# N954AT: 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: 55016
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 17, 2000
- Certificate issued: November 27, 2023
- Expires: November 30, 2030
- Mode S code: AD4395
- 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=954AT
- Page: https://openairdocs.org/aircraft/N954AT

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/N954AT/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 N954AT.

## 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.

- [Incident 20060430010269I](https://openairdocs.org/incident/20060430010269I), Apr 30, 2006: Boeing 717200 (N954AT), Atlanta, GA. (-23) Per logpage #782783 capt reported aircraft autopilot disconnected at 13000 feet during descent. Crew had no roll control. Both yokes held firmly. Afs…

## Service difficulty reports (163, 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 DALA2026080604549](https://openairdocs.org/sdr/DALA2026080604549), Aug 6, 2026: ILS SYSTEM. MALFUNCTIONED. ILS 28C STARTED LOSING THE LOCATION INTERMITTENTLY ON THE CAPTAIN`S SIDE ON SHORT FINAL, 1500 THE AUTOPILOT 1 DISCONNECTED UNCOMMON, FO'S FD WENT OFF, SCREEN IN
- [SDR DALA2026073004420](https://openairdocs.org/sdr/DALA2026073004420), Jul 29, 2026: LIGHT. INOPERATIVE. FOUND FWD AISLE LIGHT INOP. R & R AISLE LIGHT PER AMM 33-21. OP CKS GOOD. ACFT OK FOR SVC. (9223777) AIRCRAFT GROUNDED.
- [SDR DALA2025111808425](https://openairdocs.org/sdr/DALA2025111808425), Nov 17, 2025: POWER SUPPLY. FAULTED. EXTERIOR OVERWING EMERGENCY LIGHT WON'T EXTINGUISH. T/S OVERWING EMERGENCY LIGHTS PER B717 FIM 33-50-00-810-801. R & R EMERGENCY LIGHT POWER SUPPLY AT LOC B5-12
- [SDR DALA2023121310203](https://openairdocs.org/sdr/DALA2023121310203), Dec 12, 2023: UNKNOWN. UNKNOWN. SHIP 9513 -MISC/DE- THE CREW DECLARED AN EMERGENCY WHILE IN ICING CONDITIONS IN ORDER TO RAPIDLY DESCEND OUT OF ICING CONDITIONS AFTER RECEIVING A "WING MANIFOL
- [SDR DALA2023100308100](https://openairdocs.org/sdr/DALA2023100308100), Sep 29, 2023: UNKNOWN. UNKNOWN. THE CREW DISCOVERED THAT THE 1L GIRT BAR CABLE WAS DETACHED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART
- [SDR DALA2023080806440](https://openairdocs.org/sdr/DALA2023080806440), Aug 4, 2023: UNKNOWN. UNKNOWN. THE PILOT NOTICED THE 1L DOOR GIRT BAR TETHER STRAP WAS LOOSE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PA
- [SDR DALA2023070705489](https://openairdocs.org/sdr/DALA2023070705489), Jul 6, 2023: UNKNOWN. UNKNOWN. THE MAIN CABIN DOOR GIRT BAR STRAP NOT ATTACHED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MA
- [SDR DALA2023060604562](https://openairdocs.org/sdr/DALA2023060604562), Jun 4, 2023: UNKNOWN. UNKNOWN. AFTER PARKING AT GATE IT WAS DISCOVERED THAT METAL LANYARD AND BRACKET WAS DISCONNECTED FROM FWD MAIN CABIN DOOR SLIDE. THIS WOULD PREVENT PROPER OPERATION OF T
- [SDR DALA2023041302903](https://openairdocs.org/sdr/DALA2023041302903), Apr 11, 2023: UNKNOWN. UNKNOWN. IN REFERANCE TO AMDS 5352-4002: DURING INSTALLATION OF TAILCONE SLIDE, THE RESTRAINT STRAPS WERE FOUND MISSING. THIS COULD PREVENT PROPER OPERATION OF THE ESCAP
- [SDR DALA2023041002742](https://openairdocs.org/sdr/DALA2023041002742), Apr 7, 2023: UNKNOWN. UNKNOWN. CRACK ON FWD PAN NEAR TO BEAM 1 OF AFT CARGO CAMPARTMENT DOOR. (C2) SUMMARY OF NRC 00639: FWD PAN NEAR TO BEAM 1 OF AFT CARGO CAMPARTMENT DOOR (C2) WAS REPAIRED
- [SDR DALA2023041002741](https://openairdocs.org/sdr/DALA2023041002741), Apr 7, 2023: UNKNOWN. UNKNOWN. CORROSION ON WEB OF AFT CUT OUT DOOR JAMB LOWER SECTION AT ENTRY DOOR (L1). SUMMARY OF NRC 00408: CORROSION LEVEL 2. REPAIR ON WEB OF AFT CUT OUT DOOR JAMB LOWE
- [SDR DALA2023041002738](https://openairdocs.org/sdr/DALA2023041002738), Apr 6, 2023: UNKNOWN. UNKNOWN. CRACKED FRAME BTW BEAMS 4 AND 5 AT MAIN ENTRY DOOR. LOCATED JUST ON HANDLE HOUSING AREA. SUMMARY OF NRC 00075: FRAME (INTERCOSTAL) BTW BEAMS 4 AND 5 AT MAIN ENT
- [SDR DALA2023041002737](https://openairdocs.org/sdr/DALA2023041002737), Apr 6, 2023: UNKNOWN. UNKNOWN. CRACKED BEAM #6 (CENTER SECTION) AT MAIN ENTRY DOOR. SUMMARY OF NRC 00077: BEAM #6 (CENTER SECTION) AT MAIN ENTRY DOOR WAS REPAIRED PER B717-200 SRM 51-70-11-2R
- [SDR DALA2023040602681](https://openairdocs.org/sdr/DALA2023040602681), Apr 5, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP ANGLE BTW STA Y=170 TO Y=203 AND X=-60 BELOW SERVICE DOOR SURROUND. SUMMARY OF NRC 00553: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=170 TO Y=203
- [SDR DALA2023033102476](https://openairdocs.org/sdr/DALA2023033102476), Mar 30, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, AFTER TAILCONE SLIDE REMOVAL, IT WAS FOUND UNPACKED. CORRECTIVE ACTION: TAILCONE SLIDE WAS REMOVED P/N: D29984-213 S/N: 1539 PER AMM 25-61-02-000
- [SDR DALA2023032902432](https://openairdocs.org/sdr/DALA2023032902432), Mar 28, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, CORROSION ON INTERCOSTAL STA 814 BTW LONGERON 24 LH TO 23LH AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: INTERCOSTAL STA 814 BTW LONGERON 24 LH T
- [SDR DALA2023032802389](https://openairdocs.org/sdr/DALA2023032802389), Mar 28, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, CRACK ON OVERWING FRAME STA Y=674 LH SIDE AT WING BOX AREA. CORRECTIVE ACTION: OVERWING FRAME STA Y=674 LH WAS REPLACED PER CARD 5310-01436-03A. 
- [SDR DALA2023032802388](https://openairdocs.org/sdr/DALA2023032802388), Mar 27, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CRACK 3EA S BTW STA 1087 AND 1076 ABOVE LONG 14 RH AT EXTERNAL FUSELAGE SKIN. CORRECTIVE ACTION: CRACK 3EA S BTW STA 1087 AND
- [SDR DALA2023032702356](https://openairdocs.org/sdr/DALA2023032702356), Mar 27, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CORROSION AT CUSP ANGLE LOWER SURFACE ON STA=560 TO STA =579 ON FWD CARGO COMPARTMENT RH SIDE. CORRECTIVE ACTION: CUSP ANGLE 
- [SDR DALA2023032702355](https://openairdocs.org/sdr/DALA2023032702355), Mar 27, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, AFTER REMOVAL WEB BTW STA Y=200 TO 208 AND STRINGERS L13 TO L18 CORROSION WAS FOUND AT CUSP ANGLE AT STA Y-200 ON STRINGER L18. CORRECTIVE ACTION
- [SDR DALA2023032602318](https://openairdocs.org/sdr/DALA2023032602318), Mar 25, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON FLOOR SUPPORTS BTW STA Y=148 TO STA Y= 200 AND BTW X=-43 TO X=-54. CORRECTIVE ACTION: FLOOR SUPPORTS BTW STA Y=1
- [SDR DALA2023032602316](https://openairdocs.org/sdr/DALA2023032602316), Mar 24, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON LONGERON END 24RH STA Y 944 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: CLIP ON LONGERON END 24RH STA Y 944 AT 
- [SDR DALA2023032602313](https://openairdocs.org/sdr/DALA2023032602313), Mar 24, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON RH CUSP WEB STA. Y= 198 TO Y=202 (R1) RBL50 AT PASSENGER CABIN. CORRECTIVE ACTION: RH CUSP WEB STA. Y=200 TO Y=2
- [SDR DALA2023032402308](https://openairdocs.org/sdr/DALA2023032402308), Mar 24, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, CORROSION ON DIAPHRAGM STA Y=200 RBL45 - 55 (UNDER R1) VIEW FROM E/E COMPARTMENT. CORRECTIVE ACTION: REPAIR ON DIAPHRAGM STA Y=200 RBL45 - 55 (UN
- [SDR DALA2023032402307](https://openairdocs.org/sdr/DALA2023032402307), Mar 24, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON CUSP WEB TO BTW STA 218 TO STA 237 RH. CORRECTIVE ACTION: CUSP WEB TO BTW STA 218 TO STA 237 RH
- [SDR DALA2023032402306](https://openairdocs.org/sdr/DALA2023032402306), Mar 24, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON ANGLE SUPPORT BTW STA 137 TO STA 160. CORRECTIVE ACTION: ANGLE WAS FABRICATED PER DWG 5910085 R
- [SDR DALA2023032402305](https://openairdocs.org/sdr/DALA2023032402305), Mar 24, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON ANGLE SUPPORT BTW STA 200 TO STA 210. CORRECTIVE ACTION: ANGLE SUPPORT WAS REPLACED PER DRAWING
- [SDR DALA2023032402304](https://openairdocs.org/sdr/DALA2023032402304), Mar 24, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, CORROSION ON FLOOR SUPPORTS BTW STA Y=148 TO STA Y= 200 AND BTW X=-9 TO X=-42. CORRECTIVE ACTION: FLOOR SUPPORTS WERE REPLACED PER DWG 9936534 RE
- [SDR DALA2023032402303](https://openairdocs.org/sdr/DALA2023032402303), Mar 23, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, CRACKS (2EAS) AND ELONGATED HOLES ON LH CUSP WEB BTW STA=656 TO STA=715 AND X=44 TO X=60 AT PAX CABIN. CORRECTIVE ACTION: CUSP WEB BTW STA=656 TO
- [SDR DALA2023032202171](https://openairdocs.org/sdr/DALA2023032202171), Mar 21, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, CRACK ON FITTING ON FWD PAN NEAR TO BEAM 1 OF AFT CARGO COMPARTMENT DOOR WAS FOUND. CORRECTIVE ACTION: FITTING ON FWD PAN NEAR TO BEAM 1 OF AFT C
- [SDR DALA2023032202170](https://openairdocs.org/sdr/DALA2023032202170), Mar 21, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT BTW STA Y= 200 TO STA Y=218 AND X=-11 AT CABIN PAX. CORRECTIVE ACTION: FLOOR SUPPORT BTW STA Y= 20
- [SDR DALA2023032202169](https://openairdocs.org/sdr/DALA2023032202169), Mar 21, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON FRAME BTW STA=1037 BTW LONGERON 17RH AND LONGERON #18RH OF PAX CABIN. CORRECTIVE ACTION: REPAIR WAS PERFORMED PER B7
- [SDR DALA2023032202168](https://openairdocs.org/sdr/DALA2023032202168), Mar 20, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON UPPER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: UPPER PAN ON STA Y 389 AT FWD CARGO COMPARTMEN
- [SDR DALA2023031802045](https://openairdocs.org/sdr/DALA2023031802045), Mar 18, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CORROSION AND CRACK ON LH CUSP WEB (UPPER-LOWER SURFACE) STA. Y= 636 TO Y=655 AT PASSENGER CABIN. CORRECTIVE ACTION: LH CUSP 
- [SDR DALA2023031802044](https://openairdocs.org/sdr/DALA2023031802044), Mar 18, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON INNER AFT PAN ABOVE BEAM 5 AT FWD CARGO DOOR. CORRECTIVE ACTION: INNER AFT PAN ABOVE BEAM 5 AT FWD CARGO DOOR WAS RE
- [SDR DALA2023031802043](https://openairdocs.org/sdr/DALA2023031802043), Mar 17, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON LUGS (FLOOR SUPPORT) STA=147 BTW RBL=30 TO RBL=50 AT COCKPIT. CORRECTIVE ACTION: FLOOR SUPPORT ON STA=147 BTW RB
- [SDR DALA2023031802042](https://openairdocs.org/sdr/DALA2023031802042), Mar 17, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON BEAM NBR 1, (FWD EDGE) OF L1 PASSENGER ENTRANCE DOOR. CORRECTIVE ACTION: ENTRANCE DOOR L1 WAS REPAIRED PER B717-200 
- [SDR DALA2023031802041](https://openairdocs.org/sdr/DALA2023031802041), Mar 17, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CRACK INTERCOSTAL ATTACH LOWER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: INTERCOSTAL ATTACH LOWER PAN S
- [SDR DALA2023031802040](https://openairdocs.org/sdr/DALA2023031802040), Mar 17, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON CLIP ON LOWER PAN SECTION STA Y 389 AT FWD CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: CLIP OF LOWER PAN SECTION STA 
- [SDR DALA2023031702017](https://openairdocs.org/sdr/DALA2023031702017), Mar 17, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CRACKED RH CUSP WEB STA. Y=389 (UNDER SEAT TRACK) AT PASSENGER CABIN. CORRECTIVE ACTION: RH CUSP WEB STA. Y=389 (UNDER SEAT T
- [SDR DALA2023031702016](https://openairdocs.org/sdr/DALA2023031702016), Mar 17, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON CLIP ON LOWER PAN SECTION STA Y 427 AT FWD CARGO COMPARTMENT DOOR. MAINTENANCE ACTION: CLIP ON LOWER PAN SECTION STA
- [SDR DALA2023031702015](https://openairdocs.org/sdr/DALA2023031702015), Mar 16, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON FITTING ATTACH UPPER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR. MAINTENANCE ACTION: UPPER FITTING STA Y 389 WAS RE
- [SDR DALA2023031702008](https://openairdocs.org/sdr/DALA2023031702008), Mar 16, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 9513, INITIAL INSPECTION: CRACKED RH CUSP WEB (2 EA) STA. Y= 655 TO Y=674 AT PASSENGER CABIN. CORRECTIVE ACTION: CUSP WEB RH (2 EA) STA. Y= 655 TO Y=67
- [SDR DALA2023031501886](https://openairdocs.org/sdr/DALA2023031501886), Mar 15, 2023: UNKNOWN. UNKNOWN. IN REF NRC 00485 CORROSION ON RH CUSP WEB BTW STA Y=600 TO Y=615 AT PAX CABIN. SUMMARY OF NRC 00640: CORROSION LEVEL 2. CUSP WEB BTW STA Y=600 TO Y=615 AT PAX C
- [SDR DALA2023031401853](https://openairdocs.org/sdr/DALA2023031401853), Mar 13, 2023: UNKNOWN. UNKNOWN. CRACK ON INTERNAL ANGLE ON AFT PAN MIDDLE SECTION AT LH FWD OVERWING EMERGENCY EXIT DOOR. (PTAS) SUMMARY OF NRC 00073: INTERNAL ANGLE AT LH FWD OVERWING EMERGEN
- [SDR DALA2023031401850](https://openairdocs.org/sdr/DALA2023031401850), Mar 12, 2023: UNKNOWN. UNKNOWN. CRACKED ON FWD PAN OF LH FWD OVERWING EMERGENCY EXIT DOOR. SUMMARY OF NRC 00655: FWD PAN OF LH FWD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER B717-200 SRM 52
- [SDR DALA2023031001759](https://openairdocs.org/sdr/DALA2023031001759), Mar 8, 2023: NONE. NONE. CRACKED RH CUSP WEB BTW STA Y=918-925 AND Y=935-942 AT PASSENGER CABIN. SUMMARY OF NRC 00489: CORROSION LEVEL 2. CUSP WEB RH BTW STA Y=918-925 AND Y=935-942 WAS
- [SDR DALA2022122008239](https://openairdocs.org/sdr/DALA2022122008239), Dec 19, 2022: PSEU. FAILED. SHIP 9513- MISC/DE - WHILE ON APPROACH FOR LANDING THE CREW NOTED THE MASTER CAUTION WITH EICAS MESSAGE OF "PSEU FAIL". WHICH REQUIRED A NO SLAT / NO FLAP LANDI
- [SDR DALA2022031601718](https://openairdocs.org/sdr/DALA2022031601718), Mar 15, 2022: NONE. NONE. DURING CHECK THE OPERATION OF THE EMERGENCY LIGHTING SYSTEM, LEFT AND RIGHT OVER-WING EMERGENCY EXTERIOR LIGHTS DON'T ILLUMINATE IN REFERENCE CARD 0514-2001 STE
- [SDR DALA2023041302904](https://openairdocs.org/sdr/DALA2023041302904), Mar 14, 2022: UNKNOWN. UNKNOWN. ER/A 597798-14, FUSELAGE / SKIN / LH WINDOW BELT PANEL / Y=522-541 / LIGHTNING STRIKE. SUBJECT REPAIR REQUIRES FOLLOW-ON REPETITIVE INSPECTION AND PERMANENT REP

All 163: https://openairdocs.org/aircraft/N954AT/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/N954AT/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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