# N961AT: 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: 55023
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 2, 2001
- Certificate issued: December 19, 2023
- Expires: December 31, 2030
- Mode S code: AD5FEF
- 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=961AT
- Page: https://openairdocs.org/aircraft/N961AT

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/N961AT/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 N961AT.

## FAA accident and incident reports

None matched to N961AT.

## Service difficulty reports (198, 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 DALA2026101305626](https://openairdocs.org/sdr/DALA2026101305626), Oct 10, 2026: SKIN. DENTED. FOUR DENTS IDENTIFIED COMMON TO AFT INSTALLATION DOUBLER BETWEEN L2R AND L3R FRAME Y541 TO Y560. REPAIRED PER ER/A 637249-14. (1858631) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026100805561](https://openairdocs.org/sdr/DALA2026100805561), Oct 7, 2026: SKIN. DEMODIFICATION. FOUND EXISTING (DEMOD) ANTENNA, INCLUDING AN INTERNAL DOUBLER, INTERFERING WITH STC DOUBLER BETWEEN Y503 TO Y522 AND STRG L-1 TO STRG L-3R, COMPLIED WITH ER/A 6
- [SDR DALA2026070303900](https://openairdocs.org/sdr/DALA2026070303900), Jul 3, 2026: LIGHT. INOPERATIVE. LEFT OVERWING EMERGENCY EVACUATION LIGHT INOPERATIVE. REPLACED LIGHT IAW AIPC 33-50. (8777078) (AICRAFT GROUNDED).
- [SDR DALA2025102207715](https://openairdocs.org/sdr/DALA2025102207715), Oct 20, 2025: CABLE. TWISTED. SHIP 9520 DURING SSE WAS FOUND TWISTED PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT. CORRECTIVE ACTION: PULL CABLE OF TAIL CONE RELEASE
- [SDR DALA2025102207714](https://openairdocs.org/sdr/DALA2025102207714), Oct 20, 2025: CABLE. TWISTED. DURING SSE WAS FOUND TWISTED PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT. PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY CO
- [SDR DALA2025102207716](https://openairdocs.org/sdr/DALA2025102207716), Oct 18, 2025: DOOR FRAME. CRACKED. SHIP 9520 CRACK OF 0.350IN LENGTH WAS FOUND ON LH OVERWING FRAME STA Y=737 IN REFRENECE TO CARD 5310-01439-01B / JOB 068-0003, STEP 4. LEFT OVERWING FRAME STA Y
- [SDR DALA2025102207713](https://openairdocs.org/sdr/DALA2025102207713), Oct 18, 2025: SEAL. LEAKING. DURING STATIC LEAK CHECK, WATER LEAKS WERE FOUND ON INSIDE OF FWD AND AFT LT OVERWING EMERGENCY EXIT DOORS. EXIT DOOR JAMB FILLER FWD AND AFT LT WERE REPLACED P
- [SDR DALA2025102207712](https://openairdocs.org/sdr/DALA2025102207712), Oct 18, 2025: FUEL TANK. CORRODED. EXFOLIATION ON LOWER SKIN OF CENTER FUEL TANK ON STA Y= 756 AND X= 43 AT LEFT MLG WHEEL WELL. LEFT MLG WHEEL WELL WAS REPAIRED PER ER/A 629799-14AD REV. (125816
- [SDR DALA2025102207711](https://openairdocs.org/sdr/DALA2025102207711), Oct 17, 2025: RELEASE MECH. OUT OF POSITION. IN REFERENCE AMDS 5352-4002 DURING INSTALL TAILCONE SLIDE WAS FOUND TAILCONE RELEASE MECHANIS CAM OUT POSITION. TAILCONE RELEASE MECHANISM CAM WAS ADJUSTED PER 
- [SDR DALA2025101707592](https://openairdocs.org/sdr/DALA2025101707592), Oct 10, 2025: NONE. NONE. SHIP 9520 DTA ER/A 629799-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 10-OCT-25. CORRECTIVE ACTION: REPAIRED PER DTA E
- [SDR DALA2025041102826](https://openairdocs.org/sdr/DALA2025041102826), Apr 10, 2025: BATTERY PACK. INOPERATIVE. IN THE AFT TAIL SECTION, ALL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND A BAD BATTERY PACK. THE BATTERY PACK WAS REPLACED IAW B717 AMM 33-51. OPERATION
- [SDR DALA2025041102825](https://openairdocs.org/sdr/DALA2025041102825), Apr 10, 2025: SIGN. INOPERATIVE. EXIT SIGN ABOVE AFT TAIL DOOR INOPERATIVE. MAINTENANCE REMOVED THE SIGN ASSEMBLY, FOUND WIRES DISCONNECTED, SECURED WIRES, AND THE LIGHT NOW OPERATIONALLY CHECK
- [SDR DALA2025040802707](https://openairdocs.org/sdr/DALA2025040802707), Mar 27, 2025: CABLE. BROKEN. THE FLIGHT ATTENDANT FOUND THAT THE FRONT SERVICE DOOR EMERGENCY CABLE TO BAR WAS BROKEN. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS N
- [SDR DALA2025031401971](https://openairdocs.org/sdr/DALA2025031401971), Mar 12, 2025: SKIN. GOUGED. BANANA FAIRING ATTACH SCREWS HAVE GOUGED INTO THE L/H STABILIZER SKIN PANEL. MAINTENANCE REPLACED LH VERT STAB SKIN TIP PER B717 SRM 51-40. (LP #6408784)
- [SDR DALA2025010300047](https://openairdocs.org/sdr/DALA2025010300047), Jan 1, 2025: BATTERY PACK. INOPERATIVE. OVERHEAD EMERGENCY LIGHTS FROM ROW 15 TO 19 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK FOR CORRESPONDING LIGHTS PER B717 AMM 33-51.
- [SDR DALA2025011500349](https://openairdocs.org/sdr/DALA2025011500349), Dec 15, 2024: DOOR. MISSING. EXTERNAL POWER RECEPTACLE DOOR MISSING. FWD TO CDL 52-47-01 ON 15DEC24 IN LEX. FLIGHT CREW PLACARD INSTALLED. ON 14JAN25 MAINTENANCE INSTALLED A NEW DOOR ASSY P
- [SDR DALA2024111410953](https://openairdocs.org/sdr/DALA2024111410953), Nov 8, 2024: DOUBLER. CRACKED. -AD- FUSELAGE PLATE SKIN DOUBLERS STA Y=1178 BTW L1-L3 LH CRACKED. ACCOMPLISH ER/A 546495-14AD REV A SECTION III FOR THE INSPECTION OF THE REAR CANTED BULKHEAD 
- [SDR DALA2024083008601](https://openairdocs.org/sdr/DALA2024083008601), Aug 29, 2024: SIGN. INOPERATIVE. FOUND L/H AND R/H OVERWING EXIT DOOR SIDE PANEL IDENTIFIER SIGN INOPERATIVE. CONFIRMED NO POWER AT PIN 1 OF EITHER EEI. VERIFIED GOOD GROUND. POWER SUPPLY B5-11
- [SDR DALA2024021301998](https://openairdocs.org/sdr/DALA2024021301998), Feb 13, 2024: POWER SUPPLY. INOPERATIVE. THE FORWARD OVERWING LOWER EXIT EMERGENCY LIGHTS ON THE LEFT AND RIGHT SIDES ARE INOPERATIVE. MAINTENANCE REPLACED B5-118 BATTERY EMERGENCY POWER SUPPLY PER B71
- [SDR DALA2023121310202](https://openairdocs.org/sdr/DALA2023121310202), Dec 12, 2023: UNKNOWN. UNKNOWN. BOTH EXTERIOR OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHT BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOO
- [SDR DALA2023121310201](https://openairdocs.org/sdr/DALA2023121310201), Dec 12, 2023: UNKNOWN. UNKNOWN. BOTH OF THE FWD EMERGENCY DOOR FLOOR IDENTIFIER LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY AT STA 341 PER B717 AMM 33
- [SDR DALA2023120409905](https://openairdocs.org/sdr/DALA2023120409905), Dec 2, 2023: UNKNOWN. UNKNOWN. THE EXIT SIGN IS MISSING OVER DOOR 1L. MAINTENANCE INSTALLED A NEW EXIT LIGHT COVER PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4996630)
- [SDR DALA2023102608797](https://openairdocs.org/sdr/DALA2023102608797), Oct 25, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY LIGHTS REMAIN ON WHILE IN THE "ARM" POSITION. T/S PER B717 FIM 33-50 AND WDM 33-51, PG 2. L2-788, L2-789, AND L2-740 WERE ON IN FLIGHT. ISOLATED A
- [SDR DALA2023102408721](https://openairdocs.org/sdr/DALA2023102408721), Oct 23, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY LIGHTS OVER 1L AND 1R DOORS CAME ON IN FLIGHT AND WERE FLICKERING AT A FAST FREQUENCY. CEILING LIGHT OUTSIDE FIRST CLASS LAV ALSO FLICKERED ALONG 
- [SDR DALA2023102408720](https://openairdocs.org/sdr/DALA2023102408720), Oct 23, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHTS OVER L1 AND L2 DOORS STAY ILLUMINATED. ALL OTHER EMERGENCY LIGHTS OPERATE NORMALLY. *** CONTRACT MAINTENANCE EVENT - OCM: 271512 *** DISCONNECT
- [SDR DALA2023102308706](https://openairdocs.org/sdr/DALA2023102308706), Oct 21, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY LIGHTS WERE FLICKERING AT THE L1 DOOR, COCKPIT OVERHEAD, AND OVERHEAD PANEL IN THE CABIN DURING FLIGHT. MAINTENANCE INSPECTED BATTERY PACK B5-123 
- [SDR DALA2023101808566](https://openairdocs.org/sdr/DALA2023101808566), Oct 17, 2023: UNKNOWN. UNKNOWN. DURING THE SERVICE CHECK, MAINTENANCE FOUND BOTH EMERGENCY EXIT LIGHTS IN THE FWD GALLEY INOPERATIVE. SLAVED IN A NEW BATTERY CHARGER UNIT FOR BOTH, AND BOTH LI
- [SDR DALA2023101608458](https://openairdocs.org/sdr/DALA2023101608458), Oct 15, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY LIGHTS AT THE TAIL EXIT DOOR AND FORWARD OVERWING EXIT ARE INOPERATIVE. A TERMINAL LUG WAS RE-CONNECTED CORRECTLY AND BATTERY PACKS (B5-235) AND (
- [SDR DALA2023101408443](https://openairdocs.org/sdr/DALA2023101408443), Oct 13, 2023: UNKNOWN. UNKNOWN. WEAR ON INNER SKIN NEAR TO AFT HINGE, ALSO NEAR TO FWD LATCH FITTING, AT AFT CARGO DOOR. SUMMARY OF NRC 00446: INNER SKIN NEAR TO AFT HINGE AT AFT CARGO COMPART
- [SDR DALA2023101408441](https://openairdocs.org/sdr/DALA2023101408441), Oct 12, 2023: UNKNOWN. UNKNOWN. A MISSING CLAMP WAS FOUND ON THE LATCH CABLE (2 EA) FOR THE TAILCONE ASSEMBLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANC
- [SDR DALA2023101408438](https://openairdocs.org/sdr/DALA2023101408438), Oct 11, 2023: UNKNOWN. UNKNOWN. CRACK AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00570: INNER PAN ON STOP #3 AFT EDGE AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 612182-14 REV ORIGI
- [SDR DALA2023101408437](https://openairdocs.org/sdr/DALA2023101408437), Oct 11, 2023: UNKNOWN. UNKNOWN. CORROSION ON INTERNAL PRODUCTION DOUBLER BTW EXTERNAL SKIN AND LOWER PAN, AT AFT CARGO COMPARTMENT LOWER DOOR JAMB. SUMMARY OF NRC 0285: CORROSION LEVEL 2. INTE
- [SDR DALA2023100608225](https://openairdocs.org/sdr/DALA2023100608225), Oct 5, 2023: UNKNOWN. UNKNOWN. CORROSION ON LONGERONS 30, 29L BTW STA 966 TO STA 1002. SUMMARY OF NRC 00565: CORROSION LEVEL 2. CORROSION ON LONGERONS 30, 29L BTW STA 966 TO STA 1002 WERE REP
- [SDR DALA2023100608222](https://openairdocs.org/sdr/DALA2023100608222), Oct 5, 2023: UNKNOWN. UNKNOWN. SEVERAL CORROSION AROUND OF AFT CARGO DOOR JAMB. SUMMARY OF NRC 0007: CORROSION LEVEL 2. AFT CARGO DOOR JAMB WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE
- [SDR DALA2023100408151](https://openairdocs.org/sdr/DALA2023100408151), Sep 29, 2023: UNKNOWN. UNKNOWN. CORROSION REMOVAL RESULTED IN THE FRAME THICKNESS AT STA Y=275 LONG 30 TO BE OUT OF LIMITS. FWD CARGO. SUMMARY OF NRC 00543: CORROSION LEVEL 2. FRAME AT STA Y=2
- [SDR DALA2023100308086](https://openairdocs.org/sdr/DALA2023100308086), Sep 29, 2023: UNKNOWN. UNKNOWN. CRACK ON CAP STA Y=1022RH LONGERON 7RH (INNER STRUCTURE) AT CPAX. SUMMARY OF NRC 00386: CAP STA Y=1022RH LONGERON 7RH INNER STRUCTURE WAS REPAIRED PER ER/A 6118
- [SDR DALA2023100308084](https://openairdocs.org/sdr/DALA2023100308084), Sep 29, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEB STA Y=965 X=-56 AT CPAX. SUMMARY OF NRC 00669: CORROSION LEVEL 2. CUSP WEB STA Y=965 X=-56 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-
- [SDR DALA2023092908003](https://openairdocs.org/sdr/DALA2023092908003), Sep 28, 2023: UNKNOWN. UNKNOWN. CRACK ON FUSELAGE SKIN BTW STA Y=1076 AND LONGERON 14L. SUMMARY OF NRC 00036: CRACK ON FUSELAGE SKIN BTW STA Y=1076 AND LONGERON 14L.WAS REPAIRED PER PRI 611843
- [SDR DALA2023092908000](https://openairdocs.org/sdr/DALA2023092908000), Sep 28, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEB STA Y=370 X=-54 AT CPAX. SUMMARY OF NRC 00668: LEVEL CORROSION 2. CUSP WEB STA Y=370 X=-54 AT CPAX WAS REPAIRED PER B717 SRM-53-00-55-2R P
- [SDR DALA2023092907999](https://openairdocs.org/sdr/DALA2023092907999), Sep 28, 2023: UNKNOWN. UNKNOWN. CRACKS (2 EA) ON PAN (AFT EDGE) BTW STOP #2 AND #4 OF AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00445: PAN (AFT EDGE) BTW STOP #2 AND #4 OF AFT CARGO COMPARTME
- [SDR DALA2023092707959](https://openairdocs.org/sdr/DALA2023092707959), Sep 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON REPAIR DOUBLERS BTW STA Y=991 / 998, BTW STA Y=743 / 751, AND BTW STA X=54 / 60 AT LH WEBS (PAX CABIN). SUMMARY OF NRC 00405: CORROSION LEVEL 2. DO
- [SDR DALA2023092707957](https://openairdocs.org/sdr/DALA2023092707957), Sep 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON FRAME BOTH SIDES, STA 908 BTW L-28R TO L-28L BILGE AREA AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00103: CORROSION LEVEL 2. FRAME BOTH SIDES, STA 90
- [SDR DALA2023092507866](https://openairdocs.org/sdr/DALA2023092507866), Sep 24, 2023: UNKNOWN. UNKNOWN. CORROSION ON WEB STA Y=200 TO 218 BTW X=-42 TO X=-54 SIDE RH AT CPAX. SUMMARY OF NRC 00311: CORROSION LEVEL 2. WEB STA Y=200 TO 218 BTW X=-42 TO X=-54 SIDE RH A
- [SDR DALA2023092507862](https://openairdocs.org/sdr/DALA2023092507862), Sep 23, 2023: UNKNOWN. UNKNOWN. CORROSION ON GENERATION FLOOR PANEL FLOOR PANELS WERE FABRICATED AND REPLACED PER DWG 9952521 REV BB, DWG 9956320 REV G, DWG 9956336 REV G AND B717-200 SRM 51-2
- [SDR DALA2023092507858](https://openairdocs.org/sdr/DALA2023092507858), Sep 23, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP WEB DOUBLERS (5 EA) RH SIDE; (4 EA) BTW STA Y=503 AND STA Y=579 ON X=-56 AND (1 EA) BTW STA Y=794 AND STA Y=813 ON X=-56 AT PAX CABIN. SUMMARY
- [SDR DALA2023092007727](https://openairdocs.org/sdr/DALA2023092007727), Sep 19, 2023: UNKNOWN. UNKNOWN. CORROSION ON WEB STA Y=200 BTW X=0 TO X=12 AT CPAX. SUMMARY OF NRC 00310: CORROSION LEVEL 2. WEB STA Y=200 BTW X=0 TO X=12 AT CPAX WAS REPAIRED PER B717-200 SRM
- [SDR DALA2023092007726](https://openairdocs.org/sdr/DALA2023092007726), Sep 19, 2023: UNKNOWN. UNKNOWN. CORROSION ON WEB STA Y=200 BTW X=0 TO X=12 AT CPAX. SUMMARY OF NRC 00310: CORROSION LEVEL 2. WEB STA Y=200 BTW X=0 TO X=12 WAS REPAIRED PER B717-200 SRM-53-00-0
- [SDR DALA2023092007725](https://openairdocs.org/sdr/DALA2023092007725), Sep 19, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP WEB BTW STA Y=579 AND STA Y=598 ON X=-44 (INTERNAL SIDE) AT PAX CABIN. SUMMARY OF NRC 00329: CUSP WEB BTW STA Y=579 AND STA Y=598 ON X=-44 WAS REP
- [SDR DALA2023091907685](https://openairdocs.org/sdr/DALA2023091907685), Sep 18, 2023: UNKNOWN. UNKNOWN. CRACK ON LONGERON 6RH STA Y=1022RH (INNER STRUCTURE) AT CPAX. SUMMARY OF NRC 00385: LONGERON ON 6RH STA Y=1022RH (INNER STRUCTURE) AT CPAX WAS REPAIRED PER B717
- [SDR DALA2023091907689](https://openairdocs.org/sdr/DALA2023091907689), Sep 17, 2023: UNKNOWN. UNKNOWN. MISSING RELEASE CABLE AND CLIP RETAINERS (2 EA) ON TAILCONE SLIDE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CF

All 198: https://openairdocs.org/aircraft/N961AT/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/N961AT/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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