# N970AT: 2001 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [Rolls-Royce BR-700 series](https://openairdocs.org/engine/rolls-royce-br-700-series) (registry code 54565)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55031
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 10, 2001
- Certificate issued: February 6, 2024
- Expires: February 28, 2031
- Mode S code: AD83B7
- 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=970AT
- Page: https://openairdocs.org/aircraft/N970AT

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 Rolls-Royce 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 (Rolls-Royce 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/N970AT/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 ATL03LA124](https://openairdocs.org/ntsb/ATL03LA124), Aug 1, 2003: Boeing 717-200 (N970AT), Atlanta, GA, substantial damage. Probable cause: The failure of the ground crew to follow powerback procedures and directives.

## FAA accident and incident reports (2)

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 20121009022819I](https://openairdocs.org/incident/20121009022819I), Oct 9, 2012: Boeing 717-200 (N970AT), Milwaukee, WI, Minor damage. Airtran airways flight 658, a Boeing 717-200, N970AT, had just parked at gate C23 and began deplaning when it was sturck by a catering vehicle on the left…
- [Accident 20030801020079A](https://openairdocs.org/incident/20030801020079A), Aug 1, 2003: Boeing 717200 (N970AT), Atlanta, GA, Substantial damage. (-23) On August 1st, 2003 during a powerback from gate 17A (1512 hours) by an airtran airways aircraft N970AT, a B-717-200. The left wing tip trailing edge and…

## Service difficulty reports (201, 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 DALA2026102105788](https://openairdocs.org/sdr/DALA2026102105788), Oct 20, 2026: SKIN. DENTED. FOUND DENTS AT LOWER FUSELAGE SKIN BETWEEN STA Y=495 & Y=507/L-28L & L-29, COMPLIED WITH ER/A 625374-14. (1876653) (AIRCRAFT GROUNDED).
- [SDR DALA2026101405655](https://openairdocs.org/sdr/DALA2026101405655), Oct 14, 2026: SCUFF PLATE. DAMAGED. FOUND AFT CARGO BAY SCUFF PLATE DAMAGED. COMPLIED WITH ER/A 637522-14. (8981866) (AIRCRAFT GROUNDED).
- [SDR DALA2026100605531](https://openairdocs.org/sdr/DALA2026100605531), Oct 2, 2026: WINDOW. DELAMINATED. WINDOW AT 19E SHOWS SIGNS OF DELAMINATION. R & R FWD RT O/W EMERGENCY EXIT DOOR ASSY IAW AMM 52-21-01. OPS & LEAK CHKD GOOD. (8981818) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026091105081](https://openairdocs.org/sdr/DALA2026091105081), Sep 10, 2026: WINDSHIELD. CRACKED. CA WINDSHIELD CRACKED DURING FLIGHT ARCING NEAR TOP, R & R LT SIDE FLIGHT COMPARTMENT WINDSHIELD IAW AMM 56-11. (9184422) (AIRCRAFT GROUNDED).
- [SDR DALA2026090304978](https://openairdocs.org/sdr/DALA2026090304978), Sep 2, 2026: OXYGEN MASK. UNWANTED DEPLOY. O2 MASK DROPPED OVER SEATS 15CDE, RESTOWED O2 MASKS IAW AMM 35-23. (8816982) (AIRCRAFT GROUNDED).
- [SDR DALA2026071704218](https://openairdocs.org/sdr/DALA2026071704218), Jul 15, 2026: LIGHT. INOPERATIVE. FOUND OVERHEAD L1 EMERGENCY LIGHT INOPERATIVE, REMOVED & REPLACED LIGHT ASSEMBLY L2-789. IAW AMM 33-51. (8820878) (AIRCRAFT GROUNDED).
- [SDR DALA2026070103878](https://openairdocs.org/sdr/DALA2026070103878), Jun 27, 2026: LAMP. INOPERATIVE. R1 DOOR ENTRY LIGHTS INOP, RELAMPED IAW AMM 33-23-09. (8543381) (AIRCRAFT GROUNDED).
- [SDR DALA2025090906668](https://openairdocs.org/sdr/DALA2025090906668), Sep 2, 2025: BRACE. DAMAGED. PER DAL ENGINEERING REQUEST: PERFORM INSPECTIONS ON REAR SPAR AT RT WING. LOWER FLAP BRACE DOUBLER AT STA XRS 164 ON LOWER SURFACE AND REAR SPAR OF RH WING WERE
- [SDR DALA2025090406559](https://openairdocs.org/sdr/DALA2025090406559), Aug 26, 2025: DOUBLER. CRACKED. CRACK ON DOUBLER BTW STA: XRS164 AND 150.450 AT LT WING. LOWER SURFACE OF LT WING WAS REPAIRED PER ER/A 626343-14AD (1165171)
- [SDR DALA2025090406561](https://openairdocs.org/sdr/DALA2025090406561), Aug 22, 2025: REPAIR. CRACKED. LEFT WING, LOWER SURFACE, LOWER FLAP BRACE DOUBLER AT XRS 164 HAS A CRACK IN TIME LIMITED REPAIR. REPAIRED LOWER WING SKIN AND SPAR PER ERA 626343-14AD (1158212
- [SDR DALA2025040802703](https://openairdocs.org/sdr/DALA2025040802703), Apr 7, 2025: SKIN. DENTED. DENTS ON SKIN BTW STA Y=493 AND STA Y=510 BTW LONG 28L AND LONG 29R AT CTR LOWER FUSELAGE. SUMMARY OF NRC 00025: DENTS ON SKIN BTW STA Y=493 AND STA Y=510 BTW L
- [SDR DALA2024050104840](https://openairdocs.org/sdr/DALA2024050104840), May 1, 2024: BATTERY PACK. NO TEST. ON SERVICE CHECK THE EMERGENCY EXIT SIGN ABOVE THE L1 DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND POWER SUPPLY B5-235 PER B717 A
- [SDR DALA2024060405770](https://openairdocs.org/sdr/DALA2024060405770), Apr 20, 2024: WINDOW. MISSING. 17A OUTER GLASS WINDOW MISSING ON POST FLIGHT INSPECTION. REPLACED OUTER PANE AT SEAT 17A PER B717 AMM 56-20. NO LEAKS A/C OK FOR SVC. (LP #5307957)
- [SDR DALA2023051203749](https://openairdocs.org/sdr/DALA2023051203749), May 12, 2023: UNKNOWN. UNKNOWN. CRACK ON PAN (FASTENER HOLE AREA) ABOVE SEAL RETEINER AT AFT CARGO DOOR. SUMMARY OF NRC-00071: PAN ON 3 AREAS AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA
- [SDR DALA2023051203743](https://openairdocs.org/sdr/DALA2023051203743), May 10, 2023: UNKNOWN. UNKNOWN. DURING TEST OF EMERGENCY LIGHTS, THE OVERWING LIGHTS STAY ON WITH THE SWITCH AT THE FORWARD ATTENDANT PANEL, IN THE OFF POSITION. SUMMARY OF NRC 00565: THE OVER
- [SDR DALA2023051103711](https://openairdocs.org/sdr/DALA2023051103711), May 10, 2023: UNKNOWN. UNKNOWN. IN REF TO CARD AD A.A. 5530-01048-03: PERFORM PERMANENT REPAIR (VERTICAL STABILIZER SPLICE BAND). SUMMARY OF NRC-00504: 48 HOLES OF VERTICAL STABILIZER LEADING 
- [SDR DALA2023051003665](https://openairdocs.org/sdr/DALA2023051003665), May 9, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME CLIP STA Y=1028 AFT CARGO. SUMMARY OF NRC 00566: CORROSION LEVEL 2. FRAME CLIP STA Y=1028 AFT CARGO WAS REPLACED PER B717-200 SRM 53-00-06-2R
- [SDR DALA2023050903614](https://openairdocs.org/sdr/DALA2023050903614), May 9, 2023: UNKNOWN. UNKNOWN. CUT ON LANYARD ASSY CABLE OF DOOR 1 LEFT ESCAPE SLIDE (L1). THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 
- [SDR DALA2023050803568](https://openairdocs.org/sdr/DALA2023050803568), May 6, 2023: UNKNOWN. UNKNOWN. ELONGATED HOLES ON CARGO TRACK BTW STA Y408 TO Y427, LONGERONS 27L AND 28L AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00200: CARGO TRACK BTW STA Y408 TO Y427
- [SDR DALA2023050403459](https://openairdocs.org/sdr/DALA2023050403459), May 4, 2023: UNKNOWN. UNKNOWN. CORROSION ON LOWER SKIN OF CUSP ANGLE FROM STA 200 TO 218 AND -X=56 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00489: LOWER SKIN OF CUSP ANGLE FROM STA 
- [SDR DALA2023050203393](https://openairdocs.org/sdr/DALA2023050203393), May 1, 2023: UNKNOWN. UNKNOWN. CORROSION ON LONGERON END RH L24 APROX STA Y=1002 OF AFT CARGO COMPARTMENT. SUMMARY OF NRC 00256: CORROSION LEVEL 2. LONGERON END RH L24 APROX STA Y=1002 OF AFT
- [SDR DALA2023050203391](https://openairdocs.org/sdr/DALA2023050203391), Apr 28, 2023: UNKNOWN. UNKNOWN. DENTS ON EXTERNAL SKIN BTW STA Y=218 TO 245 AND L-17L TO L-18L AT FUSELAGE, IN REFERENCE TO LP 1614671 AND LP 1614671. SUMMARY OF NRC 00535: FUSELAGE EXTERNAL S
- [SDR DALA2023050203390](https://openairdocs.org/sdr/DALA2023050203390), Apr 28, 2023: UNKNOWN. UNKNOWN. CRACKS (3 EA) ON AFT PAN OF FROM BEAM #3 TO BEAM #5 AND CRACKS (3 EA) ON FWD PAN FROM BEAM #1 AND BEAM #4 OF FWD CARGO DOOR. ALSO CRACK (1 EA) ON UPPER PAN CLOS
- [SDR DALA2023042803322](https://openairdocs.org/sdr/DALA2023042803322), Apr 27, 2023: UNKNOWN. UNKNOWN. DENTS ON EXTERNAL SKIN BTW STA Y=218 TO 245 AND L-17L TO L-18L AT FUSELAGE. SUMMARY OF NRC 00525: DENTS ON EXTERNAL SKIN BTW STA Y=218 TO 229 AND L-17L TO L-18L
- [SDR DALA2023042603250](https://openairdocs.org/sdr/DALA2023042603250), Apr 26, 2023: UNKNOWN. UNKNOWN. DURING ATTENTION OF NRC 00399, FLOOR SUPPORTS (2 EA) ON STA 148 TO 200 X=-54 WERE FOUND CORRODED OUT OF LIMITS. SUMMARY OF NRC 00491: CORROSION LEVEL 2. FLOOR S
- [SDR DALA2023042603248](https://openairdocs.org/sdr/DALA2023042603248), Apr 25, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR ANGLE BTW STA Y=200 AND STA Y=210 AND X=-54 OF AFT DOOR JAMB AT FWD SERVICE DOOR. SUMMARY OF NRC 00397: CORROSION LEVEL 2. FLOOR ANGLE BTW ST
- [SDR DALA2023042503243](https://openairdocs.org/sdr/DALA2023042503243), Apr 25, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA Y=1022 AND LONGERON 7RH AT PAX CABIN. SUMMARY OF NRC 00402: CRACK ON FRAME STA Y=1022 AND LONGERON 7RH AT PAX CABIN WAS REPAIRED PER ER/A 607
- [SDR DALA2023042503242](https://openairdocs.org/sdr/DALA2023042503242), Apr 24, 2023: UNKNOWN. UNKNOWN. CRACK ON FRAME STA Y=1022 AND LONGERON 7LH AT PAX CABIN. SUMMARY OF NRC 00299: CRACK ON FRAME STA Y=1022 AND LONGERON 7LH AT PAX CABIN WAS REPAIRED PER ER/A 607
- [SDR DALA2023042503238](https://openairdocs.org/sdr/DALA2023042503238), Apr 22, 2023: UNKNOWN. UNKNOWN. CORROSION ON FLOOR ANGLE CLIP APPROX STA Y=168 AND X=-56 AT W1. SUMMARY OF NRC 00400; CORROSION LEVEL 2. FLOOR ANGLE CLIP APPROX STA Y=168 AND X=-56 AT W1 WAS F
- [SDR DALA2023042503237](https://openairdocs.org/sdr/DALA2023042503237), Apr 22, 2023: UNKNOWN. UNKNOWN. CORROSION ON MEMBRANE FROM STA Y=150 TO Y=218 AND -X=47 TO -X=60 AT PAX CABIN (CPAX). SUMMARY OF NRC 00389: CORROSION LEVEL 2. MEMBRANE FROM STA Y=150 TO Y=218 
- [SDR DALA2023042003110](https://openairdocs.org/sdr/DALA2023042003110), Apr 20, 2023: UNKNOWN. UNKNOWN. CORROSION ON UPPER MEMBRANE FROM STA Y=150 TO Y=170 AND -X=47 TO -X=60 AT PASSENGER CABIN. SUMMARY OF NRC 00528: CORROSION LEVEL 2. WEB FROM STA Y=150 TO Y=170 
- [SDR DALA2023041803050](https://openairdocs.org/sdr/DALA2023041803050), Apr 17, 2023: UNKNOWN. UNKNOWN. AD. CRACK WAS FOUND ON RH OVERWING FRAME, LENGTH=0.600 IN IN REF TASK CARD 5310-01436-01D JOB #084-0004 STEP 7. SUMMARY OF NRC 00322: OVERWING FRAME RH LENGTH=0
- [SDR DALA2023041803048](https://openairdocs.org/sdr/DALA2023041803048), Apr 16, 2023: UNKNOWN. UNKNOWN. REWRITE. SECONDARY NRC IN REF NRC 311: CORROSION ON CUSP MEMBRANE (WEB) RH STA Y=427 AT PAX CABIN. SUMMARY OF NRC 00525: CORROSION LEVEL 2. REPAIR DOUBLER WAS F
- [SDR DALA2023041803047](https://openairdocs.org/sdr/DALA2023041803047), Apr 16, 2023: UNKNOWN. UNKNOWN. CORROSION ON FWD FACE BELOW FLOOR BULKHEAD RBL 20 AND LBL 20 STA 1053 AT PAX CABIN. SUMMARY OF NRC 00429: CORROSION LEVEL 2. GUSSETS ON FWD FACE BELOW FLOOR BUL
- [SDR DALA2023041402966](https://openairdocs.org/sdr/DALA2023041402966), Apr 14, 2023: UNKNOWN. UNKNOWN. DENT ON LH CUSP MEMBRANE STA Y=927 AT PAX CABIN. SUMMARY OF NRC 00419: DENT ON LH CUSP MEMBRANE STA Y=927 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R
- [SDR DALA2023041202862](https://openairdocs.org/sdr/DALA2023041202862), Apr 11, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP WEB MEMBRANE (2EA) BTW STA Y636 AND Y655, LONGERONS 18L AND 18R AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00287: CRACK ON CUSP WEB MEMBRANE (2
- [SDR DALA2023041002744](https://openairdocs.org/sdr/DALA2023041002744), Apr 8, 2023: UNKNOWN. UNKNOWN. CRACK ON INTERCOSTAL BTW STA Y617 TO STA Y636 LONGERONS 18L AND 18R AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00291: INTERCOSTAL BTW STA Y617 TO STA Y636 LO
- [SDR DALA2023040502677](https://openairdocs.org/sdr/DALA2023040502677), Apr 4, 2023: UNKNOWN. UNKNOWN. SECONDARY NRC IN REF AMDS 5530-01048-02: "AA 5530-01048" AND "AD 2018-10-08". LOOSE FASTENERS OF RH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=5
- [SDR DALA2023040502676](https://openairdocs.org/sdr/DALA2023040502676), Apr 4, 2023: UNKNOWN. UNKNOWN. SECONDARY NRC IN REF AMDS 5530-01048-02: "AA 5530-01048" AND "AD 2018-10-08". LOOSE FASTENERS OF LH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=5
- [SDR DALA2023030101526](https://openairdocs.org/sdr/DALA2023030101526), Feb 25, 2023: NONE. NONE. FOUND LOWER AFT CORNER OF L1 DOOR DAMAGED AFTER AIRCRAFT ARRIVAL. INSPECTED DAMAGE AREA. REMOVED REQ FASTENERS AND CUT OUT DAMAGE PER B717 SRM 52-10-01-2R-1. PR
- [SDR DALA2022070504625](https://openairdocs.org/sdr/DALA2022070504625), Jul 3, 2022: NONE. NONE. THE EMERGENCY LIGHTS AT LOCATIONS POWERED BY B5-123 BATTERY PACK ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK PER B717 AMM 33-51, AT THE B5-
- [SDR DALA2022050103044](https://openairdocs.org/sdr/DALA2022050103044), May 1, 2022: LIGHT. INOPERATIVE. THE AFT OVERWING EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY TRAY FOR EXIT LIGHT POSITION B5-230 IAW B717 AMM 33-51-00. OPERATIONAL CHECK WAS 
- [SDR DALA2022042903014](https://openairdocs.org/sdr/DALA2022042903014), Apr 27, 2022: NONE. NONE. CORROSION UPPER WING SURFACE AT STA 324 & STR 5 (RIGHT WING). BLENDED CORROSION AT STA 324 STR 5 RH WING UPPER SURFACE PER B717 SRM 51-10-04. C/W HFEC INSPECTIO
- [SDR DALA2022032401938](https://openairdocs.org/sdr/DALA2022032401938), Mar 24, 2022: UNKNOWN. UNKNOWN. THE EMERGENCY EXIT SIGN ABOVE THE FWD FLIGHT ATTENDANT SEAT IS INOPERATIVE. MAINTENANCE REPLACED THE #2 EMERGENCY LIGHT BATTERY ASSEMBLY PER B717 AMM 35-51. OPE
- [SDR DALA2022031801806](https://openairdocs.org/sdr/DALA2022031801806), Mar 17, 2022: NONE. NONE. FLIGHT CREW DECLARED AN EMERGENCY DUE TO A REPORT OF A SEPERATED TIRE. THE AIRCRAFT MADE A NORMAL SAFE LANDING AND UN-EVENTFUL TAXI AT ATL. MAINTENANCE INSPECTE
- [SDR DALA2021062203376](https://openairdocs.org/sdr/DALA2021062203376), Jun 21, 2021: LENS. DETACHED. THE FORWARD EXIT SIGN COVER FELL OF ON LANDING AND COULD NOT BE FOUND. LATER, MAINTENANCE REINSTALLED THE EMERGENCY EXIT COVER. OPERATIONAL CHECK WAS OK. EMERGE
- [SDR DALA2021050302491](https://openairdocs.org/sdr/DALA2021050302491), May 2, 2021: BATTERY PACK. INOPERATIVE. THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION LIGHTS BATTERY PACK, B5-125, PER B71
- [SDR DALA2022110207101](https://openairdocs.org/sdr/DALA2022110207101), Mar 23, 2021: NONE. NONE. DAMAGE TOLERANCE EVALUATION REQUIRED FOR ERA 590529-14. REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE FROM DATE OF APPROVAL ONLY (23 MAR 2023). ADDITIONAL ENG
- [SDR DALA2021032401733](https://openairdocs.org/sdr/DALA2021032401733), Mar 21, 2021: HINGE. EXCESS PLAY. THE LT O/B FLAP HINGE HAS EXCESSIVE PLAY AT HINGE BOLT. DEFERRED FOR SDR REPORTING. NRC 331: REPAIRED PER PRI 590529-14 REV 0,1,2,3,&4 AND ER/A 590529-14 REV OR
- [SDR DALA2021032301673](https://openairdocs.org/sdr/DALA2021032301673), Mar 20, 2021: RING. DETACHED. THE R1 SLIDE PACK MANUAL DEPLOYMENT RING IS NOT ATTACHED TO THE CABLE. MAINTENANCE REPLACED THE R-1 DOOR SLIDE REF ROUTINE TASK CARD 2561-9005. (LP #1760202)

All 201: https://openairdocs.org/aircraft/N970AT/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/N970AT/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md
- The Rolls-Royce BR-700 series engine: https://openairdocs.org/engine/rolls-royce-br-700-series.md

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