# N953AT: 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: 55015
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 11, 2000
- Certificate issued: November 28, 2023
- Expires: November 30, 2030
- Mode S code: AD3FDE
- 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=953AT
- Page: https://openairdocs.org/aircraft/N953AT

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/N953AT/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 N953AT.

## FAA accident and incident reports

None matched to N953AT.

## Service difficulty reports (137, 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 DALA2026090905048](https://openairdocs.org/sdr/DALA2026090905048), Sep 9, 2026: OXYGEN MASK. INOPERATIVE. FO'S OXYGEN MASK HARNESS DOES NOT INFLATE, R & R HARNESS PER AMM 35-12. (9096980) (AIRCRAFT GROUNDED).
- [SDR DALA2025060604346](https://openairdocs.org/sdr/DALA2025060604346), Jun 5, 2025: DOOR. OPEN. SHIP 9512 -ATB/GEAR- RETURNED MSP DUE TO RUMBLING NOISE IN NOSE GEAR AREA AFTER GEAR RETRACTION. GEAR CYCLED BACK DOWN SHOWING LOCKED WITH 3 GREEN. NLG DOORS FO
- [SDR DALA2025060604343](https://openairdocs.org/sdr/DALA2025060604343), Jun 1, 2025: BATTERY PACK. INOPERATIVE. SHIP 9512 DURING SVC CHK FOUND ENERGENCY LIGHTS SEAT ROW 25 TO AFT OF CABIN INOP. T/S REF B717 SSM 33-51 REPLACED BATTERY PACK B5-231 REF B717 AMM 33-51. CHECKS
- [SDR DALA2024061105984](https://openairdocs.org/sdr/DALA2024061105984), Jun 8, 2024: DOUBLER. DAMAGED. RT WING LE REFUEL PANEL DOOR CUTOUT JAMB DOUBLER DAMAGED AT BOTH CENTER LATCH LAND LOCATIONS. CUTOUT DAMAGED AT BOTH CENTER LATCH LAND LOCATIONS PER B717 SRM 57
- [SDR DALA2024061005958](https://openairdocs.org/sdr/DALA2024061005958), Jun 8, 2024: DOOR. BENT. ON ARRIVAL FOUND FUEL SELECTOR PANEL DOOR BENT OPEN. DAMAGE TO THE SLAT SEAL, DAMAGE TO FUEL SELECTOR PANEL, AND DAMAGE TO THE GUARDED SWITCHES. ALL REFUEL ASSO
- [SDR DALA2024011500580](https://openairdocs.org/sdr/DALA2024011500580), Jan 14, 2024: UNKNOWN. UNKNOWN. DURING SERVICE CHECK, MAINTENANCE FOUND THE FORWARD OVERWING EXIT LIGHT AND ISLE OVERWING EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED 2 EACH BATTERIES, A
- [SDR DALA2023061504881](https://openairdocs.org/sdr/DALA2023061504881), Jun 11, 2023: UNKNOWN. UNKNOWN. AT CRUISE, MULTIPLE SPARKS ON CENTER WINDSHIELD AND CRACK FORMED. TURNED ANTI-ICE OFF PER QRH PROCEDURE. REMOVED CENTER WINDSHIELD IAW B717 AMM 56-11-01. REPLAC
- [SDR DALA2023042003112](https://openairdocs.org/sdr/DALA2023042003112), Apr 19, 2023: UNKNOWN. UNKNOWN. SHIP 9512 -HYD/DE- THE RIGHT HYDRAULIC SYSTEM EXPERIENCED A COMPLETE LOSS OF FLUID WHILE ON APPROACH FOR LANDING. THE CREW DECLARED AN EMERGENCY WITH ATC AND TH
- [SDR DALA2023031802046](https://openairdocs.org/sdr/DALA2023031802046), Mar 17, 2023: UNKNOWN. UNKNOWN. SHIP 9512 - MISC/HYD - DECLARED EMERGENCY FOR THE RIGHT HYDRAULIC SYSTEM QUANTITY DROPPING. CORRECTIVE ACTION: FOUND RUDDER LIMITER ACTUATOR LINE LEAKING. FOUND
- [SDR DALA2023040402603](https://openairdocs.org/sdr/DALA2023040402603), Mar 16, 2023: UNKNOWN. UNKNOWN. SHIP 9512 -HYD/MISC- THE FLIGHT CREW DECLARED AN EMERGENCY FOLLOWING THE ILLUMINATION OF THE "RIGHT HYD LO" MESSAGE AND THE RIGHT HYDRAULIC SYSTEM QUANTITY DROP
- [SDR DALA2023022001260](https://openairdocs.org/sdr/DALA2023022001260), Feb 17, 2023: NONE. NONE. SHIP 9512 -ATB/GEAR/DE- DURING CLIMB OUT AFTER TAKEOFF, THE RIGHT MAIN LANDING GEAR "UNSAFE" LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE CREW COMPLIED
- [SDR DALA2023011800364](https://openairdocs.org/sdr/DALA2023011800364), Jan 17, 2023: STRUCTURE. CRACKED. DURING PRESSURE SEAL REMOVAL, CRACK WAS FOUND ON PASSENGER DOOR FWD UPPER CORNER. PASSENGER DOOR FWD WAS REPLACED FOR THE SERVICIABLE DOOR AND A NEW BRACKET WAS
- [SDR DALA2023011700313](https://openairdocs.org/sdr/DALA2023011700313), Jan 16, 2023: SKIN. CRACKED. CRACK ON FWD SKIN PAN UPPER CORNER SIDE AT AFT CARGO COMPARTMENT DOOR (PTAS). SKIN PAN UPPER CORNER SIDE AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 604
- [SDR DALA2023011000171](https://openairdocs.org/sdr/DALA2023011000171), Jan 8, 2023: FRAME. CRACKED. CRACK ON FRAME STA Y=674, 696, & 715 BTW RH LONG 26 AND 28 AT CANTED KEEL. SUMMARY OF NRC 00332: FRAMES ON STA Y=674, 696, & 715 BTW RH LONG 26 AND 28 AT CANTED
- [SDR DALA2023011000169](https://openairdocs.org/sdr/DALA2023011000169), Jan 8, 2023: FLOORBEAM. CORRODED. CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=-9 AND X=-46 (CPAX)(W1). SUMMARY OF NRC 00334: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 BTW X=-9 AND X=-46 WAS REPL
- [SDR DALA2023011000168](https://openairdocs.org/sdr/DALA2023011000168), Jan 7, 2023: FRAME. CRACKED. CRACK ON FRAME BS 674, 696, & 715 BTW LH LONG 26 AND 28 AT CANTED KEEL. SUMMARY OF NRC 00331: FRAMES ON STA Y=674, 696, & 715 BTW LH LONG 26 AND 28 AT CANTED KE
- [SDR DALA2023010308523](https://openairdocs.org/sdr/DALA2023010308523), Dec 30, 2022: WEB. CORRODED. CORROSION ON WEB AT LWR SILL AREA BTW STA Y=946-954 PROJECTION LONG 28R-29R OF AFT CARGO COMPARTMENT. CORROSION LEVEL 2. WEB AT LWR SILL AREA BTW STA 946 TO STA
- [SDR DALA2022123008501](https://openairdocs.org/sdr/DALA2022123008501), Dec 30, 2022: DOOR FRAME. CORRODED. CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR (C2). LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR WAS REPLACED IAW SRM 53-20-15- 2R REPAIR 7, SRM 5
- [SDR DALA2022123008500](https://openairdocs.org/sdr/DALA2022123008500), Dec 29, 2022: SEAT TRACK. CORRODED. SEAT TRACK SECTION X=-56 BTW STA=479 WAS FOUND CORRODED OUT LIMITS. SEAT TRACK SECTION X=-56 BTW STA=479 WAS REPAIRED IAW SRM 53-20-52-2R REP. 1 FIG. 201.
- [SDR DALA2022122908460](https://openairdocs.org/sdr/DALA2022122908460), Dec 29, 2022: SEAT TRACK. CORRODED. RIGHT SEAT TRACK SECTION X=-44 BTW STA Y=210 TO Y=275 WAS FOUND CORRODED OUT LIMITS. SUMMARY OF NRC 00503: CORROSION LEVEL 2. RH SEAT TRACK SECTION X =-44 BTW S
- [SDR DALA2022122908459](https://openairdocs.org/sdr/DALA2022122908459), Dec 29, 2022: SEAT TRACK. CRACKED. AFTER REMOVAL RH SEAT TRACK SECTION X=-44 BTW STA Y= 218 TO Y=342 A CRACK WAS FOUND IN THE CUSP WEB AT STA Y=294 TO Y=300. SUMMARY OF NRC 00516: CUSP WEB STA Y=
- [SDR DALA2022122908458](https://openairdocs.org/sdr/DALA2022122908458), Dec 29, 2022: SEAT TRACK. CORRODED. IN REF TO NRC 00325: SEAT TRACK SECTION X=-56 BTW STA=920 TO STA=922 WAS FOUND CORRODED OUT LIMITS. SUMMARY OF NRC 00496: CORROSION LEVEL 2. SEAT TRACK SECTION 
- [SDR DALA2022122908461](https://openairdocs.org/sdr/DALA2022122908461), Dec 28, 2022: PAN. WORN. WEAR ON SKIN PAN NEAR TO AFT LATCH FITTING AT AFT CARGO COMPARTMENT DOOR (PTAS). SUMMARY OF NRC 00061: SKIN PAN NEAR TO AFT LATCH FITTING AT AFT CARGO COMPARTME
- [SDR DALA2022122908457](https://openairdocs.org/sdr/DALA2022122908457), Dec 28, 2022: LONGERON. CRACKED. CRACK ON LOGERON 2LH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT (CAT). SUMMARY OF NRC 00469: LONGERON 2LH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT WAS REP
- [SDR DALA2022122708378](https://openairdocs.org/sdr/DALA2022122708378), Dec 24, 2022: WEB. CORRODED. CORROSION ON WEB BS 256, X=49. THE WEB WAS REPAIRED IAW SRM 53-00-55-2R-4R.
- [SDR DALA2022122708377](https://openairdocs.org/sdr/DALA2022122708377), Dec 24, 2022: CUSP WEB. CRACKED. CRACK ON LT CUSP WEB INNER FACE AT BS 898, X=44. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, REPAIR 4.
- [SDR DALA2022122708376](https://openairdocs.org/sdr/DALA2022122708376), Dec 23, 2022: CUSP WEB. CRACKED. CRACK IN RT CUSP WEB BTW BS 617-636, X=-53 TO X=-59 IN PASSENGER CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, REPAIR 4.
- [SDR DALA2022122708375](https://openairdocs.org/sdr/DALA2022122708375), Dec 23, 2022: SEAT TRACK. CORRODED. SEAT TRACK X=-22 BTW BS 200-266 WAS FOUND CORRODED OUT LIMITS. SEAT TRACK REPLACED IAW SRM 51-41-01-0G & SRM 51-41-05-0G.
- [SDR DALA2022122308316](https://openairdocs.org/sdr/DALA2022122308316), Dec 23, 2022: ANGLE. CORRODED. CORRODED OUT OF LIMITS AT CLIPS STA Y=829, Y=875, Y=912. ORIGINAL THICKNESS IS 0.032 IN AND MINIMUM REMAINING THICKNESS IS 0.10 IN, THEREFORE THE AREA IS OUT OF
- [SDR DALA2022122308313](https://openairdocs.org/sdr/DALA2022122308313), Dec 22, 2022: ANGLE. CRACKED. AFTER SEAL RETAINER REMOVAL, CRACKED INTERNAL ANGLE WAS FOUND ON APROX STA Y=390 AT FWD CARGO DOOR. INTERNAL ANGLE ON AFT LOWER EDGE APROX STA Y=390 AT FWD CARG
- [SDR DALA2022122308312](https://openairdocs.org/sdr/DALA2022122308312), Dec 22, 2022: FITTING. CRACKED. AFTER SEAL RETAINER REMOVAL, CRACK WAS FOUND ON FITTING. FITTING ON AFT LOWER EDGE AT FWD CARGO DOOR WAS REPLACED IAW SRM 51-41-01-0G AND SRM 51-41-02-0G.
- [SDR DALA2022122208293](https://openairdocs.org/sdr/DALA2022122208293), Dec 22, 2022: WEB. CRACKED. CRACK ON LH CUSP WEB EDGE AT STA Y=717 AND X =56. SUMMARY OF NRC 00373: LH CUSP WEB EDGE AT STA Y=717 AND X=56 WAS PERMANENTLY REPAIRED PER B717-200 SRM 53-00-5
- [SDR DALA2022122208292](https://openairdocs.org/sdr/DALA2022122208292), Dec 21, 2022: ANGLE. CRACKED. CRACK ON INTERNAL ANGLE LOWER EDGE STA Y=389 APROX AT FWD CARGO COMPARTMENT. (CCD). SUMMARY OF NRC 00048: INTERNAL ANGLE LOWER EDGE STA Y=389 APROX AT FWD CARGO
- [SDR DALA2022122108269](https://openairdocs.org/sdr/DALA2022122108269), Dec 21, 2022: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT STA Y=218 - X=0 (CPAX)(W1). SUMMARY OF NRC 00363: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=218 - X=0 WAS REPLACED PER B717-200 SRM 51-4
- [SDR DALA2022122108268](https://openairdocs.org/sdr/DALA2022122108268), Dec 21, 2022: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=5 AND X=-5 (CPAX)(W1). SUMMARY OF NRC 00335: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 BTW X=5 AND X=-5 WAS FABRICAT
- [SDR DALA2022122108267](https://openairdocs.org/sdr/DALA2022122108267), Dec 21, 2022: SUPPORT. CORRODED. CORROSION ON GALLEY SUPPORT STA Y=210 & STA Y=217 - X=-11 (CPAX)(W1). SUMMARY OF NRC 00361: CORROSION LEVEL 2. GALLEY SUPPORT STA Y=210 & STA Y=217 - X=-11 WERE
- [SDR DALA2022122008238](https://openairdocs.org/sdr/DALA2022122008238), Dec 20, 2022: WEB. PUNCTURED. PUNCTURE ON WEB STA Y=217 - X=-11 WAS FOUND DURING REMOVAL OF GALLEY SUPPORT ON NRC 00361. (CPAX)( W1). SUMMARY OF NRC 00456: WEB STA Y=217 - X=-11 WAS REPAIRED
- [SDR DALA2022122008237](https://openairdocs.org/sdr/DALA2022122008237), Dec 20, 2022: FLOOR SUPPORT. CORRODED. SECONDARY NRC, IN REF NRC 00364: AFTER REMOVAL PARTS TO ATTEND DISCREPANCY, CORROSION ON FLOOR SUPPORT STA Y=200 AND X=-55 WAS FOUND AT PASSENGER CABIN FLOOR AR
- [SDR DALA2022121908173](https://openairdocs.org/sdr/DALA2022121908173), Dec 19, 2022: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT STA Y=180 BTW X=-9 - X=-42. CORROSION LEVEL 2. FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G AND B717-200 SRM 51-41-05-0G.
- [SDR DALA2022121908176](https://openairdocs.org/sdr/DALA2022121908176), Dec 18, 2022: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT STA Y=160-200 X=-44 (CPAX)(W1). SUMMARY OF NRC 00338: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=160-200 X=-44 (CPAX)(W1) WAS FABRICATED 
- [SDR DALA2022121908175](https://openairdocs.org/sdr/DALA2022121908175), Dec 17, 2022: FLOOR SUPPORT. CORRODED. CORROSION OUT OF LIMITS ON FLOOR SUPPORT AT STA Y=160-195. ORIGINAL THICKNESS IS 0.071 IN AND MINIMUM REMAINING THICKNESS IS 0.025 IN, THEREFORE THE AREA IS OUT
- [SDR DALA2022122008236](https://openairdocs.org/sdr/DALA2022122008236), Dec 16, 2022: DOUBLER. CORRODED. CORROSION ON RH REPAIR DOUBLER BTWN STA 908 TO STA 927 AND FROM X=44 TO X=59 OF PASSENGER CABIN FLOOR. SUMMARY OF NRC 00333: CORROSION LEVEL 2. PREVIOS REPAIR D
- [SDR DALA2022082405714](https://openairdocs.org/sdr/DALA2022082405714), Aug 23, 2022: NONE. NONE. THE EMERGENCY LIGHTS OVER THE EMERGENCY EXIT WINDOWS AND ALL OF THE CEILING LIGHTS AFT OF THE OVER WING EMERGENCY EXITS CAME ON IN FLIGHT. MAINTENANCE COULD NOT
- [SDR DALA2022081605532](https://openairdocs.org/sdr/DALA2022081605532), Aug 16, 2022: NONE. NONE. SHIP 9512 -HYD/GEAR- AN EMERGENCY WAS DECLARED FOR THE APPROACH AND LANDING IN BTR FOLLOWING THE LOSS OF THE RIGHT HYDRAULIC SYSTEM FLUID. THE ALTERNATE GEAR EX
- [SDR DALA2022051603342](https://openairdocs.org/sdr/DALA2022051603342), May 16, 2022: NONE. NONE. THE AFT LOWER OVERWING EMERGENCY EXIT LIGHTS WERE DISCOVERED AS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, PER B717 AMM 33-51. THE OPERATIONAL 
- [SDR DALA2022051603341](https://openairdocs.org/sdr/DALA2022051603341), May 16, 2022: NONE. NONE. THE AFT OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. THE BATTERY POWER SUPPLY WAS REPLACED BY MAINTENANCE PER B717 AMM 33-51. OPERATIONAL WAS CHECK GOOD. (LP
- [SDR DALA2022051603340](https://openairdocs.org/sdr/DALA2022051603340), May 16, 2022: NONE. NONE. THE AFT BULKHEAD EMERGENCY EXIT LIGHT WAS DISCOVERED TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, PER B717 AMM 33-51. OPERATIONAL CHECK WAS
- [SDR DALA2021113007344](https://openairdocs.org/sdr/DALA2021113007344), Nov 28, 2021: NONE. NONE. TAIL CONE EXTERNAL RELEASE CLAMP OUT OF RIG LEFT AND RIGHT CLAMPS. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CF
- [SDR DALA2021112907291](https://openairdocs.org/sdr/DALA2021112907291), Nov 24, 2021: NONE. NONE. THE AFT CABIN EMERGENCY EXIT DOOR FRAME HAS TWO LARGE CRACKS. RIGHT HAND MID AREA. -M- SUMMARY SEE NRC 001-0308:5212-2001/001 00084: REPAIRED DAMAGE TO AFT CABI
- [SDR DALA2021112407219](https://openairdocs.org/sdr/DALA2021112407219), Nov 23, 2021: NONE. NONE. THE LEFT HAND FORWARD ENTRY DOOR SLIDE HAS THE PARACHUTE PIN ROUTED INCORRECTLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIA

All 137: https://openairdocs.org/aircraft/N953AT/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/N953AT/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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