# N957AT: 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: 55019
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 16, 2000
- Certificate issued: December 18, 2023
- Expires: December 31, 2030
- Mode S code: AD4EBA
- 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=957AT
- Page: https://openairdocs.org/aircraft/N957AT

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/N957AT/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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB NYC03FA067](https://openairdocs.org/ntsb/NYC03FA067), Mar 27, 2003: Boeing 717-200 (N957AT), Flushing, NY, minor damage. Probable cause: A failure of the left power control distribution unit (PCDU).

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20030326025189A](https://openairdocs.org/incident/20030326025189A), Mar 26, 2003: Boeing 717200 (N957AT), New York, NY, Minor damage. (-23) Airtran flt 356 made an emergency landing at la-Guardia airport due to smoke in the cockpit and cockpit display units in flight deck blinking on and off.…

## Service difficulty reports (187, 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 DALA2026021801178](https://openairdocs.org/sdr/DALA2026021801178), Feb 17, 2026: HYDRAULIC LINE. LEAKING. ATB, THE FLIGHT CREW PERFORMED AN AIR TURNBACK DUE TO A RIGHT HYDRAULIC SYSTEM QUANTITY LOW MESSAGE. MAINTENANCE FOUND A LT MAIN LANDING GEAR HYDRAULIC LINE LEA
- [SDR DALA2025081105989](https://openairdocs.org/sdr/DALA2025081105989), Aug 7, 2025: FRAME. DAMAGED. SHIP 9516 FRAME AND FASTENERS DAMAGED AT 6 O'CLOCK POSITION ON CANTED. CORECTIVE ACTION: COMPLIED WITH ER/A 627973-14 (1130003)
- [SDR DALA2025080205797](https://openairdocs.org/sdr/DALA2025080205797), Jul 27, 2025: PAN. CORRODED. SEVERAL AREAS OF CORROSION AROUND FASTENES. REPLACED FORWARD CARGO DOOR LOWER JAMB PAN IAW B717-200 SRM 53- 20-15-2R (1108952)
- [SDR DALA2025080205798](https://openairdocs.org/sdr/DALA2025080205798), Jul 27, 2025: PIN. COCKED. TAIL CONE RELEASE CAM PIN CLOCKED INCORRECTLY. ADDED WASHERS AND SHIMS WHICH WAS MISSING FROM THE TAIL CONE RELEASE CAM PIN TO CORRECT EXCESSIVE FORWARD AND AFT
- [SDR DALA2025061504507](https://openairdocs.org/sdr/DALA2025061504507), Jun 13, 2025: COMPRESSOR. STALLED. SHIP 9516 - DIV - DIVERSION TO ORD DUE TO LEFT ENGINE COMPRESSOR STALL ON CLIMB. CORRECTIVE ACTION: PERFORMED BORESCOPE INSPECTION AND FOUND SEVERAL HPC BLADES 
- [SDR DALA2025030401652](https://openairdocs.org/sdr/DALA2025030401652), Mar 1, 2025: PCDU. FAULTED. SHIP 9516 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC FOLLOWING A "RIGHT DC BUS FAILURE" INDICATION. THE RESULT OF THAT WAS A NO FLAP, NO SLAT LAND
- [SDR DALA2024103010506](https://openairdocs.org/sdr/DALA2024103010506), Oct 30, 2024: BATTERY PACK. INOPERATIVE. THE OVERWING EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EXIT LIGHT BATTERY PACK PER B717 AMM 33-51. THE AIRCRAFT IS OK FOR SERVICE. (LP #67031
- [SDR DALA2024080507766](https://openairdocs.org/sdr/DALA2024080507766), Aug 3, 2024: POWER SUPPLY. NO TEST. DURING SERVICE CHECK, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE FROM THE FLIGHT ATTENDANT PANEL. MAINTENANCE FOUND THAT THE CABIN EMERGENCY LIGHTS WOULD
- [SDR DALA2024072407443](https://openairdocs.org/sdr/DALA2024072407443), Jul 23, 2024: CIRCUIT BREAKER. TRIPPED. SHIP 9516 -MISC/DE- THE "DC R BUS OFF" WARNING ILLUMINATED IN CRUISE FLIGHT, ALONG WITH MANY OTHER ASSOCIATED MESSAGES. THE FLIGHT CREW DECLARED AN EMERGENCY IN
- [SDR DALA2024040504129](https://openairdocs.org/sdr/DALA2024040504129), Apr 3, 2024: BATTERY. INOPERATIVE. TAIL CONE INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND POWERPACK REF B717 AMM 33-51-04. OPERATIONAL CHECK WAS GO
- [SDR DALA2024040404052](https://openairdocs.org/sdr/DALA2024040404052), Apr 3, 2024: BATTERY. INOPERATIVE. ON SERVICE CHECK, FOUND AFT OVERWUNG EXIT SIGNS ABOVE DOOR TO BE INOPERATIVE. MAINTENANCE FOUND THE BATTERY CASE CRACKED. INSTALLED NEW BATTERY IAW B717 AMM 33-
- [SDR DALA2024010210751](https://openairdocs.org/sdr/DALA2024010210751), Dec 27, 2023: UNKNOWN. UNKNOWN. GOUGES FOUND AT FUSELAGE BELLY SKIN FOR #1 RAD ALT TRANS ANTENNA. SUMMARY NRC 003-0001:0514-2001/001 00011: C/W ERA 614660-14 REV ORIG REPAIR INSTRUCTIONS. CHEC
- [SDR DALA2023122110466](https://openairdocs.org/sdr/DALA2023122110466), Dec 20, 2023: UNKNOWN. UNKNOWN. AFT OVERWING EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SE
- [SDR DALA2023081106541](https://openairdocs.org/sdr/DALA2023081106541), Aug 10, 2023: UNKNOWN. UNKNOWN. CRACK ON DOOR BEAM #1 STA Y=198 AT PASSENGER ENTRANCE DOOR L1. SUMMARY OF NRC 00141: DOOR BEAM #1 STA Y=198 AT PASSENGER ENTRANCE DOOR L1 WAS REPAIRED PER B717-
- [SDR DALA2023081006498](https://openairdocs.org/sdr/DALA2023081006498), Aug 9, 2023: UNKNOWN. UNKNOWN. OUTER EMERGENCY TAILCONE HANDLE IS ARMED INCORRECTLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.70
- [SDR DALA2023080806439](https://openairdocs.org/sdr/DALA2023080806439), Aug 7, 2023: UNKNOWN. UNKNOWN. CORROSION ON INTERCOSTAL (2 EA) BTW LONGERON 22 AND 21 LH FROM FRAME 1037 TO 1058 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00201: CORROSION LEVEL 2. INTERCOSTAL
- [SDR DALA2023080806438](https://openairdocs.org/sdr/DALA2023080806438), Aug 7, 2023: UNKNOWN. UNKNOWN. CORROSION DAMAGE TO INTERNAL SKIN BETWEEN LONGERON 21-22L, FRAMES Y1037- Y1058 AT AFT CARGO COMPARTMENT, DAMAGE IS ESTIMATED TO EXCEED THE ALLOWABLE LIMITS. SUM
- [SDR DALA2023080806436](https://openairdocs.org/sdr/DALA2023080806436), Aug 4, 2023: UNKNOWN. UNKNOWN. WEAR ON FWD/AFT LATCH FITTINGS AT AFT CARGO DOOR. SUMARY OF NRC 00135: THE LATCH FITTINGS AT AFT/FWD AT AFT CARGO DOOR WERE REPLACED PER BOEING CMM 52-30-2. (LP
- [SDR DALA2023080406295](https://openairdocs.org/sdr/DALA2023080406295), Aug 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME STA 1037 BETWEEN LONGERON 24 TO LONGERON 21 LH AT AFT CARGO COMPARTMENT IS OUT LIMITS WITH 0.040 IN PER B717-200 SRM 53-00-00-1A ALLOWABLE DA
- [SDR DALA2023080306280](https://openairdocs.org/sdr/DALA2023080306280), Aug 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON STRINGERS 22L, 23L, 24L, 26L, AND 27L FROM STA Y=898.5 TO Y=STA 1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00667: CORROSION LEVEL 2. STRINGERS 2
- [SDR DALA2023080206248](https://openairdocs.org/sdr/DALA2023080206248), Aug 1, 2023: UNKNOWN. UNKNOWN. CORROSION ON LONGERONS END (28 Y 27) LH AND LONGERONS END (23 Y 26) LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00641: CORROSION LEVEL 2. LONGERONS END (28,27,2
- [SDR DALA2023080206247](https://openairdocs.org/sdr/DALA2023080206247), Jul 31, 2023: UNKNOWN. UNKNOWN. CORROSION WAS FOUND ALONG FRAME SPLICE REPAIR AT STA 908 BTW L29-L AND L29 -R. SUMMARY OF NRC 00561: CORROSION LEVEL 2. REPAIR SPLICE AT FRAME STA 908 BTW LONGE
- [SDR DALA2023080106208](https://openairdocs.org/sdr/DALA2023080106208), Jul 31, 2023: UNKNOWN. UNKNOWN. CORROSION ON LON-30, LON-28L, AND LON-29L BTW STA 905 TO STA 1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00158: CORROSION LEVEL 2. LON-30, LON-28LH, AND LON-2
- [SDR DALA2023080106207](https://openairdocs.org/sdr/DALA2023080106207), Jul 31, 2023: UNKNOWN. UNKNOWN. CORROSION ON ANGLE OF FRAME BTW LON 27R TO LON 28L STA 908 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00161: CORROSION LEVEL 2. ANGLE OF FRAME BTW LONG 26L TO LON
- [SDR DALA2023080106204](https://openairdocs.org/sdr/DALA2023080106204), Jul 30, 2023: UNKNOWN. UNKNOWN. CORROSION WAS FOUND ALONG FRAME SPLICE REPAIR AT STA 927 BTW L26-L AND L26-R. SUMMARY OF NRC 00560: CORROSION LEVEL 2. FRAME SPLICE REPAIR AT STA 927 BTW L26-L 
- [SDR DALA2023080106203](https://openairdocs.org/sdr/DALA2023080106203), Jul 29, 2023: UNKNOWN. UNKNOWN. CORROSION WAS FOUND ON LONGERON 22LH END FORWARD SECTION AT STA Y=1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00679: CORROSION LEVEL 2. LONGERON END 22LH WAS 
- [SDR DALA2023080106202](https://openairdocs.org/sdr/DALA2023080106202), Jul 29, 2023: UNKNOWN. UNKNOWN. CORROSION ON ANGLE BTW LONGERON 29 RH TO 28 LH AND FRAME 950 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00233: CORROSION LEVEL 2. ANGLE BTW LONGERON 29 RH TO 28 L
- [SDR DALA2023072806112](https://openairdocs.org/sdr/DALA2023072806112), Jul 27, 2023: UNKNOWN. UNKNOWN. DISBOND ON RUDDER TAB LH SIDE OF 1.7000IN LENGTH X 0.500IN WIDTH AT DENT #2, (9" ABOVE #2 HINGE 3"AFT L/E RUDDER TAB) IN REF MON JOB 029-0001, LOG 1488874. SUMM
- [SDR DALA2023072706097](https://openairdocs.org/sdr/DALA2023072706097), Jul 26, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME CLIP BTW LONGERON 26LH TO 26 RH STA Y=1022 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00710: CORROSION LEVEL 2. FRAME CLIP STA Y=1022 BTW STR 2
- [SDR DALA2023072505978](https://openairdocs.org/sdr/DALA2023072505978), Jul 22, 2023: UNKNOWN. UNKNOWN. CORROSION ON LOWER CUTOUT BTW FRAME 990 TO 950 AFT DOOR CARGO. SUMMARY OF NRC 00240: CORROSION LEVEL 2. LOWER DOOR JAMB WAS REPLACED PER B-717-200 SRM 51-41-02-
- [SDR DALA2023072105927](https://openairdocs.org/sdr/DALA2023072105927), Jul 20, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR PANELS 222XF, 222NF, 223EF, 221SF, 221XF, 222HF, 222MF, 223AF, 222AQF, 222AWF, 222AJF, 222ASF, 222ZF, 222ALF, AND 222EF AT PASSENGER CABIN. S
- [SDR DALA2023072505975](https://openairdocs.org/sdr/DALA2023072505975), Jul 19, 2023: UNKNOWN. UNKNOWN. CORROSION ON TRACK BTW FRAME 950 TO 884 RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00242: CORROSION LEVEL 2. TIE TRACK BTW FRAME 884 TO 950 RH AT AFT CARGO COM
- [SDR DALA2023072105920](https://openairdocs.org/sdr/DALA2023072105920), Jul 19, 2023: UNKNOWN. UNKNOWN. CORROSION ON AFT CARGO DOOR JAMB LOWER PAN SPLICE BTW STA 954 TO 994 AND L-27R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00563: CORROSION LEVEL 2. AFT CARGO DOOR
- [SDR DALA2023072105919](https://openairdocs.org/sdr/DALA2023072105919), Jul 19, 2023: UNKNOWN. UNKNOWN. CORROSION ON ANGLE OF FRAME STA 927 BTW L29R TO L27L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00166: CORROSION LEVEL 2. ANGLE OF FRAME STA 927 BTW L29R TO L27L 
- [SDR DALA2023072105922](https://openairdocs.org/sdr/DALA2023072105922), Jul 19, 2023: UNKNOWN. UNKNOWN. CORROSION ON TRACKS RBL16 AND LBL16 BTW STA 810 TO STA 895 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00167: CORROSION LEVEL 2. TIE TRACKS RBL16 AND LBL16 BTW STA
- [SDR DALA2023072105921](https://openairdocs.org/sdr/DALA2023072105921), Jul 19, 2023: UNKNOWN. UNKNOWN. CORROSION ON TRACK BTW FRAME 1022 TO 884 LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00241: CORROSION LEVEL 2. TIE TRACK BTW FRAME 884 TO 1022LH AT AFT CARGO CO
- [SDR DALA2023071905862](https://openairdocs.org/sdr/DALA2023071905862), Jul 18, 2023: UNKNOWN. UNKNOWN. CORROSION ON SPLICE (4 EA) BTW FRAME 990 TO 950 FROM LONGERON 30 AND 27 LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00227: CORROSION LEVEL 2. SPLICE (4 EA) L-28
- [SDR DALA2023071405738](https://openairdocs.org/sdr/DALA2023071405738), Jul 14, 2023: UNKNOWN. UNKNOWN. CORROSION ON GIRT BAR FITTINGS AT R1 DOOR. SUMMARY OF NRC 00691: CORROSION LEVEL 2. GIRT BAR FITTINGS (2 EA) WERE REPLACED PER B717 SRM 51-40-08-0G. (LP #286512
- [SDR DALA2023071405737](https://openairdocs.org/sdr/DALA2023071405737), Jul 13, 2023: UNKNOWN. UNKNOWN. AFTER LONGERON 26 LH BTW STA Y=900 TO STA Y=1053 REMOVAL, CORROSION WAS FOUND AT FUSELAGE SKIN BTW STA 1000 TO STA 1006 L-26 LH. SUMMARY OF NRC 00688: CORROSION
- [SDR DALA2023071405736](https://openairdocs.org/sdr/DALA2023071405736), Jul 13, 2023: UNKNOWN. UNKNOWN. CORROSION ON TRIM PANELS (2 EA) FROM SERVICE DOOR STA Y=148 - Y=200. SUMMARY OF NRC 00472: CORROSION LEVEL 2. TRIM PANELS (2 EA) FROM SERVICE DOOR STA Y=148 - Y
- [SDR DALA2023071205664](https://openairdocs.org/sdr/DALA2023071205664), Jul 11, 2023: UNKNOWN. UNKNOWN. CORROSION ON WEBS BTW STA Y=148/218 AND BTW STA X=-60/60 AT PAX CABIN (W1). SUMMARY OF NRC 00373: CORROSION LEVEL 2. WEB STA Y=158/200 AND BTW X=-3.5/-60 AND Y=
- [SDR DALA2023071205660](https://openairdocs.org/sdr/DALA2023071205660), Jul 8, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP ANGLE BTW STA Y=158/171 APROX, BTW STA Y=195/207 APROX AND BTW RBL=54/60 AT PAX CABIN (W1). SUMMARY OF NRC 00413: CORROSION LEVEL 2. CUSP ANGL
- [SDR DALA2023070705488](https://openairdocs.org/sdr/DALA2023070705488), Jul 7, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAMES STA=680 AND 715 AND LONGERON 26RH UNDER WING BARREL KEEL BEAMS AND CANTED KEEL INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00291: FRAMES STA=680
- [SDR DALA2023070605438](https://openairdocs.org/sdr/DALA2023070605438), Jul 5, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS BTW STA Y=197/158 AND LBL=54 AND FLOOR SUPPORTS STA Y=200 AND BTW RBL=44/54 AT PAX CABIN WERE FOUND OUT OF LIMITS (W1). SUMMARY OF N
- [SDR DALA2023070605437](https://openairdocs.org/sdr/DALA2023070605437), Jul 5, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS STA Y=197 AND BTW LBL=15/43 WAS FOUND OUT LIMITS AT PAX CABIN (W1). SUMMARY OF NRC 00677: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=197
- [SDR DALA2023070505393](https://openairdocs.org/sdr/DALA2023070505393), Jul 4, 2023: UNKNOWN. UNKNOWN. FLOOR SUPPORT STA Y=200 LBL=6 WAS FOUND CORRODED OUT OF LIMITS AT PAX CABIN (W1). SUMMARY OF NRC 00678: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 LBL=6 TO RBL=
- [SDR DALA2023070305310](https://openairdocs.org/sdr/DALA2023070305310), Jul 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON LONGERON END 24 RH BTW FRAME 1022 TO 1002 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00212: CORROSION LEVEL 2. LONGERON END 24 RH BTW STA Y=1022-Y=10
- [SDR DALA2023070305307](https://openairdocs.org/sdr/DALA2023070305307), Jul 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR SUPPORTS BTW STA Y=158/200 AND RBL=44, STA Y=179 AND BTW RBL=8/43, STA Y=200 AND BTW RBL=8/44. SUMMARY OF NRC 00604: CORROSION LEVEL 2. FLOOR
- [SDR DALA2023070305299](https://openairdocs.org/sdr/DALA2023070305299), Jun 30, 2023: UNKNOWN. UNKNOWN. CORROSION ON SEAT TRACK -X=22.0 BTW STA Y=200 TO STA Y=270. SUMMARY OF NRC 00603: CORROSION LEVEL 2. SEAT TRACK SECTION X=-22.0 BTW STA Y=200 TO STA Y=270 WAS R
- [SDR DALA2023063005263](https://openairdocs.org/sdr/DALA2023063005263), Jun 30, 2023: UNKNOWN. UNKNOWN. SEVERAL CRACKS ON CUSP WEB LH SIDE LOWER SIDE STA Y=586 BTW X=+60 AT PAX CAB. SUMMARY OF NRC 00520: CUSP WEB LH STA 579 TO STA 598 WAS FABRICATED PER B717-200 S

All 187: https://openairdocs.org/aircraft/N957AT/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/N957AT/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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