# N949AT: 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: 55003
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 24, 2000
- Certificate issued: December 31, 2019
- Expires: December 31, 2029
- Mode S code: AD2EA9
- 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=949AT
- Page: https://openairdocs.org/aircraft/N949AT

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/N949AT/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 N949AT.

## FAA accident and incident reports

None matched to N949AT.

## Service difficulty reports (238, 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 DALA2026031001638](https://openairdocs.org/sdr/DALA2026031001638), Mar 4, 2026: SKIN. DAMAGED. SHIP 9500 ELONGATED HOLE (1EA) AND TOOL MARKS (1EA ) ON INNER/OUTER SKIN FROM FUEL ACCESS PANEL 620JB AT RH WING. CORRECTIVE ACTION: REPAIRED PER PRI 632126-14 
- [SDR DALA2026031001637](https://openairdocs.org/sdr/DALA2026031001637), Mar 4, 2026: DOUBLER. CRACKED. CRACK ON INTERNAL PRODUCTION DOUBLER INSIDE OF AFT ACCESSORY COMPARMET IN LONGERON 3 RH,CANTED STA Y= 1178.225 APPROX. CORRECTIVE ACTION: REPAIRED PER B717-200 
- [SDR DALA2026030501523](https://openairdocs.org/sdr/DALA2026030501523), Mar 4, 2026: LONGERON. CRACKED. CRACKED LONGERON 2L, BS 1133 IN AFT ACCESSORY COMPARTMENT. REPAIRED IAW SRM 53-00-05 -2R-2. (1478132)
- [SDR DALA2026030501521](https://openairdocs.org/sdr/DALA2026030501521), Mar 1, 2026: FUEL TANK. CRACKED. CRACKED WEB, FUEL TANK, X=56 APROX BS 696 AT LH CENTRAL FUEL TANK. : WEB FUEL TANK X=56 APROX STA Y =696 AT LH CENTRAL FUEL TANK WAS REPAIRED PER ERA 631718-14A
- [SDR DALA2026030501520](https://openairdocs.org/sdr/DALA2026030501520), Mar 1, 2026: FRAME. CRACKED. CRACKED FRAME BS 1133, LONGERON 2 RT, AFT ACCESSORY COMPARTMENT. THE FRAME WAS REPAIRED IAW ERA 631717-14 REV. (1474071)
- [SDR DALA2026030201419](https://openairdocs.org/sdr/DALA2026030201419), Feb 26, 2026: DIAPHRAGM. CRACKED. SHIP 9500 CRACKS ON DIAPHRAGM BTW STA Y=160 TO STA Y= 170 X=8 TO X=9 AT PASSENGER CABIN. CORRECTIVE ACTION: REPAIRED PER B717- 200 SRM 53-00-00 (1468333)
- [SDR DALA2026030201418](https://openairdocs.org/sdr/DALA2026030201418), Feb 24, 2026: SKIN. CORRODED. CORROSION ON SKIN STA 737 X: -15 TO -30 APROX AT FUSELAGE. REPAIR INSTRUCTIONS AND PRI 631685-14 (1466288)
- [SDR DALA2026030201416](https://openairdocs.org/sdr/DALA2026030201416), Feb 24, 2026: SKIN. CRACKED. SHIP 9500 BENT, ALSO CRACK ON RUDDER SKIN AT LH LOWER EDGE XR -5.000 CANT. CORRECTIVE ACTION: REPAIRED PER PRI 631766-14 (1466225)
- [SDR DALA2026022501336](https://openairdocs.org/sdr/DALA2026022501336), Feb 23, 2026: CUSP WEB. CRACKED. CRACK ON RH CUSP WEB AT Y=940 AND Y= 665 X=-53 TO X=-56 ALSO Y=716 X= -44. DAMAGED AREA REPAIRED PER B717-200 SRM 53-00-55 (1464546)
- [SDR DALA2026022501335](https://openairdocs.org/sdr/DALA2026022501335), Feb 23, 2026: SEAT TRACK. DAMAGED. AFTER THICKNESS MEASUREMENT WAS ACCOMPLISHED ON RH SEAT TRACK X= -22.0 (BTW Y=250 TO Y=260. DAMAGED AREA REPAIRED PER SRM 53-20-52 (1464489)
- [SDR DALA2026022501334](https://openairdocs.org/sdr/DALA2026022501334), Feb 23, 2026: CUSP WEB. CRACKED. SHIP 9500 CORROSION ON RH CUSP WEB BTW Y=237 TO Y= 257, BTW Y= 450 TO Y= 455, BTW Y= 484 TO Y= 491, BTW Y= 794 TO Y= 802, BTW Y= 860 TO Y= 865 BTW Y=938 TO Y= 9
- [SDR DALA2026022501333](https://openairdocs.org/sdr/DALA2026022501333), Feb 21, 2026: CUSP WEB. CRACKED. CORROSION ON RH CUSP WEB PREVIOUS REPAIR DOUBLER BTW STA 446 TO 456 X=-60 CABIN FLOOR STRUCTURE. DAMAGED AREA REPAIRED PER SRM 53-00-55 (1462080)
- [SDR DALA2026022501332](https://openairdocs.org/sdr/DALA2026022501332), Feb 21, 2026: CUSP WEB. CRACKED. CORROSION TYPE EXFOLATION AND CRACKED RH CUSP WEBS X=-56 BTW STA 234 TO 248. DAMAGED AREA REPAIRED PER SRM 53-00-55 (1462073)
- [SDR DALA2026022501331](https://openairdocs.org/sdr/DALA2026022501331), Feb 21, 2026: SEAT TRACK. CORRODED. SEAT TRACK BTW STA Y= 200 TO STA Y= 304 X= -22 APPROX CORROSION. DAMAGED AREA REPAIRED IAW SRM 51-70-10 (1460872)
- [SDR DALA2026021901202](https://openairdocs.org/sdr/DALA2026021901202), Feb 19, 2026: WEB. CRACKED. AIRCRAFT 9500, CRACK ON WEB WAS FOUND FROM STA 465 TO STA 475, AFTER REMOVAL OF RT OUTB SEAT TRACK. CRACK ON WEB STA 465 TO STA 475 OF RH OUTB SEAT TRACK WAS RE
- [SDR DALA2026021901199](https://openairdocs.org/sdr/DALA2026021901199), Feb 15, 2026: CUSP WEB. CRACKED. AIRCRAFT 9500, CRACK LT ON CUSP WEB BS 852, BTW Y=655 TO Y=700 AT PAX CABIN. REPLACED IAW SRM 51-41-05-0G, AND SRM 51-41-02-0G PAR 4. (LP 1452693)
- [SDR DALA2026021901198](https://openairdocs.org/sdr/DALA2026021901198), Feb 15, 2026: CUSP WEB. DAMAGED. AFTER THICKNES MEASUREMENT ON LT CUSP WEB BTW BS 332 - 351, BS 446 - 465, BS 522 - 579, BS 813 - 832, BS 889 - 908, & BS 908 - 927. REWORKED AREAS ARE OUT OF LI
- [SDR DALA2026021801120](https://openairdocs.org/sdr/DALA2026021801120), Feb 13, 2026: LONGERON. CRACKED. CRACK, LONGERONS 5R, 6R, & 8R, BS 1022. REPAIRED IAW SRM 53-00-05-2R. (1449808).
- [SDR DALA2026021801115](https://openairdocs.org/sdr/DALA2026021801115), Feb 10, 2026: SKIN. CRACKED. CRACKED FUSELAGE EXTERNAL SKIN, BS 1076, BTW LONGERONS 13-14R. REPAIRED IAW ER/A 631539-14 (1445437).
- [SDR DALA2026021801114](https://openairdocs.org/sdr/DALA2026021801114), Feb 10, 2026: DOUBLER. WORN. WORN PRODUCTION DOUBLER, RT SIDE ON FLIGHT ATTENDANT SEAT STOWAGE AREA, AFT CABIN PRESSURE BULKHEAD. REPAIRED IAW ER/A 14-631800. (1445027).
- [SDR DALA2026020900910](https://openairdocs.org/sdr/DALA2026020900910), Feb 8, 2026: DOOR FRAME. PUNCTURED. PUNCTURED BULKHEAD DOOR JAM AT LOWER SECTION AT Y= 1053, X= 7 APPROX AFT ACCESSORY BAY. REPAIRED IAW SRM 51-70-10. (1442140)
- [SDR DALA2026020900909](https://openairdocs.org/sdr/DALA2026020900909), Feb 8, 2026: LONGERON. CRACKED. CRACKED LONGERONS NR 5L & 6L AT Y= 1022. LONGERONS NR 5L & 6L INSIDE HAT SECTION IN THE PAX CABIN WERE REPAIRED IAW SRM 53-00-05. (1442139)
- [SDR DALA2026020200755](https://openairdocs.org/sdr/DALA2026020200755), Jan 30, 2026: FRAME ANGLE. CRACKED. CRACKED FRAME ANGLES (2 EACH) BS 1022 AND LONGERON 7 RT & LT SIDES AT PASSENGER CABIN. PERMANENT REPAIR IAW PRI 631537-14, REV 1, ERA 631536-14. (1426473)
- [SDR DALA2026020200754](https://openairdocs.org/sdr/DALA2026020200754), Jan 28, 2026: FRAME. CRACKED. CRACKED FRAME BS 1037 AND LONGERON 17LT AT PASSENGER CABIN. FRAME BTWN WAS REPAIRED IAW SRM 53-20-07-2R, PROCEDURE 4, REPAIR 4. (1424411)
- [SDR DALA2026012700603](https://openairdocs.org/sdr/DALA2026012700603), Jan 25, 2026: FRAME. CRACKED. CRACKED FRAME BTW BS 1037, L17R, THE FRAME WAS REPAIRED IAW SRM 53-20-07. (1419213)
- [SDR DALA2026012700600](https://openairdocs.org/sdr/DALA2026012700600), Jan 24, 2026: SKIN. CRACKED. CRACKED LEFT FUSELAGE EXTERNAL SKIN BS 1087 BTW LONGERONS 13 - 14L. REPAIRED IAW ER/A 631513-14 REV. (1416717)
- [SDR DALA2026012200492](https://openairdocs.org/sdr/DALA2026012200492), Jan 16, 2026: SKIN. CRACKED. CRACK INTERNAL SKIN ON TOP FWD EDGE AT FWD ENTRY DOOR. INTERNAL SKIN ON TOP FWD EDGE AT FWD ENTRY DOOR WAS REPAIRED PER B717-200 S.R.M. 52-10-02 (1404734)
- [SDR DALA2025081105988](https://openairdocs.org/sdr/DALA2025081105988), Aug 6, 2025: COVER. UNSECURE. SHIP 9500 ROW 19C & 19D EMERGENCY BATTERY COVER LOOSE. CORECTIVE ACTION: RE-SECURED AS REQUIRED (7813580)
- [SDR DALA2025081105987](https://openairdocs.org/sdr/DALA2025081105987), Aug 6, 2025: APU. ODOR. SHIP 9500 DIRTY SOCKS SMELL WITH APU AIR ON WHEN TAKING OVER THE AIRPLANE. CORECTIVE ACTION: R/R APU REF B717 AMM 49-10 (7813574)
- [SDR DALA2025100807329](https://openairdocs.org/sdr/DALA2025100807329), Jun 30, 2025: SKIN. DAMAGED. AFT CARGO DOOR AND DOOR FRAME: FUSELAGE SKIN DOOR CUTOUT AREA AFT EDGE DAMAGED. C/W AFT CARGO CORROSION ERA 627055-14 REV A. (1055785)
- [SDR DALA2025070104880](https://openairdocs.org/sdr/DALA2025070104880), Jun 30, 2025: WEB. CORRODED. SHIP 9500 AFT CARGO DOOR THRESHOLD WEB CORRODED SEVERAL LOCATIONS AT UPPER AND LOWER SURFACES. CORRECTIVE ACTION: REMOVED AND REPLACED WEB PER B717 DWG 5910158 
- [SDR DALA2025070104876](https://openairdocs.org/sdr/DALA2025070104876), Jun 30, 2025: NOT ENTERED. NO DISCREPANCY. 9500 REPETITIVE INSP PER SECT II. OF ERA 627055-14 REV A. CORRECTIVE ACTION: ACCOMPLISH SECTION II: REPETITIVE INSPECTIONS EVERY EIGHT THOUSAND (8,000) FLIGHT C
- [SDR DALA2025061104462](https://openairdocs.org/sdr/DALA2025061104462), Jun 8, 2025: SKIN. BENT. AIRCRAFT 9500, FWD CARGO DOOR AND DOOR FRAME: DOOR SKIN BENT ALONG LOWER EDGE. CORRECTIVE ACTION: REPAIRED PER B717 SRM 52-00-01-2R-8. (LP 1011857)
- [SDR DALA2025060604329](https://openairdocs.org/sdr/DALA2025060604329), May 27, 2025: SPAR CAP. CRACKED. SHIP 9500 LH WING REAR SPAR LOWER CAP CRACK. REPAIRED PER ERA 623615-14AD REV 0 (0990246)
- [SDR DALA2025060604324](https://openairdocs.org/sdr/DALA2025060604324), May 25, 2025: REPAIR. NOT REPORTED. SHIP 9500 EXISTING REPAIR FOUND PER ERA 623617-14AD REV ORIG. CORRECTIVE ACTION: REPAIRED PER 623617-14AD (0986223)
- [SDR DALA2025020500872](https://openairdocs.org/sdr/DALA2025020500872), Jan 2, 2025: SPAR CAP. CRACKED. -AD- LEFT WING REAR SPAR LOWER CAP IB OF FLAP TRACK. CRACK INDICATION IN HOLE THAT IS 2 HOLES IB OF EXISTING CRACK, XRS 164. REF PRI 621050-14 REV 1 STEP 11 AND
- [SDR DALA2025020500871](https://openairdocs.org/sdr/DALA2025020500871), Jan 2, 2025: SPAR. CRACKED. -AD- VISIBLE CRACK FOUND ON LEFT WING REAR SPAR LOWER CAP IB OF FLAP TRACK, OB OF THE TE RIB CLIP BETWEEN XRS 150.450 AND XRS 164.000. SUMMARY SEE NRC 006-0001:
- [SDR DALA2025020500870](https://openairdocs.org/sdr/DALA2025020500870), Jan 2, 2025: NONE. NONE. -AD- WHILE IN MAINTENANCE, AA WORK CARD 5720-01103-01B RH WING XRS 164, REAR SPAR AND LWR SKIN INSPECTION WAS COMPLETED WITH NO FINDINGS. DAL BELIEVES ADDITIONA
- [SDR DALA2024081408115](https://openairdocs.org/sdr/DALA2024081408115), Aug 14, 2024: BATTERY PACK. INOPERATIVE. FOUND L & R FWD OVERWING EXIT EMERGENCY LIGHTS TO BE INOPERATIVE. ALSO FOUND L & R FWD SERVICE DOOR EXIT EMERGENCY LIGHTS INOPERATIVE. PER B717 WDM 33-51-14, AL
- [SDR DALA2024072907542](https://openairdocs.org/sdr/DALA2024072907542), Jul 27, 2024: BATTERY PACK. INOPERATIVE. CEILING PANEL 6,7,8, AND MID CABIN OVERHEAD EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED #5 EMERGENCY BATTERY PACK PER B717 FRMFIM 33-50. OPERATIONAL CHECK WAS 
- [SDR DALA2024062606519](https://openairdocs.org/sdr/DALA2024062606519), Jun 26, 2024: BATTERY PACK. INOPERATIVE. THE EMERGENCY LIGHT IN CEILING PANELS FROM ROW 2 TO ROW 11 ARE INOPERATIVE. MAINTENANCE FOUND THE EMERGENCY BATTERY #5 B5-227 TO BE INOPERATIVE PER B717 FRMFIM 
- [SDR DALA2024062106298](https://openairdocs.org/sdr/DALA2024062106298), Apr 10, 2024: FLOOR PANEL. GOUGED. FWD CARGO FLOOR PANEL HAS GOUGE AND UPPER SURFACE CRACKED. REPAIRED FLOOR PANEL 121NF FWD CARGO IAW B717-200, SRM 53-20-50-2R, ACCOMPLISH PERMANENT REPAIR WITHI
- [SDR DALA2023101608459](https://openairdocs.org/sdr/DALA2023101608459), Oct 15, 2023: UNKNOWN. UNKNOWN. SHIP 9500 -ATB- THE AIRCRAFT WAS RETURNED TO ATL FOLLOWING COMPRESSOR SURGES IN THE #1 ENGINE. THE PILOT DECLARED AN EMERGENCY WITH ATC AND THE LANDING & TAXI T
- [SDR DALA2023091907688](https://openairdocs.org/sdr/DALA2023091907688), Sep 17, 2023: UNKNOWN. UNKNOWN. FOUND TAIL SLIDE CONTAINER OPEN AND SLIDE UNPACKED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703.
- [SDR DALA2023031702019](https://openairdocs.org/sdr/DALA2023031702019), Mar 15, 2023: UNKNOWN. UNKNOWN. SHIP 9500 -ATB- THE CREW DECLARED AN EMERGENCY AND RETURNED THE AIRCRAFT MYR DUE THE #2 BRAKE OVER TEMPERATURE WARNING ILLUMINATING. QRH PROCEDURES FAILED TO LO
- [SDR DALA2023031401856](https://openairdocs.org/sdr/DALA2023031401856), Mar 13, 2023: UNKNOWN. UNKNOWN. THE FORWRD EMERGENCY OVERWING LIGHTS ARE INOPERATIVE. MAINTENACE REPLACED THE EMERGENCY BATTERY POWER SUPPLY B5-118 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GO
- [SDR DALA2023031401854](https://openairdocs.org/sdr/DALA2023031401854), Mar 13, 2023: UNKNOWN. UNKNOWN. THE OVERHEAD EMERGENCY LIGHT OVER THE CATWALK IS INOPERATIVE. MAINTENACE REPLACED THE POWER SUPPLY B5-116 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR
- [SDR DALA2022122708379](https://openairdocs.org/sdr/DALA2022122708379), Dec 26, 2022: SKIN. DENTED. SEVERAL DENTS ON LOWER SKIN OF RT WING FLAP FIXED VANE, THE SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1, AND SRM 51-70-02-0G.
- [SDR DALA2022122808451](https://openairdocs.org/sdr/DALA2022122808451), Dec 24, 2022: VANE. DAMAGED. DURING TAP-TEST INSPECTION OF DENTS AT RHS FWD MOVABLE VANE, A DISBONDED AREA OF 4.750 IN LENGTH AND 2.000 IN WIDTH WAS FOUND ON THE RUB STRIP. RT FWD MOVABLE V
- [SDR DALA2022122208294](https://openairdocs.org/sdr/DALA2022122208294), Dec 21, 2022: SUPPORT RIB. WORN. WORN INBD RIB SUPPORT ON FIXED LEADING EDGE WS XRS 267.000 APPROX AT RH WING. AD. SUMMARY OF NRC 00166: INBD RIB SUPPORT ON FIXED LEADING EDGE WS XRS 267.000 AP

All 238: https://openairdocs.org/aircraft/N949AT/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/N949AT/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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