# N950AT: 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: 55012
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 10, 2000
- Certificate issued: December 31, 2019
- Expires: December 31, 2029
- Mode S code: AD34B9
- 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=950AT
- Page: https://openairdocs.org/aircraft/N950AT

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/N950AT/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 N950AT.

## FAA accident and incident reports

None matched to N950AT.

## Service difficulty reports (215, 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 DALA2026090204949](https://openairdocs.org/sdr/DALA2026090204949), Sep 2, 2026: THRESHOLD. DAMAGED. AFT CARGO THRESHOLD FWD INBD CORNER STICKING UP AND DAMAGED, COMPLIED WITH ERA 636705-14. (9622032) (AIRCRAFT GROUNDED).
- [SDR DALA2026080604547](https://openairdocs.org/sdr/DALA2026080604547), Aug 2, 2026: SKIN. DENTED. DENT FOUND ON THE FUSELAGE BTWN BS 218 - 229, COMPLIED WITH ER/A 636117-14. (1734913) (AIRCRAFT GROUNDED).
- [SDR DALA2026072204285](https://openairdocs.org/sdr/DALA2026072204285), Jul 21, 2026: BATTERY PACK. INOPERATIVE. OVERHEAD EXIT EMERGENCY LIGHT SIGN AND EMERGENCY LIGHT IN FWD GALLEY INOPERATIVE, R & R EMERGENCY BATTERY B5-259 IAW AMM 33- 51. (9127379) (AIRCRAFT GROUNDED).
- [SDR DALA2026072004263](https://openairdocs.org/sdr/DALA2026072004263), Jul 18, 2026: RELAY. FAULTED. DIVERTED TO CVG DUE TO MULTIPLE FLIGHT DECK EFFECTS AFTER TAKEOFF. REPLACED LT PCDU, EMERGENCY POWER SWITCH AND EMERGENCY DC POWER RELAY. PERFORMED VERIFICATION
- [SDR DALA2026041702450](https://openairdocs.org/sdr/DALA2026041702450), Apr 14, 2026: ENGINE. FIRE. FIRE- DURING RIGHT ENGINE START, TGT ROSE RAPIDLY ALONG WITH AUDIBLE STALL. ENGINE SHUTDOWN AND FIRE BOTTLE DISCHARGED. PERFORMED BORESCOPE INSPECTION OF LPC AN
- [SDR DALA2025120108775](https://openairdocs.org/sdr/DALA2025120108775), Nov 25, 2025: NONE. NONE. SHIP 9509 ER/A 623425-14AD REV C REQUIRES STAGE 2 DTA APRPOVAL. C/W ER/A 623425-14AD. (1321407)
- [SDR DALA2025070805067](https://openairdocs.org/sdr/DALA2025070805067), Jul 2, 2025: PAN. CRACKED. SHIP 9509 INITIAL INSPECTION: CRACK ON FWD EDGE INNER AND OUTER PAN DOOR BTW BEAM 1 AT AFT CARGO DOOR COMPARMENT. CORRECTIVE ACTION: FWD EDGE INNER AND OUTER PA
- [SDR DALA2025062504749](https://openairdocs.org/sdr/DALA2025062504749), Jun 24, 2025: FRAME ANGLE. CORRODED. CORROSION ON FRAME ANGLES BTW LONG 28L & 28R AT STA Y=927 AFT CARGO COMPARTMENT. CORROSION LEVEL 2. FRAME ANGLES BTW LONG 28L & 28R AT STA Y=927 AFT CARGO COMPA
- [SDR DALA2025062504748](https://openairdocs.org/sdr/DALA2025062504748), Jun 24, 2025: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTALS BTW STA Y=1022 & Y =1037 AT LONG 30 & LONG 29R BILGE AREA AT AFT CARGO COMPARTMENT. DAMAGED AREA REPAIRED PER B717-200 SRM 51-41-05- 0
- [SDR DALA2025062504746](https://openairdocs.org/sdr/DALA2025062504746), Jun 23, 2025: GUIDE VANE. WORN. WEAR ON GUIDE VANE BEHIND HINGUE FLAP 1 AT RH WING. CORRECTIVE ACTION: GUIDE VANE WAS REPAIRED PER B717-200 SRM 57-53-01.
- [SDR DALA2025062104660](https://openairdocs.org/sdr/DALA2025062104660), Jun 20, 2025: SKIN. DENTED. DENT OUT OF LIMITS, AT LOWER SURFACE ON LH AFT MOVABLE FLAP VANE AT STA XF74 APROX (2 INCHES FROM T.E. AND 12 INCH FROM L.E.): W=WIDTH, Y =DEPTH (NO MORE 0.060 
- [SDR DALA2025062004658](https://openairdocs.org/sdr/DALA2025062004658), Jun 20, 2025: SKIN. CORRODED. AIRCRAFT 9509, CORROSION AT LOWER SKIN DOOR JAMB ON MIDDLE DOORSTOP (AFT CARGO COMPARTMENT). CORRECTIVE ACTION: (CORROSION LEVEL 2) DOOR JAMB ON MIDDLE DOOR TOP
- [SDR DALA2025062004657](https://openairdocs.org/sdr/DALA2025062004657), Jun 19, 2025: FRAME. CRACKED. AIRCRAFT 9509, CRACK ON FRAME STA Y1037 AND L13L AT PAX CABIN. CORRECTIVE ACTION: CRACK ON FRAME STA Y1037 AND L13L AT PAX CABIN. WAS REPAIRED PER B717-200 SRM 
- [SDR DALA2025062004656](https://openairdocs.org/sdr/DALA2025062004656), Jun 19, 2025: FRAME. CRACKED. AIRCRAFT 9509, CRACK ON FRAME STA Y1037 AND L13R AT PAX CABIN. CORRECTIVE ACTION: CRACK ON FRAME STA Y1037 AND L13R AT PAX CABIN. WAS REPAIRED PER B717-200 SRM 
- [SDR DALA2025061904606](https://openairdocs.org/sdr/DALA2025061904606), Jun 19, 2025: PAN. CRACKED. AIRCRAFT 9509, CRACK ON PAN NEAR TO BEAM NBR 2 AFT EDGE AT PASSENGER ENTRANCE DOOR. CORRECTIVE ACTION: PASSENGER ENTRANCE DOOR WAS REPAIRED PER B717-200 SRM 52-
- [SDR DALA2025061904605](https://openairdocs.org/sdr/DALA2025061904605), Jun 18, 2025: DOOR FRAME. CORRODED. AIRCRAFT 9509, CORROSION WAS FOUND ON DOUBLERS REPAIR STA 954 AND 994 BTW S-26R TO S-27R AT LOWER SKIN DOOR JAMB ON AFT CARGO COMPARTMENT. CORRECTIVE ACTION: DO
- [SDR DALA2025061904604](https://openairdocs.org/sdr/DALA2025061904604), Jun 17, 2025: SEAT TRACK. CORRODED. AIRCRAFT 9509, CORROSION ON LH INB SEAT TRACK BTW STA 256 TO 200 AT CABIN PAX. CORRECTIVE ACTION: CORROSION LEVEL 2 // LH INB SEAT TRACK BTW STA 256 TO 200 AT C
- [SDR DALA2025061904603](https://openairdocs.org/sdr/DALA2025061904603), Jun 17, 2025: SEAT TRACK. CORRODED. AIRCRAFT 9509, CORROSION ON INBD RH SEAT TRACK BTW STA 256 TO 200 AT CABIN PAX. CORRECTIVE ACTION: CORROSION LEVEL 2 // INBD RH SEAT TRACK BTW STA 256 TO 200 AT
- [SDR DALA2025061504505](https://openairdocs.org/sdr/DALA2025061504505), Jun 13, 2025: LONGERON. CRACKED. AIRCRAFT 9509, CRACK ON LONGERON 3(EAS) LONGERON 4, 5, AND 6 RH SIDE STA Y=1022 AT PASSENGER CABIN (CPAX). CORRECTIVE ACTION: LONGERON 3(EAS) LONGERON 4, 5, AND
- [SDR DALA2025060904376](https://openairdocs.org/sdr/DALA2025060904376), Jun 8, 2025: PAN. CRACKED. AIRCRAFT 9509, AFTER SEAL RETAINERS REMOVAL, CRACK ON INNER PAN BTW STOP FITTING #1 AND #2 AFT EDGE, AT FWD CARGO DOOR WAS FOUND. CORRECTIVE ACTION: INNER PAN B
- [SDR DALA2025060804360](https://openairdocs.org/sdr/DALA2025060804360), Jun 7, 2025: CUSP WEB. CORRODED. AIRCRAFT 9509, CORROSION ON RH CUSP WEB UPPER & LOWER FACE ON STA Y=373 AT CABIN PAX. CORROSION LEVEL 2, CUSP WEB ON STA Y=373 AT CABIN PAX WAS REAPAIRED PER B7
- [SDR DALA2025052704024](https://openairdocs.org/sdr/DALA2025052704024), May 21, 2025: INSPECTION. NONE. SHIP 9509 COMPLY WITH ERA 623616-14AD RH WING/ REAR SPAR/ LOWER CAP CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 623616-14AD (0978229)
- [SDR DALA2025052704022](https://openairdocs.org/sdr/DALA2025052704022), May 18, 2025: NONE. NONE. SHIP 9509 INSTALL LH INBOARD AND CENTER BUTE DOORS. CORRECTIVE ACTION: C/W ER/A 623425-14AD (0972844)
- [SDR DALA2025052704021](https://openairdocs.org/sdr/DALA2025052704021), May 18, 2025: STRUCTURE. WORN. SHIP 9509 LT WING OUTBD-AIRFRAME-HINGE BOLT HOLE IS WORN. CORRECTIVE ACTION: ALL WORK C/W ON ERA 625207 -14 REV ORG. (0973047)
- [SDR DALA2024123112105](https://openairdocs.org/sdr/DALA2024123112105), Dec 30, 2024: SPAR. CRACKED. CRACK AT LEFT WING REAR SPAR, PRI 623253-14 REV 0 ISSUED. REMOVE TANK PLATES 520FT, 520CB, AND TWO FUEL LINES FOR MAINTENANCE. REMOVED AND REINSTALLED L/H OVER 
- [SDR DALA2024122712030](https://openairdocs.org/sdr/DALA2024122712030), Dec 23, 2024: SPAR CAP. CRACKED. CRACKS FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP RADIUS. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. FC 5720-01103 2N
- [SDR DALA2023081406584](https://openairdocs.org/sdr/DALA2023081406584), Aug 13, 2023: UNKNOWN. UNKNOWN. PUNCTURE IN FUSELAGE RT SIDE AFT OF FORWARD CARGO DOOR. THIS WAS ORIGINALLY DOCUMENTED IN LP #4849328 AND TRANSFERRED TO THIS LOG PAGE. MAINTENANCE REMOVED THE 
- [SDR DALA2023070405377](https://openairdocs.org/sdr/DALA2023070405377), Jul 3, 2023: UNKNOWN. UNKNOWN. THE CEILING EMERGENCY EXIT LIGHT COVER FELL OFF AT ROW 22. MAINTENANCE RESECURED THE LIGHTING COVER. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #8310082)
- [SDR DALA2023022501422](https://openairdocs.org/sdr/DALA2023022501422), Feb 23, 2023: NONE. NONE. LT SLANT PANEL HAS CORROSION ON IT AT NUT PLATE LOCATION SEEN FROM THE INSIDE. BOTTOM ROW APPROX. LBL27. SUMMARY SEE NRC 001-0196:5300-2005/001 00276: COMPLIED 
- [SDR DALA2023021401131](https://openairdocs.org/sdr/DALA2023021401131), Feb 9, 2023: UNKNOWN. UNKNOWN. C/W ERA 597013-14 REV A FUSELAGE SKIN REPAIR AT LAV WASTE VENT. SUMMARY NRC 001-0002:2040-0015/001 00026: COMPLIED WITH ERA 597013-14 REV A FUSELAGE SKIN REPAIR
- [SDR DALA2022051003229](https://openairdocs.org/sdr/DALA2022051003229), May 6, 2022: DOOR SILL. DAMAGED. FORWARD EDGE OF AFT CARGO DOOR FRAME SILL WAS DAMAGED BY BAGGAGE CREW WITH BELT LOADER. MAINTENANCE REMOVED DAMAGED SCUFF PLATE AND REFORMED PER B717 SRM 51-20-
- [SDR DALA2022042903018](https://openairdocs.org/sdr/DALA2022042903018), Apr 28, 2022: NONE. NONE. SHIP 9509 - THE FLIGHT CREW DECLARED AN EMERGENCY DURING LANDING DUE TO THE RIGHT HYDRAULIC QUANTITY SHOWING A LOW INDICATION (BUT NOT EMPTY). CORRECTIVE ACTION
- [SDR DALA2022021500951](https://openairdocs.org/sdr/DALA2022021500951), Feb 12, 2022: NONE. NONE. FUSELAGE CROWN LIGHTNING STRIKE DAMAGE AT PREVIOUS BLEND OUT. NO REPAIR TAG PRESENT. -M-. SUMMARY SEE NRC 001-0249:5300-2018/003 00365: REPAIRED LIGHTNING STRIK
- [SDR DALA2022021500949](https://openairdocs.org/sdr/DALA2022021500949), Feb 12, 2022: NONE. NONE. CORROSION AROUND EXTERIOR SIDE OF VACUUM BLOWER FOR LAV TANK EXHAUST VENT -M-. SUMMARY SEE NRC 001-0247:2550-2003/001 00405: REPAIRED AREA AROUND VENT PER ER/A 
- [SDR DALA2022021500945](https://openairdocs.org/sdr/DALA2022021500945), Feb 4, 2022: NONE. NONE. WHILE PERFORMING INSPECTION OF APU ENCLOSURE FWD SKIN ASSY. STA 1064 FOUND -2 REPAIR DOUBLER TO BE MISSING UPPER RH FASTENER PER ERA 540237-14 REV. O FIG. 2. SU
- [SDR DALA2019020500805](https://openairdocs.org/sdr/DALA2019020500805), Feb 4, 2019: FITTING. CORRODED. CORROSION ON FLOOR FITTINGS G-7 (CPAX). CORROSION LEVEL 2, FLOOR FITTING OF G-7 WAS REPLACED PER ER/A 535099-14MA REV H AND CMM 25-30-16 REPAIR SECTION.
- [SDR DALA2019020400713](https://openairdocs.org/sdr/DALA2019020400713), Feb 3, 2019: CARGO TRACK. CORRODED. SEVERAL POINTS OF CORROSION ON LH TIE TRACK BTW STA 813 TO 1022 AT AFT CARGO COMPARTMENT (CCT). NRC 00271: CORROSION LEVEL 2, CORROSION ON TIE TRACK BTW STA 813
- [SDR DALA2019020400711](https://openairdocs.org/sdr/DALA2019020400711), Feb 3, 2019: CARGO TRACK. CORRODED. SEVERAL POINTS OF CORROSION ON RH TIE TRACK BTW STA 813 TO 954 AT AFT CARGO COMPARTMENT (CCT). NRC 00272: CORROSION LEVEL 2, ON RH TIE TRACK BTW STA 813 TO 954 
- [SDR DALA2019020430710](https://openairdocs.org/sdr/DALA2019020430710), Feb 2, 2019: DOUBLER. CORRODED. DURING INSPECTION OF A REPAIRED AREA AT FUSELAGE SKIN STA 851; L29L-29R, SOME CORROSION WAS FOUND. NRC 00225: REPAIR DOUBLER WAS REPLACED PER ER/A 540245-14 REV
- [SDR DALA2019020200708](https://openairdocs.org/sdr/DALA2019020200708), Feb 2, 2019: ACCESS PANEL. CORRODED. CORROSION ON LAVATORY SERVICE ACCESS INNER PANE AT FUSELAGE. (FUS). NRC 00059: LAVATORY SERVICE ACCESS INNER PANE AT FUSELAGE WAS REPLACED PER B717-200 SRM 51-4
- [SDR DALA2019020430706](https://openairdocs.org/sdr/DALA2019020430706), Feb 2, 2019: SKIN. CORRODED. CORROSION WAS FOUND AT FUSELAGE SKIN STA 851; L29L-29R. NRC 00225: REPAIR DOUBLER WAS REPLACED PER ER/A 540245-14 REV. ORIGINAL. PERFORM ACOMPLISH ER/A 540245-1
- [SDR DALA2019013100635](https://openairdocs.org/sdr/DALA2019013100635), Jan 30, 2019: FLOOR SUPPORT. CORRODED. EXFOLIATION TYPE CORROSION ON FLOOR SUPPORT STA 655 BTW L28L TO L28R 5331-2007 (CCD). NRC 00291: CORROSION LEVEL 2, SUPPORT WAS REPLACED PER SRM 51-41-02-0G AND
- [SDR DALA2019013000624](https://openairdocs.org/sdr/DALA2019013000624), Jan 29, 2019: DOUBLER. CORRODED. CORROSION ON PRODUCTION DOUBLER OF INNER SKIN FUSELAGE BTW STA Y=974 TO 954 AND L30 TO L29R AT AFT CARGO COMPARTMENT 5331-2001. NRC 00224: CORROSION LEVEL 2, PR
- [SDR DALA2019012901848](https://openairdocs.org/sdr/DALA2019012901848), Jan 28, 2019: WINDOW FRAME. CRACKED. CRACK ON LT SLIDE WINDOW FRAME UPPER AFT CORNER STA 120. NRC 00500: LT SLIDE WINDOW STIFFENER (BRACKET) UPPER AFT CORNER STA 120 WAS REPLACED PER SRM 51-41-01-0
- [SDR DALA2019030601500](https://openairdocs.org/sdr/DALA2019030601500), Jan 28, 2019: SKIN. CRACKED. TWO CRACKS ON FWD TOP SKIN AND ONE CRACK ON UPPER RIGHT EDGE AT FWD WALL OF APU COMPARTMENT IN REF NRC 00369. (CAT). NRC 00513: CRACKS (2) ON FWD TOP SKIN AND C
- [SDR DALA2019012900620](https://openairdocs.org/sdr/DALA2019012900620), Jan 28, 2019: LONGERON. NOT REPORTED. REMOVE LONGERON 25L BETWEEN STA 974/994 (IN REF NRC 00059) FOR SPLICE REPAIR PER SRM 53-00-05-2R-2. LONGERON 25L WAS REPAIRED PER SRM 53-00-05-2R-2. (LP #092251
- [SDR DALA2019012800571](https://openairdocs.org/sdr/DALA2019012800571), Jan 27, 2019: BRACKET. CRACKED. CRACK ON RT SLIDE WINDOW FRAME UPPER AFT CORNER STA 120. NRC 00499: RT SLIDE WINDOW STIFFENER (BRACKET) UPPER AFT CORNER STA 120 WAS REPLACED PER SRM 51-41-01-0
- [SDR DALA2019012800570](https://openairdocs.org/sdr/DALA2019012800570), Jan 27, 2019: FLOOR PANEL. CORRODED. CORROSION ON FLOOR PANEL STA 120 (CPAX). NRC 00514: CORROSION LEVEL 2, FLOOR PANEL STA 120 WAS REPLACED PER DWG #9957828 REV: Y. (UT) ACCOMPLISHED PER NDT 04-00
- [SDR DALA2019012800569](https://openairdocs.org/sdr/DALA2019012800569), Jan 27, 2019: SPLICE. CORRODED. CORROSION TYPE EXFOLIATION ON SPLICE STA Y=898.500 BTW L27R TO L26L AT AFT CARGO COMPARTMENT AMDS 5331-2001. (CCT). NRC 00165: CORROSION LEVEL 2. SPLICE STA Y=8
- [SDR DALA2019012900621](https://openairdocs.org/sdr/DALA2019012900621), Jan 26, 2019: BEAM. CRACKED. CRACK ON RT NLG DOOR JAMB BEAM STA Y=40. (NLG). NRC 00155: RT NLG DOOR JAMB BEAM STA Y=40 WAS REPAIRED PER ER/A 495600-14MA REV. C.(ET)(HFEC) WAS ACCOMPLISHED O

All 215: https://openairdocs.org/aircraft/N950AT/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/N950AT/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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