# N955AT: 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: 55017
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard
- Airworthiness date: November 15, 2000
- Certificate issued: November 21, 2023
- Expires: November 30, 2030
- Mode S code: AD474C
- 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=955AT
- Page: https://openairdocs.org/aircraft/N955AT

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/N955AT/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 DCA23FA339](https://openairdocs.org/ntsb/DCA23FA339), Jun 28, 2023: Boeing 717-200 (N955AT), Charlotte, NC, substantial damage. Probable cause: A fatigue fracture of the upper lock link that initiated along scratch features on the lower surface at the parting line of the forged aluminum component. Contributing to the accident was the…

## 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 20230628013469A](https://openairdocs.org/incident/20230628013469A), Jun 28, 2023: Boeing 717-200 (N955AT), Charlotte, NC, Substantial damage. On June 28, 2023, about 0858 eastern daylight time (EDT), [privacy data omitted], a Boeing 717-200, Sustained substantial damage when the nose landing gear did…

## Service difficulty reports (197, 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 DALA2026101905722](https://openairdocs.org/sdr/DALA2026101905722), Oct 18, 2026: OXYGEN MASK. FAULTED. F/O O2 MASK-SETTINGS DO NOT ALIGN WITH INSIDE INDICATOR IE AT 100% THE INDICATOR READS EMERGENCY, R/R F/O O2 MASK PER B717 AMM 35-13. (9520956) (AIRCRAFT GROUND
- [SDR DALA2026081304644](https://openairdocs.org/sdr/DALA2026081304644), Aug 12, 2026: STRIP. DISCONNECTED. FOUND METAL STRIP DISCONNECTED ON RIGHT WING LEADING EDGE, COMPLIED WITH ER/A 485300- 14. (9085798) (AIRCRAFT GROUNDED).
- [SDR DALA2025032002095](https://openairdocs.org/sdr/DALA2025032002095), Mar 19, 2025: PAN. CRACKED. CRACK ON PAN NEXT TO AFT HINGE DOOR (UPPER AREA) AT FWD CARGO DOOR. SUMMARY OF NRC 00193: PAN NEXT TO AFT HINGE DOOR (UPPER AREA) OF FWD CARGO DOOR WAS REPAIRED
- [SDR DALA2025032002093](https://openairdocs.org/sdr/DALA2025032002093), Mar 19, 2025: PAN. CRACKED. CRACK ON OUTER PAN BTW BEAM 1 AND 2 (AFT EDGE) OF FWD CARGO DOOR WAS FOUND. SUMMARY OF NRC 00552: OUTER PAN AND INNER PAN BTW BEAM #1 AND BEAM #2 (AFT EDGE) AT 
- [SDR DALA2025032002092](https://openairdocs.org/sdr/DALA2025032002092), Mar 19, 2025: PAN. CRACKED. CRACK WAS FOUND ON INNER PAN AT AFT CARGO DOOR AT STOP FITTING ON BEAM 5 AFT EDGE. SUMMARY OF NRC 00577: INNER PAN ON BEAM 5 AFT EDGE OF AFT CARGO DOOR WAS REPA
- [SDR DALA2025031902064](https://openairdocs.org/sdr/DALA2025031902064), Mar 19, 2025: BEAM. CRACKED. CRACK WAS FOUND ON INNER/OUTER PAN BEAM 2 AND INNER PAN BEAM 1 FWD EDGE AT AFT CARGO DOOR. SUMMARY OF NRC 00578: INNER/OUTER PAN BEAM 2 AND INNER PAN BEAM 1 FWD
- [SDR DALA2025031702028](https://openairdocs.org/sdr/DALA2025031702028), Mar 15, 2025: PAN. CRACKED. CRACKS (2 EA) WERE FOUND ON INNER PAN AT AFT CARGO DOOR STOP FITTING ON BEAM 1 STA Y=990. SUMMARY OF NRC 00589: INNER PAN ON AFT SIDE BETWEEN STOP #1 AND STOP #
- [SDR DALA2025031702019](https://openairdocs.org/sdr/DALA2025031702019), Mar 14, 2025: PAN. CRACKED. CRACKS (2 EA) ON OUTER PAN IN BEAM 5 AT AFT CARGO DOOR FWD AND AFT EDGES. SUMMARY OF NRC 00111: DAMAGED AREA OF OUTER PAN IN BEAM 5 AT AFT CARGO DOOR FWD AND AF
- [SDR DALA2025031101890](https://openairdocs.org/sdr/DALA2025031101890), Mar 11, 2025: BEAM. CRACKED. CRACK WAS FOUND ON BEAM 5 AND INNER PAN (FWD EDGE) AT AFT CARGO DOOR. SUMMARY OF NRC 00574: BEAM 5 AND INNER PAN (FWD EDGE) AT AFT CARGO DOOR. WERE REPAIRED PER
- [SDR DALA2025031101888](https://openairdocs.org/sdr/DALA2025031101888), Mar 10, 2025: SKIN. CORRODED. CORROSION ON INNER SKIN PANEL FROM STA Y=657 TO Y=636 BTW L29L AND L29R, STA Y=588 L30 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00183: CORROSION LEVEL 2. INNER 
- [SDR DALA2025030501711](https://openairdocs.org/sdr/DALA2025030501711), Mar 4, 2025: HINGE FITTING. DAMAGED. AN ELONGATED HOLE WAS FOUND AT THE RH WING FLAP HINGE FITTING #3 PIVOT POINT. SUMMARY OF NRC 00535: RH WING FLAP HINGE FITTING #3 WAS REPAIR PER PRI 624272-14 R
- [SDR DALA2025030501710](https://openairdocs.org/sdr/DALA2025030501710), Mar 4, 2025: HINGE FITTING. CORRODED. AN ELONGATED HOLE INBD ON INBD FACE ON HINGE FLAP #3 AT LH WING, ALONG WITH CORROSION ON BOTH HOLES INBD/OUTBD HINGE. SUMMARY OF NRC 00543: HINGE FLAP #3 AT LH 
- [SDR DALA2025030501709](https://openairdocs.org/sdr/DALA2025030501709), Mar 4, 2025: FRAME. CORRODED. CORROSION ON FRAME BTW STA Y=1022 L28L TO L28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00177: CORROSION LEVEL 2. FRAME BTW STA Y=1022 L28L TO L28R AT AFT CARGO
- [SDR DALA2025030401650](https://openairdocs.org/sdr/DALA2025030401650), Mar 3, 2025: SHEAR TIE. CORRODED. FRAME CLIP STA 1022 BTW LONG 28RH TO 28LH, AFT CARGO COMPARTMENT, WAS FOUND CORRODED OUT OF LIMITS WITH MINIMUM REMAINING THICKNESS 0.048 IN PER B717-200 SRM 53
- [SDR DALA2025030301647](https://openairdocs.org/sdr/DALA2025030301647), Feb 28, 2025: ANGLE. CORRODED. CORROSION ON ANGLE CUSP BTW STA Y=197 TO STA Y=210 OF FWD GALLAY SERVICE DOOR AT CABIN PASSENGER. SUMMARY OF NRC 00283: CORROSION LEVEL 2. ANGLE CUSP BTW STA Y=
- [SDR DALA2025030101571](https://openairdocs.org/sdr/DALA2025030101571), Feb 27, 2025: CUSP WEB. CRACKED. CRACK ON CUSP WEB (BELOW AREA) IN X=-54 AND STA 257, STA 277, STA 656, STA 674, STA 818, AND STA 937 AT CPAX. SUMMARY OF NRC 00336: CUSP WEB AT STA 277, STA 257
- [SDR DALA2025022601481](https://openairdocs.org/sdr/DALA2025022601481), Feb 26, 2025: SKIN. DAMAGED. LH ELEVATOR WAS FOUND DENTED AND SCRATCHED ON UPPER SKIN. SUMMARY OF NRC 00575: LH ELEVATOR WAS REPAIRED PER B717-200 SRM 51-70-13-2R REPAIR 2. PERFORM DECAL CO
- [SDR DALA2025022601480](https://openairdocs.org/sdr/DALA2025022601480), Feb 25, 2025: CUSP WEB. CRACKED. CRACK ON CUSP WEBS (LOWER AND UPPER AREA) IN X=54 AND STA 225, STA 237, STA 258, STA 655, AND STA 663. ALSO, X=58 AND STA 668, STA 807 AT CPAX WAS CRACKED. SUMM
- [SDR DALA2025022601479](https://openairdocs.org/sdr/DALA2025022601479), Feb 25, 2025: ANGLE. CORRODED. CORROSION ON ANGLE CUSP BTW STA Y=190 TO STA Y=200 OF FWD ENTRY DOOR AT PASSENGER CABIN. SUMMARY OF NRC 00270: CORROSION LEVEL 2. ANGLE CUSP BTW STA Y=190 TO ST
- [SDR DALA2025022501469](https://openairdocs.org/sdr/DALA2025022501469), Feb 22, 2025: DOOR FRAME. CORRODED. CORROSION ON DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00062: CORROSION LEVEL 2. DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLED PER B717
- [SDR DALA2025022501468](https://openairdocs.org/sdr/DALA2025022501468), Feb 21, 2025: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BTW STA Y=194 TO STA Y=200 X=56 OF FWD ENTRY DOOR AT PASSENGER CABIN. SUMMARY OF NRC 00276: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 
- [SDR DALA2025022101363](https://openairdocs.org/sdr/DALA2025022101363), Feb 21, 2025: WEB. CORRODED. CORROSION OUT OF LIMITS FOUND AT WEB STA 200 TO STA 216 X=25 TO X=54. SUMMARY OF NRC 00492: CORROSION LEVEL 2. WEB STA 200 TO STA 216 X=25 TO X=54 WAS FABRICATE
- [SDR DALA2025022101362](https://openairdocs.org/sdr/DALA2025022101362), Feb 20, 2025: WEB. CORRODED. CORROSION ON WEB BTW STA Y=225 TO STA Y=228 X=56 AT FWD CABIN PASSENGER. SUMMARY OF NRC 00280: CORROSION LEVEL 2. CUSP WEB STA 216 TO 237 X=45 TO X=57 WAS FABRI
- [SDR DALA2025022101359](https://openairdocs.org/sdr/DALA2025022101359), Feb 20, 2025: PAN. CRACKED. CRACK WAS FOUND ON AFT SIDE ON BEAM 4 OUTER PAN AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00508: AFT SIDE ON BEAM 4 OUTER PAN AT FWD COMPARTMENT DOOR WAS RE
- [SDR DALA2025022001286](https://openairdocs.org/sdr/DALA2025022001286), Feb 20, 2025: CUSP WEB. CORRODED. CORROSION ON CUSP WEB, REWORKED AREAS AT X=58 STA 866 AND STA 840-847 WAS FOUND OUT OF LIMITS WITH MINIMUM REMAINING THICKNESS OF 0.010IN PER B717 SRM 53-00-55-
- [SDR DALA2025021801196](https://openairdocs.org/sdr/DALA2025021801196), Feb 18, 2025: SEAT TRACK. CORRODED. CORROSION OUT OF LIMITS IN REF NRC 188: CORROSION ON SIDE TRACK (RH) BWT STA 644 TO 648 SEAT TRACK FLANGE: WITH ORIGINAL THICKNESS =0.060" AND MINIMUM REMAINING
- [SDR DALA2025021401141](https://openairdocs.org/sdr/DALA2025021401141), Feb 13, 2025: CUSP WEB. CRACKED. CRACK ON CUSP WEB BTW STA Y=218/Y=237 AND X-54/X-44 AND CUSP WEB BTW STA Y=200/Y=218 AND X-54/X-24 AT PAX CABIN. SUMMARY OF NRC 00495: CUSP WEB BTW STA Y=218/Y=
- [SDR DALA2025021401140](https://openairdocs.org/sdr/DALA2025021401140), Feb 13, 2025: FRAME. CRACKED. CRACK ON FRAME STA Y=1037, L-17L AND L-17R AT CPAX. SUMMARY OF NRC 00379: FRAME STA Y=1037, L-17L AND L-17R AT CPAX WERE REPAIRED PER B717-200 SRM 53-20-07-2R P
- [SDR DALA2025021401139](https://openairdocs.org/sdr/DALA2025021401139), Feb 13, 2025: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORTS (3 EA) BTW STA Y=1022 TO STA Y=1074 AND -X=44 TO -X=56 AT AFT PASSENGER CABIN (W2). SUMMARY OF NRC 00271: CORROSION LEVEL 2. CORRODE
- [SDR DALA2025021401138](https://openairdocs.org/sdr/DALA2025021401138), Feb 12, 2025: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BTW STA Y=1022 TO STA Y=1074 AND X=44 AT AFT PASSENGER CABIN (W2). SUMMARY OF NRC 00275: CORROSION LEVEL 2. CORRODED FLOOR SUPPORT BT
- [SDR DALA2025021001045](https://openairdocs.org/sdr/DALA2025021001045), Feb 7, 2025: PAN. CRACKED. CRACK WAS FOUND ON INNER PAN OF THE AFT EDGE AT FWD CARGO DOOR. SUMMARY OF NRC-00306: AFT EDGE AT FWD CARGO DOOR CRACK ON INNER PAN WAS REPAIRED PER B717-200 SR
- [SDR DALA2024032803862](https://openairdocs.org/sdr/DALA2024032803862), Mar 27, 2024: DRAIN. CRACKED. CRACK ON DRAIN OF LH CLEAR VIEW WINDOW AT COCKPIT. SUMMARY OF NRC 00080: LH CLEAR VIEW WINDOW RETAINER AT COCKPIT WAS REPAIRED PER ERA 616781-14 REV ORIGINAL. A
- [SDR DALA2024022102374](https://openairdocs.org/sdr/DALA2024022102374), Oct 25, 2023: TRUNNION. CORRODED. RMLG FIXED STRUT OB ATTACH POINT BORE BUSHING CORRODED. REPLACED BUSHING PER BOEING DWG 5924841 ON NRC 008. (LP #0033263)
- [SDR DALA2023091407536](https://openairdocs.org/sdr/DALA2023091407536), Sep 13, 2023: UNKNOWN. UNKNOWN. LWR FRAME SECTION STA 120 DAMAGED DURING LANDING. C/W PRI 610432-14 REV 0. C/W PRI 610432-14 REV 1. C/W PRI 610432-14 REV 2. C/W PRI 610432-14 REV 3. C/W PRI 61
- [SDR DALA2023091207455](https://openairdocs.org/sdr/DALA2023091207455), Sep 10, 2023: UNKNOWN. UNKNOWN. LHS NLG SUPPORT BEAM DAMAGED ON LANDING. REMOVED DAMAGED NLG SUPPORT BEAM PER BOEING DWG 9910088. REPLACED NLG SUPPORT BEAM PER BOEING DWG 9910088. (LP #2963209
- [SDR DALA2023090507180](https://openairdocs.org/sdr/DALA2023090507180), Aug 31, 2023: UNKNOWN. UNKNOWN. LOWER SKIN PANEL ASSY 5911401-537 DAMAGED DRUING LANDING. REMOVED -537 SKIN ASSY PER DWG 5911401. LOCATED AND DRILLED NEW SKIN ASSY PER DWG 5911401. APPLIED TOP
- [SDR DALA2023082907002](https://openairdocs.org/sdr/DALA2023082907002), Aug 28, 2023: UNKNOWN. UNKNOWN. LOWER FRAME SECTION AT STA 160 DAMAGED DURING LANDING. (REF PAPER NR 012) REMOVED LOWER FRAME SECTION STA 160 PER B717 SRM 51-40-02. C/W REV 0 OF PRI 610940-14.
- [SDR DALA2023082506912](https://openairdocs.org/sdr/DALA2023082506912), Aug 24, 2023: UNKNOWN. UNKNOWN. C/W ERA 610811-14 INTERNAL DOUBLER FABRICATION DAMAGED DURING LANDING. C/W PRI 610811-14 REV 0. C/W ERA 610811-14 REV ORIG. PRI REV 0 MATCHES FINAL ERA. (LP #29
- [SDR DALA2023081806720](https://openairdocs.org/sdr/DALA2023081806720), Aug 16, 2023: UNKNOWN. UNKNOWN. LH NLG SKIN PANEL 5911400-99 DAMAGED DURING LANDING. REF NR 066: C/W PRI 610190-14 REV 0. C/W PRI 610190-14 REV 1. C/W PRI 610190-14 REV 2. C/W PRI 610190-14 RE
- [SDR DALA2023081606675](https://openairdocs.org/sdr/DALA2023081606675), Aug 15, 2023: UNKNOWN. UNKNOWN. -39 AND -22 CHORDS AT STA 110 BULKHEAD DAMAGED DURING LANDING. REMOVED DAMAGED PORTION OF -39 AND -22 CHORDS PER B717 SRM 51-70 -11-2R-2. FABRICATED NEW -22 SEC
- [SDR DALA2023081606674](https://openairdocs.org/sdr/DALA2023081606674), Aug 15, 2023: UNKNOWN. UNKNOWN. RHS NLG SUPPORT BEAM WAS DAMAGED ON LANDING. C/W PRI 610297-14 REV 0. C/W PRI 610297-14 REV 1. C/W ERA 610297-14 REV ORIG. PRI REVS 0 AND 1 MATCH FINAL ERA. (LP
- [SDR DALA2023081606673](https://openairdocs.org/sdr/DALA2023081606673), Aug 15, 2023: UNKNOWN. UNKNOWN. E&E DOOR SURROUND JAMB PAN AND SUPPORT FRAMES DAMAGED DURING LANDING. REMOVED E&E DOOR SURROUND JAMB PAN PER B717 SRM 51-40-02. INSTALLED E&E JAMB PAN AND SUPPO
- [SDR DALA2023081606672](https://openairdocs.org/sdr/DALA2023081606672), Aug 15, 2023: UNKNOWN. UNKNOWN. STA 110 BULKHEAD AND LWR CHORD DAMAGED DURING LANDING. REMAINING SECTIONS OD ST110 CHORD REMOVED. REMOVED DAMAGE SECTION OF BULKHEAD PER B717 SRM 53-10-08-2R RE
- [SDR DALA2023081606671](https://openairdocs.org/sdr/DALA2023081606671), Aug 15, 2023: UNKNOWN. UNKNOWN. LONGERON AT STA 160-STA 180 STR 30 DAMAGED DURING LANDING. REMOVED LONGERON AT STA 160 - STA 180 STR 30 PER B717 SRM 51-40- 02. REPLACED LONGERON AFT STA 160- S
- [SDR DALA2023081606670](https://openairdocs.org/sdr/DALA2023081606670), Aug 15, 2023: UNKNOWN. UNKNOWN. SEVEN LONGERONS STA 110-120 STR 28L-28R WERE DAMAGED DURING LANDING. (REF BUFF NR 010) LOCATED AND DRILLED LONGERON SECTIONS PER B717 DWG 5911401. INSTALLED 7 E
- [SDR DALA2023072505984](https://openairdocs.org/sdr/DALA2023072505984), Jul 24, 2023: UNKNOWN. UNKNOWN. LOWER FRAME SECTION STA 132 WAS DAMAGED DURING LANDING. MAINTENANCE REMOVED LOWER FRAME SECTION PER B717 SRM 51-40-02. LOCATED AND DRILLED NEW SPLICES PER B717 
- [SDR DALA2023063005265](https://openairdocs.org/sdr/DALA2023063005265), Jun 28, 2023: UNKNOWN. UNKNOWN. SHIP 9514 -GEAR/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC AFTER NOT BEING ABLE TO EXTINGUISH THE "NLG UNSAFE" INDICATION ON APPROACH. THE QRH WAS COMPL
- [SDR DALA2023040402601](https://openairdocs.org/sdr/DALA2023040402601), Mar 29, 2023: UNKNOWN. UNKNOWN. WHILE REMOVING CEILING PANELS MAINTENANCE FOUND A BROKEN EMERGENCY LIGHT WIRE. THE WIRE WAS REPAIRED PER SWPM 20-30. THE OPERATIONAL CHECK WAS GOOD. (LP #402535
- [SDR DALA2023022201327](https://openairdocs.org/sdr/DALA2023022201327), Feb 18, 2023: NONE. NONE. FOUND OVER WING INTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE #7 EMERGENCY LIGHT BATTERY POWER SUPPLY, LOCATION 685R, PER B717 AMM 33-51. OPER
- [SDR DALA2022040602329](https://openairdocs.org/sdr/DALA2022040602329), Apr 3, 2022: FRAME. CRACKED. FRAME AT STA Y1116 AND STR R11 CRACKED. REMOVED DAMAGED AREA PER B717SRM 53-00-07-2R-1. FABRICATED & INSTALLED REPAIR PARTS IAW B717 SRM53-00-07-2R-1. (LP #2182

All 197: https://openairdocs.org/aircraft/N955AT/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/N955AT/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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