# N965AT: 2001 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: 55026
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 1, 2001
- Certificate issued: February 6, 2024
- Expires: February 28, 2031
- Mode S code: AD6ECB
- 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=965AT
- Page: https://openairdocs.org/aircraft/N965AT

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/N965AT/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 N965AT.

## 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 20030129006899I](https://openairdocs.org/incident/20030129006899I), Jan 29, 2003: Boeing 717200 (N965AT), Bloomington-Nor, IL, Minor damage. (-23) Climbing thru 16000 ft, the right engine emitted a loud bang and spooled down to idle power. "Eng low RPM", "eng surge r" and the "increase eng bleed"…

## Service difficulty reports (196, 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 DALA2026102205832](https://openairdocs.org/sdr/DALA2026102205832), Oct 21, 2026: SKIN. DAMAGED. FOUND SEVERAL EXISTING LIGHTNING STRIKE DAMAGES COMMON TO STRINGER L2R IN THE KA1717 STC AREA, COMPLIED WITH ER/A 637562-14. (1877071) (AIRCRAFT GROUNDED).
- [SDR DALA2026102205830](https://openairdocs.org/sdr/DALA2026102205830), Oct 21, 2026: DOUBLER. DAMAGED. FOUND LIGHTNING STRIKE DAMAGE LOCATED IN PCS ANTENNA DOUBLER AREA, COMPLIED WITH ER/A 637562-14AD. (1878172) (AIRCRAFT GROUNDED).
- [SDR DALA2026102205829](https://openairdocs.org/sdr/DALA2026102205829), Oct 21, 2026: DOUBLER. DAMAGED. LIGHTNING STRIKE DAMAGE LOCATED IN ESA ANTENNA DOUBLER AREA, COMPLIED WITH ER/A 637560-14AD. (1878165) (AIRCRAFT GROUNDED).
- [SDR DALA2026082704865](https://openairdocs.org/sdr/DALA2026082704865), Aug 26, 2026: PROXIMITY SENSOR. OUT OF ADJUST. ATB- RETURNED TO LIT DUE TO LEFT GEAR UNSAFE ANNUNCIATION. MLG DOOR PROX SENSOR ADJUSTED TO BE WITHIN LIMITS IAW AMM 32-61. OPS CHECKS GOOD. R&R LEFT MLG DOOR P
- [SDR DALA2026082104770](https://openairdocs.org/sdr/DALA2026082104770), Aug 19, 2026: FMU. FAULTED. ABORTED TAKEOFF AT 110 KTS DUE TO LT ENGINE UNABLE TO MAKE TAKEOFF POWER. R & R NR 1 ENGINE FMU IAW AMM 73-21 AND R & R NR 1 ENGINE FUEL PUMP IAW AMM 73-12. (92
- [SDR DALA2026080704571](https://openairdocs.org/sdr/DALA2026080704571), Aug 6, 2026: TAB. DAMAGED. LIGHTNING STRIKE ON RH ELEVATOR CONTROL TAB UPPER SURFACE, R/R RH ELEVATOR CONTROL TAB PER B717 AMM 27-31-04-000-801. (1742126) (AIRCRAFT GROUNDED).
- [SDR DALA2026080604543](https://openairdocs.org/sdr/DALA2026080604543), Aug 6, 2026: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN BS 1087 BTW LONG 13L & 14L, COMPLIED WITH ER/A 635909-14. (1741062) (AIRCRAFT GROUNDED).
- [SDR DALA2026080404488](https://openairdocs.org/sdr/DALA2026080404488), Aug 3, 2026: SKIN. CRACKED. CRACKS FUSELAGE SKIN STA Y=1087, L-13L TO L-14L. REPAIRED PER ERA 635909-14. (1735466) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026080304467](https://openairdocs.org/sdr/DALA2026080304467), Jul 31, 2026: PANEL. CORRODED. CORROSION ON ATTACH POINTS OF SLAT PANEL NR 2 AT WING LT. REPLACED PER SERVICEABLE LT WING SLAT NR 2 PER AMDS 2780-4000-LH-2. (1731207) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026080304466](https://openairdocs.org/sdr/DALA2026080304466), Jul 31, 2026: FRAME. CRACKED. CRACK ON CAP OF FRAME STA Y# = 1,178 BTW LONG 14RH TO 15RH AT AFT ACCESORIES COMPARTMENT. REPAIRED PER ER/A 635890-14. (1731671) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026042302606](https://openairdocs.org/sdr/DALA2026042302606), Apr 23, 2026: ACOUSTIC LINER. DAMAGED. DURING SERVICE CHECK FOUND DAMAGE IN #1 ENG INLET COWEL ACOUSTIC LINER. REPAIRED DAMAGE IN #1 ENG INLET COWEL ACOUSTIC LINER PER B717 SRM 54-10-01 (7985278) (AI
- [SDR DALA2025090406565](https://openairdocs.org/sdr/DALA2025090406565), Aug 30, 2025: SEAL. DIRTY. TAILCONE DOOR NOT FULLY SEATING AND SEALING ON UPPER RT SIDE OF THE DOOR. NOISE OBSERVED FROM THE UNSEATED PORTION OF THE DOOR. CLEANED SEAL, CYCLED DOOR AND PR
- [SDR DALA2025022001287](https://openairdocs.org/sdr/DALA2025022001287), Feb 18, 2025: LOCK LINK ASSY. DAMAGED. SHIP 9524 -IFSD/DE- THE CREW RECEIVED A "LEFT REVERSER UNLOCK" MESSAGE. THE QRH WAS COMPLIED WITH, WHICH INCLUDED SHUTTING DOWN THE LEFT ENGINE. CORRECTIVE ACTI
- [SDR DALA2024081608209](https://openairdocs.org/sdr/DALA2024081608209), Aug 14, 2024: STATIC WICK. DAMAGED. DURING LIGHTRING STRIKE INSPECTION FOUND LH ELEVATOR O/B STATIC DISCHARGER CONDUCTIVE DOUBLER DAMAGED. COMPLETED TEMP REPAIR PER ENGINEEREING CONCURRENCE EMAIL 
- [SDR DALA2024081508165](https://openairdocs.org/sdr/DALA2024081508165), Aug 14, 2024: SKIN. CRACKED. CORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LH MLG WHEEL WELL. SUMMARY OF NRC 00384: CORROSION LEVEL 2. C
- [SDR DALA2024081508164](https://openairdocs.org/sdr/DALA2024081508164), Aug 14, 2024: SKIN. CRACKED. CORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LH MLG WHEEL WELL. SUMMARY OF NRC 00384: CORROSION LEVEL 2. C
- [SDR DALA2024081508163](https://openairdocs.org/sdr/DALA2024081508163), Aug 14, 2024: SKIN. CRACKED. CORROSION ON LOWER SKIN OF CENTER FUEL TANK BTW STA APROX Y=696 AND ON STA Y=655 INTERNAL STRUCTURE AT RH CANTED KEEL. SUMMARY OF NRC 00492: CORROSION LEVEL 2. 
- [SDR DALA2024081208007](https://openairdocs.org/sdr/DALA2024081208007), Aug 11, 2024: HINGE. DAMAGED. ELONGATED HOLES ON INTERNAL PAN AT FWD CARGO DOOR HINGE ATTACH POINTS (FWD/AFT). (PTAS). SUMMARY OF NRC 00106: HOLES ON INTERNAL PAN AT FWD CARGO DOOR HINGE ATT
- [SDR DALA2024081208006](https://openairdocs.org/sdr/DALA2024081208006), Aug 10, 2024: SKIN. CRACKED. CRACKS WERE FOUND ON UPPER AND LOWER SKIN OF OUTBOARD TIP ELEVATOR LH. SUMMARY OF NRC 00701: UPPER AND LOWER SKIN OF OUTBOARD TIP ELEVATOR LH WAS REPAIRED PER E
- [SDR DALA2024080807887](https://openairdocs.org/sdr/DALA2024080807887), Aug 8, 2024: SKIN. DENTED. DENTS (2EA) ON FUSELAGE SKIN BTW STA Y=120 TO 144 APPROX AND LONG 18LH TO 19LH. ALSO PJECTION LONG-16LH TO LONG-17LH. SUMMARY OF NRC 00669: FUSELAGE SKIN BTW ST
- [SDR DALA2024080807885](https://openairdocs.org/sdr/DALA2024080807885), Aug 7, 2024: PAN. CRACKED. CRACK ON PAN (BEAM 3) AT AFT CARGO COMPARTMENT DOOR AFT EDGE. SUMMARY OF NRC 00402: PAN (BEAM 3) AT AFT CARGO COMPARTMENT DOOR AFT EDGE WAS REPAIRED PER PRI 618
- [SDR DALA2024080707853](https://openairdocs.org/sdr/DALA2024080707853), Aug 6, 2024: SKIN. CRACKED. CRACK ON INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT LH SLIDING WINDOW CUTOUT AREA WAS FOUND. SUMMARY OF NRC 00628: INTERNAL FUSELAGE SKIN JUST AFT UPPER CO
- [SDR DALA2024072907536](https://openairdocs.org/sdr/DALA2024072907536), Jul 26, 2024: SKIN. CORRODED. SEVERAL SPOTS OF CORROSION ON WING CENTER SECTION UPPER SKIN BTW STA Y=655 TO 674, Y=674 TO 696, Y=696 TO 715, AND BTW X=45 TO X=60 AT PASSENGER COMPARTMENT (CP
- [SDR DALA2024072207311](https://openairdocs.org/sdr/DALA2024072207311), Jul 18, 2024: CUSP WEB. CRACKED. CRACK WAS FOUND ON LH CUSP WEB STA 588 AT PAX CABIN. SUMMARY OF NRC 00798: LH CUSP WEB STA 588 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 
- [SDR DALA2024071707227](https://openairdocs.org/sdr/DALA2024071707227), Jul 16, 2024: SKIN. WORN. WEAR ON EDGE SKIN AROUND HOOK AT L1 DOOR. SUMMARY OF NRC 00111: EDGE SKIN AROUND HOOK AT L1 DOOR WAS REPAIRED PER PRI 619136-14 REV 1 AND ERA 619136-14 REV ORIG
- [SDR DALA2024071707226](https://openairdocs.org/sdr/DALA2024071707226), Jul 16, 2024: LONGERON. CORRODED. CORROSION ON END LONGERONS 25R AND 26R STA Y=1004 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00783: CORROSION LEVEL 2. END LONGERONS 25R AND 26R STA Y=1004 AT AFT
- [SDR DALA2024071507158](https://openairdocs.org/sdr/DALA2024071507158), Jul 13, 2024: FRAME. CRACKED. -AD- CRACK OF 1.00 IN LENGTH APPROX ON UPPER RADIUS OF THE LH OVERWING FRAME TAB STA Y=715.00 (IN REF. CARD 5310-01436-01B STEP 7). SUMMARY OF NRC 000333: THE L
- [SDR DALA2024071107017](https://openairdocs.org/sdr/DALA2024071107017), Jul 10, 2024: PAN. CRACKED. CRACK ON INTERNAL PAN (BEAM #1 AREA) FWD EDGE AT FWD CARGO DOOR. (PTAS) SUMMARY OF NRC 00099: INTERNAL PAN (BEAM #1 AREA) FWD EDGE AT FWD CARGO DOOR WAS REPAIRE
- [SDR DALA2024071006985](https://openairdocs.org/sdr/DALA2024071006985), Jul 9, 2024: FRAME. CRACKED. CRACK ON FRAME STA Y=696 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE. SUMMARY OF NRC 00499: FRAME STA Y=696 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE WAS REPAIRED
- [SDR DALA2024071006983](https://openairdocs.org/sdr/DALA2024071006983), Jul 9, 2024: DOUBLER. CORRODED. CORROSION ON PRODUCTION DOUBLER OF MASTER DRAIN BTW STA Y=199 AND Y=218 L28R AND L29R AT E/E COMPARTMENT. SUMMARY OF NRC 00766: CORROSION LEVEL2. PRODUCTION DOU
- [SDR DALA2024071006982](https://openairdocs.org/sdr/DALA2024071006982), Jul 8, 2024: CUSP WEB. CORRODED. CORROSION ON CUSP WEB STA 397-406 AND X=-59. ORIGINAL THICKNESS 0.020" AND MINIMUM REMAINING THICKNESS 0.003", THEREFORE IT IS OUT OF LIMITS PER B717-200 SRM 53
- [SDR DALA2024070806852](https://openairdocs.org/sdr/DALA2024070806852), Jul 7, 2024: SKIN. CRACKED. CRACK ON INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW CUTOUT AREA. INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW CUTOUT
- [SDR DALA2024070506803](https://openairdocs.org/sdr/DALA2024070506803), Jul 4, 2024: SEAT TRACK. CORRODED. AIRCRAFT 9524, CORROSION ON INB SEAT TRACK X22 STA Y=200 TO STA Y= 218 AT PAX CABIN (W1). CORRECTIVE ACTION: CORROSION LEVEL 2, SEAT TRACK WERE REPAIRED ON X= 2
- [SDR DALA2024070306744](https://openairdocs.org/sdr/DALA2024070306744), Jul 3, 2024: CUSP WEB. CORRODED. CORROSION ON PREVIOUS REPAIR DOUBLERS OF CUSP WEB STA Y=568-577 RH/LH SIDES AND X=55 AT PASSENGER CABIN (CPAX). CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLERS OF C
- [SDR DALA2024062906604](https://openairdocs.org/sdr/DALA2024062906604), Jun 29, 2024: SEAT TRACK. CORRODED. AIRCRAFT 9524, CORROSION ON SEAT TRACK AT STA Y=898 X=44.5 AT PAX CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2, SEAT TRACK SECTION BTW STA Y=898 TO STA Y= 935 X=
- [SDR DALA2024062906601](https://openairdocs.org/sdr/DALA2024062906601), Jun 28, 2024: PAN. CORRODED. AIRCRAFT 9524, CORROSION ON PAN DOOR JAMB STA Y=994 TO Y= 954 BTW LONG 24 AND 28 RH AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: CORROSION LEVEL 2, PAN DOOR JAM
- [SDR DALA2024062706573](https://openairdocs.org/sdr/DALA2024062706573), Jun 26, 2024: FITTING. CORRODED. AIRCRAFT 9524, CORROSION ON MAIN FRAME FITTING STAY=560 L18L AT PAX CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2. MAIN FRAME FITTING STAY= 560 L18L AT PAX CABIN 
- [SDR DALA2024062506491](https://openairdocs.org/sdr/DALA2024062506491), Jun 25, 2024: WEB. NICKED. NICK ON MEMBRANE WEB BTW STA Y=172/173, AND X46 APROX AT CABIN PAX. SUMMARY OF NRC 00434: MEMBRANE WEB BTW STA Y=172/173, AND X46 APROX AT CABIN PAX WAS REPAIRE
- [SDR DALA2024062506490](https://openairdocs.org/sdr/DALA2024062506490), Jun 25, 2024: CUSP WEB. CORRODED. CORROSION OUT OF LIMITS ON CUSP WEB BTW STA Y=739-745 AND X=59 AT PASSENGER CABIN. SUMMARY OF NRC 00744: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER ON CUSP WEB 
- [SDR DALA2024062406341](https://openairdocs.org/sdr/DALA2024062406341), Jun 21, 2024: BEAM. CRACKED. CRACK ON BEAM #2 STA Y=196 APROX IN PASSANGER DOOR (L1) AT CABIN PAX. SUMMARY OF NRC 00090: AREA ON BEAM #2 STA Y=196 IN PASSANGER DOOR L1 AT CABIN PAX WAS REPA
- [SDR DALA2024062006270](https://openairdocs.org/sdr/DALA2024062006270), Jun 20, 2024: FRAME. CRACKED. CRACK ON MAIN FRAME STA Y=1037 L17L, L17R AT PAX CABIN. SUMMARY OF NRC 00441: MAIN FRAME STA Y=1037 L17L, L17R AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-
- [SDR DALA2024040804186](https://openairdocs.org/sdr/DALA2024040804186), Apr 8, 2024: HINGE FITTING. WORN. CORROSION AND WEAR IN THE HINGE BOLT BORE OF THE OUTBOARD FLAP IDLER HINGE ON THE RH WING. ER/A 541841-14 ISSUED FOR REPAIR. THIS IS THE LOG PAGE THAT TRACKS TH
- [SDR DALA2024040804185](https://openairdocs.org/sdr/DALA2024040804185), Apr 8, 2024: HINGE FITTING. WORN. CORROSION AND WEAR IN THE HINGE BOLT BORE OF THE OUTBOARD FLAP IDLER HINGE ON THE RH WING. ER/A 541845-14 ISSUED FOR REPAIR. THIS IS THE LOG PAGE THAT TRACKS TH
- [SDR DALA2024031303283](https://openairdocs.org/sdr/DALA2024031303283), Mar 10, 2024: PSEU. FAILED. SHIP 9524 -GEAR/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC APPROACHING ATL DUE TO THE LEFT AND RIGHT "GEAR UNSAFE" INDICATIONS WITH THE GEAR HANDLE UP. 
- [SDR DALA2024030803185](https://openairdocs.org/sdr/DALA2024030803185), Mar 7, 2024: UPLOCK SENSOR. FAULTED. SHIP 9524 -GEAR/DE- AFTER TAKEOFF AND LANDING GEAR SELECTED TO RETRACT, THE CREW RECEIVED A "LEFT GEAR UNSAFE" INDICATION AFTER RETRACTION. THE QRH WAS COMPLIED
- [SDR DALA2024010900329](https://openairdocs.org/sdr/DALA2024010900329), Jan 7, 2024: UNKNOWN. UNKNOWN. SHIP 9524 -GEAR/DE- THE NOSE GEAR DID NOT EXTEND NORMALLY WHEN HANDLE WAS MOVED TO THE DOWN POSITION DURING APPROACH FOR LANDING AT HSV. THE TOWER DECLARED AN E
- [SDR DALA2024010200015](https://openairdocs.org/sdr/DALA2024010200015), Dec 31, 2023: UNKNOWN. UNKNOWN. SHIP 9524 -GEAR/DE- THE NOSE LANDING GEAR FAILED TO EXTEND NORMALLY AFTER TWO ATTEMPTS. THE FLIGHT CREW ACCOMPLISHED A GO-AROUND, DECLARED AN EMERGENCY WITH ATC
- [SDR DALA2023112909805](https://openairdocs.org/sdr/DALA2023112909805), Nov 28, 2023: UNKNOWN. UNKNOWN. THE COCKPIT EMERGENCY PATH LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK (B5-123). OPERATIONAL CHECK WAS GOOD. (LP #5508919)
- [SDR DALA2023112909804](https://openairdocs.org/sdr/DALA2023112909804), Nov 28, 2023: UNKNOWN. UNKNOWN. MULTIPLE EMERGENCY LIGHTS ARE INOPERATIVE IN THE CABIN AND TAIL. MAINTENANCE REPLACED THE BATTERY PACKS B5-118, B5-260, B5116, & B5-231. OPERATIONAL CHECK WAS G
- [SDR DALA2023103008884](https://openairdocs.org/sdr/DALA2023103008884), Oct 28, 2023: UNKNOWN. UNKNOWN. THE AISLE EXIT SIGN IS HANGING FREE. *** CONTRACT MAINTENANCE EVENT - OCM: 271717 *** COMPLIED WITH ERA 613272- 14 REV ORIG. TIME LIMITED REPAIR SECT I. DEFERED

All 196: https://openairdocs.org/aircraft/N965AT/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/N965AT/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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