# N952AT: 2000 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: 55014
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 3, 2000
- Certificate issued: November 22, 2023
- Expires: November 30, 2030
- Mode S code: AD3C27
- 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=952AT
- Page: https://openairdocs.org/aircraft/N952AT

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/N952AT/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 N952AT.

## FAA accident and incident reports

None matched to N952AT.

## Service difficulty reports (251, 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 DALA2026062503779](https://openairdocs.org/sdr/DALA2026062503779), Jun 24, 2026: SLIDE. NO DISCREPANCY. L1 DOOR SLIDE REMOVED FOR MTC REF AMDS W/C 2561-9004. INSTALLED L1 DOOR SLIDE PER AMDS WORK CARD 2561-9004. (8908875) (AIRCRAFT GROUNDED)
- [SDR DALA2026031801858](https://openairdocs.org/sdr/DALA2026031801858), Mar 12, 2026: PAN. CRACKED. CRACKED WAS FOUND ON INNER PAN (FWD SIDE)Y 964 BEAM 4 ALSO CRACKED INNER PAN (AFT SIDE)Y 994 BEAM 5 AT AFT CARGO COMPARTMENT DOOR. REPAIRED PER ER/A 631760-14. 
- [SDR DALA2026031301747](https://openairdocs.org/sdr/DALA2026031301747), Mar 12, 2026: ACCESS PANEL. DAMAGED. ELONGATED FASTENER HOLE ON ACCESS PANEL NBR:340UT AT RH ELEVATOR, AND ON 330ST AT LH ELEVATOR. REPAIRED PER ER/A NO. 631774-14 (1490586)
- [SDR DALA2026031301749](https://openairdocs.org/sdr/DALA2026031301749), Mar 10, 2026: SUPPORT ANGLE. CRACKED. CRACK ON ANGLE SUPPORT STA Y=713 X=44 AT PAXCABIN WINGBOX AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 631793-14 (1488643)
- [SDR DALA2026031301746](https://openairdocs.org/sdr/DALA2026031301746), Mar 10, 2026: FRAME ANGLE. CRACKED. SHIP 9511 CRACK ON ANGLE OF FRAME STA 1153 AND BTW S1 TO S2L ALSO MISSING FASTENER ON SAME POSITION AFT ACCESSORY COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER E
- [SDR DALA2026031001642](https://openairdocs.org/sdr/DALA2026031001642), Mar 7, 2026: DOOR FRAME. CRACKED. SHIP 9511 CRACK ON HOLE DOOR JAMB BTW STA Y=946 TO Y= 948 APROX LONG 28 RH BELOW TIE TRACK AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 5
- [SDR DALA2026030501524](https://openairdocs.org/sdr/DALA2026030501524), Mar 3, 2026: LONGERON. CORRODED. AFTER REMOVING CORROSION ON LONGERON 30, BTW BS 1022 - 927 IN THE AFT CARGO BAY. REPLACED IAW SRM 51-41-02-0G AND SRM 51-41-05-0G. (1477180)
- [SDR DALA2026030201421](https://openairdocs.org/sdr/DALA2026030201421), Feb 26, 2026: SKIN. CRACKED. CRACK ON FUSELAGE SKIN STA Y = 1087 LONG 13 LH-14LH SIDE. REPAIR AND PRI 631743-14 (1469678)
- [SDR DALA2026030201420](https://openairdocs.org/sdr/DALA2026030201420), Feb 26, 2026: HINGE FITTING. CORRODED. CORROSION WAS FOUND ON INB AND OUT HOLES (4EAS) UPPER AND LOWER HINGE FLAP ALSO ON SETTLEMENT AREA. REPAIRED PRI 631842-14 REV 2 AND ER/A 631842-14. (1469307)
- [SDR DALA2026030201417](https://openairdocs.org/sdr/DALA2026030201417), Feb 24, 2026: SKIN. CRACKED. CRACK ON FUSELAGE SKIN STA Y =1037 LONG 13 LH-14LH SIDE. REPAIRED PER PRI 631741-14 (1466248)
- [SDR DALA2026021801177](https://openairdocs.org/sdr/DALA2026021801177), Feb 17, 2026: CUSP WEB. CRACKED. AIRCRAFT 9511, CRACK WAS FOUND ON CUSP WEB AT X=-44 BTW BS 636 - 655 AT PAX CABIN. CRACKED ON CUSP WEB AT X=-44 BTW STA Y=636 - 655 AT PAX CABIN WAS REPAIRED PE
- [SDR DALA2026021801124](https://openairdocs.org/sdr/DALA2026021801124), Feb 15, 2026: FRAME. CRACKED. CRACKS ON LT & RT FRAMES BS 1037 LONGERON 17. DAMAGED AREA REPAIRED IAW SRM 53-20-07 (1452565).
- [SDR DALA2026021801123](https://openairdocs.org/sdr/DALA2026021801123), Feb 14, 2026: CUSP WEB. CORRODED. CORRODED CUSP WEB, BS 794 - 813, X= 55. DAMAGED AREA REPAIRED IAW SRM 53-20-07. (1451076).
- [SDR DALA2026021801122](https://openairdocs.org/sdr/DALA2026021801122), Feb 13, 2026: CUSP WEB. CORRODED. CORROSION ON LT CUSP WEB BTW BS 380 - 389, BS 461 - 465, BS 503 - 522. DAMAGED AREA REPAIRED IAW SRM 53-20-07. (1449930).
- [SDR DALA2026021801121](https://openairdocs.org/sdr/DALA2026021801121), Feb 13, 2026: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORTS BTW BS 195, X= 18 - 22, BS 200, X=10 - 15, & BS 200, X=12 TO X=44. DAMAGED AREA REPAIRED IAW SRM 51-41-02. (1449816).
- [SDR DALA2026021801119](https://openairdocs.org/sdr/DALA2026021801119), Feb 13, 2026: SKIN. CRACKED. CRACKED FUSELAGE SKIN, BTW LONGERONS 13 - 14R BS 1022. DAMAGED AREA REPAIRED IAW ER/A 631752-14. (1449591).
- [SDR DALA2026021801117](https://openairdocs.org/sdr/DALA2026021801117), Feb 12, 2026: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORTS BTW BS 60 - 200, X=56. DAMAGED AREA REPAIRED IAW SRM 51-41-05 (1448041).
- [SDR DALA2026021801116](https://openairdocs.org/sdr/DALA2026021801116), Feb 11, 2026: WEB. CRACKED. CRACKED LOWER WEB, BS 674, X= - 44.5, DAMAGED AREA REPAIRED IAW SRM 53-00-55. (1446890).
- [SDR DALA2026021801131](https://openairdocs.org/sdr/DALA2026021801131), Feb 11, 2026: CUSP WEB. PUNCTURED. PUNCTURED CUSP WEB, BS 678, X=- 54. DAMAGED AREA REPAIRED IAW SRM 53-00-55. (1446439)
- [SDR DALA2026021801130](https://openairdocs.org/sdr/DALA2026021801130), Feb 11, 2026: CUSP WEB. CRACKED. CRACKED LOWER SURFACE OF RT CUPS WEB BS 219, 238, 654, 896, AND 942. DAMAGED AREA REPAIRED IAW SRM 53-00-55-2R (1446401).
- [SDR DALA2026021801125](https://openairdocs.org/sdr/DALA2026021801125), Feb 10, 2026: HINGE FITTING. DAMAGED. DAMAGED RT WING FLAP HINGE FITTING AT XW=251.68 28. DAMAGED AREA REPAIRED IAW ER/A 00-631842 (1445336).
- [SDR DALA2026020900907](https://openairdocs.org/sdr/DALA2026020900907), Feb 4, 2026: VANE. NICKED. INITIAL INSPECTION: NICKS (2EA) ON AFT FLAP MOVEABLE VANE LOWER SURFACE AT LT WING. REPAIRED IAW SRM 51-70-02, AND SRM 57-53-01 (1435960)
- [SDR DALA2026012700602](https://openairdocs.org/sdr/DALA2026012700602), Jan 25, 2026: PAN. CRACKED. CRACKED OUTER PAN BS 370 BEAM 3 AT FWD CARGO DOOR. REPAIRED IAW SRM 52-30-02 (1418911)
- [SDR DALA2026012700601](https://openairdocs.org/sdr/DALA2026012700601), Jan 21, 2026: CUSP WEB. CRACKED. CRACKED LOWER SURFACE OF LT CUSP WEB, BS 258 - 814. REPAIRED IAW SRM 53-00-55. (1413152)
- [SDR DALA2025102407792](https://openairdocs.org/sdr/DALA2025102407792), Oct 21, 2025: DOUBLER. NOT REPORTED. EXISTING REPAIRS FOUND THAT IMPACTS INSPECTION ACCOMPLISHMENT. REPAIR INVESTIGATION REQUIRED PRIOR TO FURTHER FLIGHT. PERFORMED DOUBLER INSPECTION PER ERA 62583
- [SDR DALA2025082606325](https://openairdocs.org/sdr/DALA2025082606325), Aug 22, 2025: FITTING. LEAKING. FUEL LEAK THROUGH FLAP HINGE BRACE FITTING ATTACHING FASTENERS AT LEFT WING STA XRS=164. LH WING AFT LOWER SKIN DOUBLER AT STA XRS= 164 WAS REPAIRED PER PRI 624
- [SDR DALA2025082606324](https://openairdocs.org/sdr/DALA2025082606324), Aug 20, 2025: SKIN. LEAKING. RIGHT WING LOWER SKIN, XRS -164 AT FLAP BRACE FITTING FUEL LEAK TIME LIMITED REPAIR. REPAIRED RH LOWER WING SKIN PER ERA 625837-14AD REV ORIGINAL SECTION I TIME
- [SDR DALA2025013000724](https://openairdocs.org/sdr/DALA2025013000724), Jan 29, 2025: SAFETY PIN. MISSING. MISSING SAFETY PIN OF SLIDE R1 DOOR. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF
- [SDR DALA2025012900689](https://openairdocs.org/sdr/DALA2025012900689), Jan 29, 2025: DOUBLER. CORRODED. CORROSION ON DOUBLER REPAIR, BTW PROJECTION LONGS 26/27RH AT AFT CARGO DOOR, FWD JAMB C2. SUMMARY OF NRC 00010: CORROSION LEVEL 2. DOUBLER REPAIR BTW PROJECTION
- [SDR DALA2024111911029](https://openairdocs.org/sdr/DALA2024111911029), Nov 17, 2024: LIGHT. INOPERATIVE. THE CABIN CEILING MOUNTED EMERGENCY LIGHT AT 2AB IS INOPERATIVE. FORWARD TO MEL 33-51-01A. PLACARDS INSTALLED. ON 18NOV24 MAINTENANCE REPLACED THE 2AB CABIN CEI
- [SDR DALA2024072307417](https://openairdocs.org/sdr/DALA2024072307417), Jul 23, 2024: POWER SUPPLY. INOPERATIVE. PANELS 1-5 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY B5-227 BATTERY PER B717 AMM 33-51. (LP #6208532)
- [SDR DALA2024070506805](https://openairdocs.org/sdr/DALA2024070506805), Jul 4, 2024: BATTERY PACK. NO TEST. AIRCRAFT 9511, DURING SVC CHECK FOUND MID CABIN EMER LIGHTS INOP.CORRECTIVE ACTION: REPLACED MID CABIN EMER LIGHTS BATTERY PACK. (LP 6209356)
- [SDR DALA2023031401852](https://openairdocs.org/sdr/DALA2023031401852), Mar 12, 2023: UNKNOWN. UNKNOWN. INTERFERENCE BETWEEN FITTING TO ATTACH RIGHT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PANEL 630AF AT RH WING FLAP INTERNAL STRUCTURE. SUMMARY
- [SDR DALA2023031401851](https://openairdocs.org/sdr/DALA2023031401851), Mar 12, 2023: UNKNOWN. UNKNOWN. INTERFERENCE BETWEEN FITTING TO ATTACH LEFT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PANEL 530AF AT LH WING FLAP INTERNAL STRUCTURE. SUMMARY 
- [SDR DALA2023031401849](https://openairdocs.org/sdr/DALA2023031401849), Mar 12, 2023: UNKNOWN. UNKNOWN. CORROSION AT INTERNAL FUSELAGE SKIN ON STA Y=636 TO Y=655 BTW STR 29LH AND STR 29RH AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00189: CORROSION LEVEL 2. CORROSION
- [SDR DALA2023031401846](https://openairdocs.org/sdr/DALA2023031401846), Mar 10, 2023: UNKNOWN. UNKNOWN. AFT SPLICE BTW L-28R TO L-28L REMOVAL, FOUND CRACK ON SPLICE FRAME AT STA 636. SUMMARY OF NRC 00244: SPLICE FRAME AT STA 636 WAS REPAIRED PER B-717-200 SRM 51-7
- [SDR DALA2023030801720](https://openairdocs.org/sdr/DALA2023030801720), Mar 7, 2023: NONE. NONE. AFTER DOOR ASSEMBLY, CORROSION WAS FOUND ON SETTLEMENT AREA AT DOOR PANEL P/N 5971074. SUMMARY OF NRC 0240: LEVEL CORROSION 2. (UT) THICKNESS MEASUREMENT WAS AC
- [SDR DALA2023030701661](https://openairdocs.org/sdr/DALA2023030701661), Mar 6, 2023: NONE. NONE. CORROSION ALONG LONGERON L30 FROM STA Y=900 TO Y=1022 AT AFT CARGO COMPARTMENT C2. SUMMARY OF NRC 00178: CORROSION LEVEL 2. NEW SECTION LONGERON L30 FROM STA Y=
- [SDR DALA2023030701660](https://openairdocs.org/sdr/DALA2023030701660), Mar 6, 2023: NONE. NONE. CORROSION ON LONGERION 30 RH BTW STA Y=1031 TO STA Y=1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00195: CORROSION LEVEL 2. LONGERON SECTION 30 FROM STA Y=1022
- [SDR DALA2023030701658](https://openairdocs.org/sdr/DALA2023030701658), Mar 3, 2023: NONE. NONE. CORROSION ON FUSELAGE SKIN ON STA Y=1053 BTW STR 29 LH TO STR 29 RH AT AFT CARGO COMPARTMENT. CORROSION WAS FOUND ON PRODUCTION DOUBLER. SUMMARY OF NRC 00241: C
- [SDR DALA2023030301615](https://openairdocs.org/sdr/DALA2023030301615), Mar 2, 2023: NONE. NONE. CORROSION ON FRAME CLIP ON AFT CARGO COMPARTMENT C2 STA Y=908 BTW LONG L30/L29. SUMMARY OF NRC 00174: CORROSION LEVEL 2. SECTION ON FRAME CLIP ON AFT CARGO COMP
- [SDR DALA2023030201554](https://openairdocs.org/sdr/DALA2023030201554), Mar 1, 2023: NONE. NONE. CORROSION ON INTERCOSTAL AT STR 30 BTW STA Y=1022 TO STA Y=1037 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00193: CORROSION LEVEL 2. INTERCOSTAL AT STR 30 BTW STA
- [SDR DALA2023030201553](https://openairdocs.org/sdr/DALA2023030201553), Mar 1, 2023: NONE. NONE. CORROSION ON FRAME CLIP AND SKIN ON AFT CARGO COMPARTMENT C2 STA Y=1022 BTW LONG L30. SUMMARY OF NRC 00182: CORROSION LEVEL 2. SECTION ON FRAME CLIP AFT CARGO C
- [SDR DALA2023022701428](https://openairdocs.org/sdr/DALA2023022701428), Feb 25, 2023: NONE. NONE. CRACKED PAN ON AFT EDGE BELOW STOP FITTING #2 AT PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE. SUMMARY OF NRC 00235: PAN ON AFT EDGE BELOW STOP FITTING #2 AT PASS
- [SDR DALA2023022501420](https://openairdocs.org/sdr/DALA2023022501420), Feb 24, 2023: NONE. NONE. CRACKED BEAM ON AFT SECTION BELOW STOP FITTING #2 AT PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE. SUMMARY OF NRC 00236: BEAM ON AFT SECTION BELOW STOP FITTING #2
- [SDR DALA2023022201324](https://openairdocs.org/sdr/DALA2023022201324), Feb 21, 2023: NONE. NONE. SECONDARY IN REF TO AMDS 5310-01436-01A: CRACK ON CUSP MEMBRANE WEB AT STA 674 L-18 LH. SUMMARY NRC 00198: CUSP MEMBRANE WEB AT STA 674 L-18 LH WAS REPAIRED PER
- [SDR DALA2023022001258](https://openairdocs.org/sdr/DALA2023022001258), Feb 19, 2023: NONE. NONE. CRACK ON CUSP MEMBRANE WEB AT STA 696 L-18 LH. SUMMARY OF NRC 0209: CUSP MEMBRANE WEB WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE 203. (LP #263606
- [SDR DALA2022112307517](https://openairdocs.org/sdr/DALA2022112307517), Nov 22, 2022: LENS. MISSING. THE EXIT SIGN AT DOOR 1R IS MISSING. MAINTENANCE REPLACED THE MISSING LENS IAW B717 AMM 33-51. (LP #8566118)
- [SDR DALA2022062104328](https://openairdocs.org/sdr/DALA2022062104328), Jun 20, 2022: BATTERY PACK. INOPERATIVE. THE TAIL COMPARTMENT (CATWALK) AFT EMERGENCY CEILING LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK, B5-116, PER B-717 AMM 33-51. O
- [SDR DALA2022052003458](https://openairdocs.org/sdr/DALA2022052003458), May 20, 2022: STRIP. MISSING. THE EMERGENCY ESCAPE PATH LIGHTING STRIP AT ROW 19AB IS MISSING. MAINTENANCE INSTALLED A NEW EEPL INDIGO TAPE STRIP AND END CAPS. THE LUMINESCENT STRIP IS NOW O

All 251: https://openairdocs.org/aircraft/N952AT/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/N952AT/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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