1 to 6 rotor disc assemblies · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 8, 2014
- [AD 2013-12-03](https://openairdocs.org/ad/2013-12-03): Fuel pump tube · Rolls-Royce Deutschland BR700-725A1-12. Effective Jun 14, 2013
- [AD 2013-03-17](https://openairdocs.org/ad/2013-03-17): High-pressure turbine (HPT) stage 1 and stage 2 discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Mar 21, 2013
- [AD 2012-14-01](https://openairdocs.org/ad/2012-14-01): LP compressor booster rotor · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Oct 19, 2012
- [AD 2009-07-01 R1](https://openairdocs.org/ad/2009-07-01-R1): High-pressure (HP) turbine stage 1 discs, and HP turbine stage 2 discs · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 6, 2012
- [AD 2011-22-01](https://openairdocs.org/ad/2011-22-01): Touch-and-go and overshoot on life cycle counting · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Nov 23, 2011
- [AD 2010-25-05](https://openairdocs.org/ad/2010-25-05): Turbine Discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 13, 2011
- [AD 2009-21-04](https://openairdocs.org/ad/2009-21-04): Engine Failure · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Dec 3, 2009
- [AD 2009-04-13](https://openairdocs.org/ad/2009-04-13): Low pressure (LP) compressor (fan) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Mar 26, 2009
- [AD 2005-21-05](https://openairdocs.org/ad/2005-21-05): Fan discs and fan blades · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Nov 25, 2005
- [AD 2005-16-12](https://openairdocs.org/ad/2005-16-12): Independent Overspeed Protection (IOP) unit. · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 26, 2005
- [AD 2000-25-51](https://openairdocs.org/ad/2000-25-51): High Pressure Turbine Disks · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Feb 20, 2001
- [AD 2001-01-01](https://openairdocs.org/ad/2001-01-01): Oil Filter · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Jan 31, 2001
- [AD 98-24-03 R1](https://openairdocs.org/ad/98-24-03-R1): Combustion Core Fairings · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Dec 27, 1999

### Historical (superseded or no longer in force)

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2020-03-20](https://openairdocs.org/ad/2020-03-20) (historical): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Feb 18, 2020
- [AD 2016-09-05](https://openairdocs.org/ad/2016-09-05) (historical): Stabilizers · Boeing 717-200. Effective Jun 8, 2016
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2007-11-13](https://openairdocs.org/ad/2007-11-13) (historical): Principal structural elements (PSEs) · Boeing 717-200. Effective Jun 29, 2007
- [AD 2004-18-04](https://openairdocs.org/ad/2004-18-04) (historical): Airplane Flight Manual (AFM) · McDonnell Douglas 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Sep 20, 2004
- [AD 2003-17-01](https://openairdocs.org/ad/2003-17-01) (historical): Flap system · McDonnell Douglas 717-200. Effective Sep 23, 2003
- [AD 2000-03-51](https://openairdocs.org/ad/2000-03-51) (historical): Jackscrew Assembly · McDonnell Douglas 717-200, DC-9 Series (all), MD-88 and 1 more. Effective Mar 6, 2000
- [AD 2022-24-06](https://openairdocs.org/ad/2022-24-06) (historical): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 6, 2023
- [AD 2013-05-13](https://openairdocs.org/ad/2013-05-13) (historical): Fuel pump splined couplings · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 24, 2013
- [AD 2012-26-14](https://openairdocs.org/ad/2012-26-14) (historical): High-pressure (HP) compressor stages 1 to 6 rotor disc assembly · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Jan 10, 2013
- [AD 2009-07-01](https://openairdocs.org/ad/2009-07-01) (historical): High Pressure (HP) Turbine · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Apr 27, 2009
- [AD 2003-07-11](https://openairdocs.org/ad/2003-07-11) (historical): Fan discs · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Apr 28, 2003
- [AD 2001-05-06](https://openairdocs.org/ad/2001-05-06) (historical): Fan Disk · BMW Rolls-Royce BR700-710A1-10 and BR700-710A2-20. Effective Mar 29, 2001

All 92: https://openairdocs.org/aircraft/N943AT/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 N943AT.

## FAA accident and incident reports

None matched to N943AT.

## Service difficulty reports (213, 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 DALA2026051703032](https://openairdocs.org/sdr/DALA2026051703032), May 13, 2026: COVER. BROKEN. EMERGENCY LIGHT COVER IN FRONT OF FIRST CLASS LAV HAS BROKEN OFF. INSTALLED NEW LIGHT COVER FWD EMG LIGHT PER AMM 33-51 (8903400) (AIRCRAFT GROUNDED)
- [SDR DALA2026041302319](https://openairdocs.org/sdr/DALA2026041302319), Apr 8, 2026: ACM. CONTAMINATED. FUME/SMKE - ON TAXI IN WITH RT PACK ON, WET SOCK SMELL WITH VISIBLE FOG/SMOKE. CORRECTIVE ACTION: FOUND APU WITH NO OIL IN OIL TANK AND EXTENSIVE OIL CONTAMINAT
- [SDR DALA2025121509137](https://openairdocs.org/sdr/DALA2025121509137), Dec 9, 2025: WINDSHIELD. ARCED. WHEN TURNING ON THE WINDSHIELD ANTI ICE SWITCH SENSOR ON F/O'S FWD WINDOW STARTED ARCHING. REMOVED AND REPLACED CENTER WINDSHIELD REF B717 AMM 56-11. (7791708)
- [SDR DALA2025121009012](https://openairdocs.org/sdr/DALA2025121009012), Dec 8, 2025: SWITCH. FAULTED. ATB, CREW REPORTED SMOKE IN THE COCKPIT WITH ASSOCIATED ELECTRICAL SMELL. FOUND ELECTRICAL ODOR TO BE EMITTING FROM THE FIRST OFFICERS MASTER CAUTION PUSH BUTTO
- [SDR DALA2025081806157](https://openairdocs.org/sdr/DALA2025081806157), Aug 1, 2025: TIRE. FAILED. TIRE- #1 MLG TIRE FAILURE AFTER LANDING WITH LEFT ANTISKID FAIL MESSAGE. REPLACED #1 ANTISKID TRANSDUCER, ANTISKID CONTROLLER AND #1-#2 MLG WHEEL ASSEMBLIES. OP
- [SDR DALA2025060704351](https://openairdocs.org/sdr/DALA2025060704351), Jun 2, 2025: SEAT TRACK. CORRODED. AIRCRAFT 9503, FWD GALLEY AREA CORROSION: RH O/B SEAT TRACK CORRODED AT FWD END. CORRECTIVE ACTION: REPAIRED SEAT TRACK PER B717 SRM 53-20-52-2R-5. (LP 1001907)
- [SDR DALA2025060604347](https://openairdocs.org/sdr/DALA2025060604347), Jun 1, 2025: WEB. CRACKED. SHIP 9503 CUSP MEMBRANE DAMAGE (CRACKED) RIGHT SIDE STA STA 200. CORRECTIVE ACTION: REPAIRED PER B717-200SRM 53-00-55-2R PROCEDURE 4. (0999891)
- [SDR DALA2025020400815](https://openairdocs.org/sdr/DALA2025020400815), Feb 4, 2025: BATTERY PACK. INOPERATIVE. THE FWD EXIT SIGN IS NOT ILLUMINATING. MAINTENANCE REPLACED THE BATTERY PACK AT THE FWD OVERHEAD EQUIPMENT F5-259 COMPARTMENT PER B717 AMM 33-51. OPERATIONAL CH
- [SDR DALA2025010300044](https://openairdocs.org/sdr/DALA2025010300044), Dec 31, 2024: SKIN. DAMAGED. SKIN AT FWD LOWER CORNER OF LAV WASTE DUMP CUT OUT PUSHED OUT APPROX .75" FWD LAV WASTE BOX. CREASE IN SKIN APPROX 4" LONG. MAX DEEP IN GAP BETWEEN SKIN AND WAS
- [SDR DALA2024121611739](https://openairdocs.org/sdr/DALA2024121611739), Dec 14, 2024: WIRE. SHORTED. THE FWD EXIT SIGN OVER FWD F/A SEAT IS INOPERATIVE. ALSO, 4 EXIT LIGHTS ON AFT CATWALK ARE INOPERATIVE. MAINTENANCE REPLACED THE FWD EMERGENCY EXIT SIGN (L2-790
- [SDR DALA2024091809133](https://openairdocs.org/sdr/DALA2024091809133), Sep 14, 2024: ANGLE. CRACKED. ANGLE BRACKET AT STATION 1178.255 ABOVE L-9L CRACKED. REPLACED ANGLE BRACKET AT STATION 1178.255 ABOVE L-9L IAW B717 SRM 51-40-02 AND B DRAWING 5420838. INSTALL
- [SDR DALA2024042504694](https://openairdocs.org/sdr/DALA2024042504694), Apr 25, 2024: POWER SUPPLY. NO TEST. DURING THE SERVICE CHECK, THE EMERGENCY LIGHTS AT THE CATWALK WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY B5-237 PER B717 AMM 33-51-03. 
- [SDR DALA2023091508000](https://openairdocs.org/sdr/DALA2023091508000), Aug 8, 2023: RUDDER. DAMAGED. RUDDER RH SKIN PANEL DAMAGED ON UPPER SIDE NEAR STA ZR165.3.
- [SDR DALA2023072505985](https://openairdocs.org/sdr/DALA2023072505985), Jul 25, 2023: UNKNOWN. UNKNOWN. THE TAILCONE COMPARTMENT EMERGENCY LIGHTING IS INOPERATIVE. MAINTENANCE TROUBLE SHOT PER B717 FIM 33-50-00-810-801, WDM 33-51-13, AND 33-51-14. FOUND B5-116 BAT
- [SDR DALA2023071305675](https://openairdocs.org/sdr/DALA2023071305675), Jul 10, 2023: UNKNOWN. UNKNOWN. THE TAIL CONE RELEASE CAM IS CLOCKED INCORRECTLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. M
- [SDR DALA2024022002330](https://openairdocs.org/sdr/DALA2024022002330), Jul 2, 2023: PANEL. CORRODED. AREA OF CORROSION NOTED DIRECTLY FWD OF LEFT SLANT PANEL (MARKED). COMPLIED WITH ERA 610004-14 REV ORIG. PRI 610004-14 REV 0 MATCHES ERA 610004-14 REV ORIG. ASS
- [SDR DALA2023080406298](https://openairdocs.org/sdr/DALA2023080406298), Jul 2, 2023: UNKNOWN. UNKNOWN. AFT CARGO DOOR JAMB CORROSION ON SKIN TO LONGERON ADJACENT TO REAR CARGO DOOR FRAME AT STA 1000. REPAIRED PER ER/A 610079-14 REV. ORIGINAL. (LP #2846315)
- [SDR DALA2023070305303](https://openairdocs.org/sdr/DALA2023070305303), Jul 1, 2023: UNKNOWN. UNKNOWN. AFT CARGO DOOR LOWER PAN HAS CORROSION IN SEVERAL LOCATIONS. MARKED. SUMMARY SEE NRC 001-0270:5300-2016/003 00024: EDGED SEALED AFT CARGO DOOR LOWER PAN REF REP
- [SDR DALA2023063005258](https://openairdocs.org/sdr/DALA2023063005258), Jun 26, 2023: UNKNOWN. UNKNOWN. FWD CARGO DOOR FRAME LOWER PAN HAS CORROSION IN AT LEAST 2 LOCATIONS NEAR STOP FITTINGS. MARKED. SUMMARY SEE NRC 001-0270:5300-2016/001 00018: REPAIRED CARGO DO
- [SDR DALA2023060604564](https://openairdocs.org/sdr/DALA2023060604564), Jun 6, 2023: UNKNOWN. UNKNOWN. FOUND THAT THE EMERGENCY LIGHT IN ROW 20 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-230. OPERATIONAL CHECK WAS GOOD PER B717 AMM 33-51. (LP #9964
- [SDR DALA2023013100774](https://openairdocs.org/sdr/DALA2023013100774), Jan 28, 2023: CHARGER. INOPERATIVE. THE AFT WALKWAY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE AFT BATTERY CHARGER ASSEMBLY PER B717 AMM 33-51-01. (LP #4048883)
- [SDR DALA2023010300006](https://openairdocs.org/sdr/DALA2023010300006), Jan 3, 2023: BATTERY PACK. NO TEST. DURING THE SERVICE CHECK, MAINTENANCE FOUND THE SIDE EXIT LIGHTS INOPERATIVE ON L1, R1 DOORS & FWD OVERWING L&R DOORS. THE EMERGENCY LIGHT BATTERY B5-118 WAS RE
- [SDR DALA2022112107449](https://openairdocs.org/sdr/DALA2022112107449), Nov 18, 2022: LIGHT. INOPERATIVE. THE OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE AT ROW 10. MAINTENANCE FOUND SPLICE FOR EMERGENCY LIGHT TO BE BROKEN. AFTER RESPLICE, THE LIGHT OPERATIONAL CHECK 
- [SDR DALA2022110807207](https://openairdocs.org/sdr/DALA2022110807207), Nov 5, 2022: NONE. NONE. THE EMERGENCY EXIT LIGHT OVER THE AFT CABIN BULKHEAD DOOR AND THE TAIL COMPARTMENT EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BA
- [SDR DALA2022071504932](https://openairdocs.org/sdr/DALA2022071504932), Jul 14, 2022: NONE. NONE. THE FLIGHT ATTENDANT REPORTS THAT THE EMERGENCY SEAT MOUNTED LIGHTING IS INOPERATIVE AT SEAT 20B. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT AT 20B PER B717 
- [SDR DALA2022071504931](https://openairdocs.org/sdr/DALA2022071504931), Jul 14, 2022: NONE. NONE. THE FLIGHT ATTENDANT REPORTS THAT THE EMERGENCY SEAT MOUNTED LIGHTING IS INOPERATIVE AT SEAT 20A. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT AT 20A PER B717 
- [SDR DALA2022031401649](https://openairdocs.org/sdr/DALA2022031401649), Mar 11, 2022: NONE. NONE. THE EMERGENCY EXIT LOCATOR (SIGN) AT L2-791 BY SEAT ROW IA, ON THE CEILING IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN THE POWER SUPPLY B5-259. THE EMER
- [SDR DALA2022091406089](https://openairdocs.org/sdr/DALA2022091406089), Oct 2, 2021: NONE. NONE. REPEAT INSPECTION PER ER/A 594509-14 REQUIRED EVERY 3000FC AFTER REPAIR INSTALLATION. REPAIR IS APPLIED TO RUDDER SN 55010 INSTALLED. ASSOCIATED ER/A 00-594509 
- [SDR DALA2022091406088](https://openairdocs.org/sdr/DALA2022091406088), Oct 2, 2021: NONE. NONE. ESTABLISHING DTE RESTRICTION FOR ER/A 594509-14. REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE FROM THE APPROVAL DATE. ADDITIONAL ENGINEERING AUTHORIZATION (E
- [SDR DALA2021051002629](https://openairdocs.org/sdr/DALA2021051002629), May 9, 2021: POWER SUPPLY. INOPERATIVE. THE EMERGENCY EXIT SIGN ABOVE THE AFT CABIN DOOR IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL C
- [SDR DALA2021040501963](https://openairdocs.org/sdr/DALA2021040501963), Apr 4, 2021: BATTERY PACK. INOPERATIVE. THE FLIGHT ATTENDANT NOTED THAT THE EMERGENCY EXIT SIGN LIGHTS AT THE GALLEY SERVICE DOOR AND CABIN ENTRANCE DOOR, THE LOWER EXIT SIGN LIGHTS AT RT & LT FWD OVE
- [SDR DALA2021011100137](https://openairdocs.org/sdr/DALA2021011100137), Jan 9, 2021: BATTERY PACK. INOPERATIVE. THE TAIL CONE SECTION EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE B5-260 AND B5 -116 BATTERY PACKS AND THE OPERATIONAL CHECKS WERE G
- [SDR DALA2020091403054](https://openairdocs.org/sdr/DALA2020091403054), Sep 13, 2020: DRIVE ASSY. DAMAGED. THE CREW DIVERTED THE AIRCRAFT INTO IAH FOLLOWING A "SLAT DISAGREE" UPON SLAT EXTENSION. IAH HAS A LONGER RUNWAY THAN HOU. CORRECTIVE ACTION: MAINTENANCE FOUND 
- [SDR DALA2020090802971](https://openairdocs.org/sdr/DALA2020090802971), Sep 6, 2020: LENS. MISSING. EMERGENCY LIGHT LENS AT 29L IS MISSING. MAINTENANCE REPLACED THE LENS IAW B717 AMM 33-51.
- [SDR DALA2020050502351](https://openairdocs.org/sdr/DALA2020050502351), May 3, 2020: LANYARD. OUT OF POSITION. THE R1 DOOR SLIDE LANYARD WAS FOUND TO BE INSTALLED IMPROPERLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IS NOT IN COMPLIANCE WITH 14 CFR PART
- [SDR DALA2019120307003](https://openairdocs.org/sdr/DALA2019120307003), Dec 3, 2019: BATTERY PACK. INOPERATIVE. THE EMERGENCY EXIT LIGHTS ABOVE THE AFT DOOR AND IN THE AFT ACCESSORY COMPARTMENT ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK REF AMM
- [SDR DALA2019070704061](https://openairdocs.org/sdr/DALA2019070704061), Jul 6, 2019: ACCESS PANEL. CORRODED. OUT OF LIMITS - CORROSION IN ACCESS 520FT, 520GB, 520DT, 520CT, 520CB AND CENTER FUEL TANK UPPER ACCES PANNEL, SETTLEMENT AREA AND COUNTERSINK HOLES. AT FUEL TA
- [SDR DALA2019070704060](https://openairdocs.org/sdr/DALA2019070704060), Jul 6, 2019: ACCESS PANEL. CORRODED. OUT OF LIMITS- CORROSION IN ACCESS 620 CB, 620AT AND 620 DT SETTLEMENT AREA AND COUNTERSINK HOLES. AT FUEL TANK (AD). ACCES PANEL 620CB WAS REPLACED AND PART NU
- [SDR DALA2019070604055](https://openairdocs.org/sdr/DALA2019070604055), Jul 6, 2019: HINGE BRACKET. CORRODED. AWR, HIDDEN CORROSION (IN REF NRC S/N 00283): CORROSION WAS FOUND ON ELEVATOR HINGE BRACKET HOLES AT RT HORIZONTAL STABILIZER STA XHS=104, 158, 204 AND 2. CORRO
- [SDR DALA2019070604054](https://openairdocs.org/sdr/DALA2019070604054), Jul 5, 2019: LONGERON. CORRODED. INITIAL INSPECTION: SEVERAL CORROSION ON LONGERON L30 FROM STA 889 TO STA 1053 AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2 CORROSION ON LONGERON 30 BTW STA Y=89
- [SDR DALA2019070504040](https://openairdocs.org/sdr/DALA2019070504040), Jul 4, 2019: FASTENER. DAMAGED. INITIAL INSPECTION: DAMAGED INTERNAL HARDWARE ON LEVER OF THE TAIL CONE JETTISON MECHANISM AT RT LOWER CORNER OF THE TAILCONE CUTOUT. NEW HARDWARE ON LEVER OF T
- [SDR DALA2019070504038](https://openairdocs.org/sdr/DALA2019070504038), Jul 4, 2019: SKIN. DENTED. SEVERAL DENTS ( 7 EAS ) ON RH WING AILERON CONTROL TAP UPPER SKIN BTW STATION XAC=3.5 TO XAC=48.2. RT AILERON CONTROL TAB UPPER SKIN DENT 7 WAS REPAIRED PER SRM
- [SDR DALA2019070404035](https://openairdocs.org/sdr/DALA2019070404035), Jul 3, 2019: HANDLE. OUT OF ADJUST. AWR: DURING CHECK OF THE TAILCONE RELEASE SYSTEM, TAILCONE WAS NO RELEASED WITH "EMERGENCY OPERATING HANDLE" OF THE PASSENGER AFT ENTRANCE DOOR PER 5352-2001, S
- [SDR DALA2019070404033](https://openairdocs.org/sdr/DALA2019070404033), Jul 3, 2019: SKIN. CRACKED. INITIAL INSPECTION: CRACKED FUSELAGE SKIN STA Y=97 ON NLG DOOR CUT OUT LT AFT HINGE DOOR. SUMMARY IN REF OF NRC 00039 AREA WAS REPAIRED PER SRM 53-10-01-2R-11, 
- [SDR DALA2019070404031](https://openairdocs.org/sdr/DALA2019070404031), Jul 3, 2019: SKIN. CORRODED. INITIAL INSPECTION: CORROSION ON FUSELAGE SKIN BTW STA Y= 1022 - 1035 AND LONG 23L - 26L. CORROSION LEVEL 2 IN REF OF NRC 00063 AREA WAS REPAIRED PER ER/A 57899
- [SDR DALA2019070203974](https://openairdocs.org/sdr/DALA2019070203974), Jul 1, 2019: FRAME. CORRODED. CORROSION ON FRAME OF STA 974 FROM L29R TO L28L AT AFT CARGO COMPARMENT (C2). NRC 00152: CORROSION LEVEL 2, CORROSION WAS REMOVED PER SRM 51-10-04-0G PAR 26. (L
- [SDR DALA2019070203973](https://openairdocs.org/sdr/DALA2019070203973), Jul 1, 2019: FRAME. CORRODED. CORROSION ON FRAME AFT AND FWD SURFACE AT STA 1022 BTW L28R TO L28L AT AFT CARGO COMPARMENT (C2 ). NRC 00156: CORROSION LEVEL 2, CORROSION ON FRAME AFT AND FWD 
- [SDR DALA2019070103956](https://openairdocs.org/sdr/DALA2019070103956), Jun 30, 2019: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL AT LONG 30 STA=1022-1040 AT AFT CARGO COMPARMENT (REF NRC SN 146) (C2). NRC 00210: CORROSION LEVEL 2, INTERCOSTAL AT LONG 30 STA=1022-1
- [SDR DALA2019070103955](https://openairdocs.org/sdr/DALA2019070103955), Jun 30, 2019: FRAME. CORRODED. CORROSION ON AFT AND FWD FRAME SURFACE AT STA 1037 AFT CARGO COMPARMENT (C2). NRC 160: CORROSION LEVEL 2, CORROSION ON AFT AND FWD FRAME SURFACE AT STA 1037 WAS
- [SDR DALA2019070103954](https://openairdocs.org/sdr/DALA2019070103954), Jun 30, 2019: HINGE. CORRODED. CORROSION ON LT APU DOOR UPPER SECTION HINGE (FUS). NRC 0064: CORROSION LEVEL 2, CORROSION IN UPPER HINGE ON LT APU DOOR WAS REMOVED PER SRM 51-10-04-0G PAR. 26

All 213: https://openairdocs.org/aircraft/N943AT/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/N943AT/stcs.md

## Related

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

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