# N940AT: 1999 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: 55004
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 3, 1999
- Certificate issued: December 31, 2019
- Expires: December 31, 2029
- Mode S code: AD0D3A
- 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=940AT
- Page: https://openairdocs.org/aircraft/N940AT

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/N940AT/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 N940AT.

## FAA accident and incident reports

None matched to N940AT.

## Service difficulty reports (243, 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 DALA2026102005747](https://openairdocs.org/sdr/DALA2026102005747), Oct 19, 2026: ENGINE. FAILED. DECLARED AN EMERGENCY AND DIVERTED TO BNA DUE TO RIGHT ENGINE FAILURE. INSPECTED RIGHT ENGINE CHIP DETECTOR AND FOUND METAL DEBRIS. R & R ENGINE #2 IAW AMDS JIC
- [SDR DALA2026101605699](https://openairdocs.org/sdr/DALA2026101605699), Oct 16, 2026: WIRE. BROKEN. DURING SVC CHK FOUND OVERHEAD EMERGENCY LIGHT AT ROW 27/28 INOPERATIVE, BROKEN WIRE. WIRE PULLED OUT OF CONTACT AT CONNECTOR, STRIPPED WIRE TO APPROPRIATE DIMS 
- [SDR DALA2026100605533](https://openairdocs.org/sdr/DALA2026100605533), Oct 4, 2026: PUMP. FAULTED. THE FLIGHT RETURNED TO ATL DUE TO A RIGHT HYDRAULIC TEMP HIGH MESSAGE. MAINTENANCE REPLACED THE AUX PUMP, THE PTU, AND THE RUDDER HYDRAULIC SHUTOFF VALVE. ALSO 
- [SDR DALA2026092505348](https://openairdocs.org/sdr/DALA2026092505348), Sep 24, 2026: SKIN. CRACKED. CRACKS WERE FOUND ON FUSELAGE SKIN AND INNER DOUBLER -39, BS 1022 BETWEEN LONGERONS 13-14R, COMPLIED WITH ER/A 577210-14. (1830070) (AIRCRAFT GROUNDED).
- [SDR DALA2026062903843](https://openairdocs.org/sdr/DALA2026062903843), Jun 27, 2026: OXYGEN MASK. NO TEST. CAPT O2 MASK FAILED TEST. R & R FO'S CREW O2 MASK PER B717 AMM 35-23. (6545751) (AIRCRAFT GROUNDED).
- [SDR DALA2026060203341](https://openairdocs.org/sdr/DALA2026060203341), May 30, 2026: SKIN. DAMAGED. ELONGATED HOLES ON EXTERNAL FUSELAGE SKIN BTW STA Y=813-832 AND LONG 26LH. PERMANENT REPAIR AND PRI 634243-14 (1621845) (AIRCRAFT GROUNDED)
- [SDR DALA2026060203338](https://openairdocs.org/sdr/DALA2026060203338), May 29, 2026: DOUBLER. CORRODED. CORROSION ON PRODUCTION DOUBLER BTW STA Y 813. FUSELAGE WAS REPLACED PER B717-200 SRM 51-41-05 (1620108) (AIRCRAFT GROUNDED)
- [SDR DALA2026051903062](https://openairdocs.org/sdr/DALA2026051903062), May 15, 2026: PAN. CRACKED. CRACK ON UPPER DOOR JAMB PAN AT LH FWD OVERWING EMERGENCY EXIT CUT OUT AT PAXCABIN. CRACK ON UPPER DOOR JAMB PAN AT LH FWD OVERWING EMERGENCY EXIT CUT OUT AT PA
- [SDR DALA2026051703031](https://openairdocs.org/sdr/DALA2026051703031), May 14, 2026: SUPPORT. CORRODED. CORROSION ON FILLET FAIRING SUPPORT ( UPPER/LOWER , FWD/AFT FACE) AT STA 832 BTW L29 AND L26 LH AND STA 832 BTW. CORROSION LEVEL 2, FILLET FAIRING SUPPORT (UPPE
- [SDR DALA2026051703028](https://openairdocs.org/sdr/DALA2026051703028), May 12, 2026: FRAME. CRACKED. CRACK ON FRAME STA Y=1037 AND LONGERON 17L AT PASSENGER CABIN. CRACK ON FRAME STA Y=1037 AND LONGERON 17L WAS REPAIRED PER ER/A 633987-14 REV ORIG. AND PRI 6339
- [SDR DALA2026051102943](https://openairdocs.org/sdr/DALA2026051102943), May 7, 2026: LONGERON SPLICE. CORRODED. CORROSION ON LONGERON SPLICE (LONG 30) AT Y= 1009 ON AFT CARGO COMPARTMENT. DAMAGED AREA REPAIRED PER B717-200 SRM 51-41-05 (1581979) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502820](https://openairdocs.org/sdr/DALA2026050502820), May 2, 2026: FUEL TANK. CRACKED. CRACK ON WEB FUEL TANK X=56 APROX STA Y =696 AT LH CENTRAL FUEL TANK. REPAIRED PER ER/A 633561-14AD (1573556) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502819](https://openairdocs.org/sdr/DALA2026050502819), May 1, 2026: PAN. CRACKED. CRACK ON OUTER PAN (UPPER EDGE) UNDER MID BRACKET (CUTOUT AREA STA Y972 APPROX) AT AFT CARGO COMPARTMENT DOOR. REPAIR PER ER/A 633588-14 (1573299) (AIRCRAFT GRO
- [SDR DALA2026050502815](https://openairdocs.org/sdr/DALA2026050502815), Apr 29, 2026: FRAME. CRACKED. CRACK ON FRAME STA Y=1037 ON LONGERON 17R AT CPAX. REPAIRED PER SRM 53-20-07 (1569682) (AIRCRAFT GROUNDED)
- [SDR DALA2026050502813](https://openairdocs.org/sdr/DALA2026050502813), Apr 29, 2026: HINGE. CORRODED. AFTER REMOVAL BOLT ON RH WING FLAP OUTBD HINGE PIVOT AREA BS 331.1 WAS FOUND CORROSION, TOOL MARKS, ELONGATED HOLES ON HOUSING ON INBD/OUTBD FACE AT RH WING. RT
- [SDR DALA2026042302605](https://openairdocs.org/sdr/DALA2026042302605), Apr 22, 2026: PAN. CRACKED. CRACK ON INNER PAN (AFT EDGE IN BEAM 2) AT FWD PASSENGER DOOR. REPAIRED PER B717-200 S.R.M. 52-10-02 (1557418) (AIRCRAFT GROUNDED)
- [SDR DALA2026042202562](https://openairdocs.org/sdr/DALA2026042202562), Apr 20, 2026: CUSP WEB. DAMAGED. LEFT FLOOR CUPS WEB AREA (UPPER/LOWER SURFACES) BTW STA 876 TO 884 WITH ORIGINAL THICKNESS IS 0.020 INCH AND MINIMUM REMAINING THICKNESS IS 0.008 INCH THEREFORE
- [SDR DALA2026042102511](https://openairdocs.org/sdr/DALA2026042102511), Apr 17, 2026: FLOOR SUPPORT. CRACKED. CRACKED INTERCOSTAL OF FLOOR STRUCTURE BTW STA Y= 1002 TO 1022 X=0 AT CPAX. REPAIRED PER B717-200 SRM 51-70-11 (1549483) (AIRCRAFT GROUNDED)
- [SDR DALA2026042902731](https://openairdocs.org/sdr/DALA2026042902731), Apr 16, 2026: HINGE FITTING. DAMAGED. FWD HINGE FITTING #3, XW=-333.148 / INBD A OUTBD LUG / ELONGATED HOLES AND CORROSION. ASSOCIATED ER/A 00-633572 (1559456) (AIRCRAFT GROUNDED)
- [SDR DALA2026042102509](https://openairdocs.org/sdr/DALA2026042102509), Apr 16, 2026: SKIN. CRACKED. CRACK ON EXTERNAL SKIN ON STA Y=1087 BTW LONG13L AND LONG14L AT AFT UPPER FUSELAGE. REPAIRED PER ER/A 633315- 14 (1548241) (AIRCRAFT GROUNDED)
- [SDR DALA2026042902732](https://openairdocs.org/sdr/DALA2026042902732), Apr 14, 2026: SPAR CAP. CORRODED. RH HORIZONTAL STABILIZER REAR SPAR LOWER CAP, HOLES #29 AND #30, XHR=-7.234 / CORROSION. RREPAIRED PER ER/A 00-633497. (1559543) (AIRCRAFT GROUNDED)
- [SDR DALA2026041702448](https://openairdocs.org/sdr/DALA2026041702448), Apr 14, 2026: CUSP WEB. CRACKED. CRACK ON RH FLOOR CUPS WEB UNDER REPAIRED DOUBLER STA 343, X=-55.5 APROX AT PAX CABIN. DAMAGED AREA REMOVED AND INSTALLED PER B717-200 SRM 53-00-55. (1544260) (
- [SDR DALA2026041702446](https://openairdocs.org/sdr/DALA2026041702446), Apr 13, 2026: CUSP WEB. CORRODED. CORROSION ON RH FLOOR CUPS WEB AREA (UPPER/ LOWER SURFACES) STA 229, BTW-X =55.5 -X=44.5 APROX AT PAX CABIN. REPAIRED PER B717-200 SRM 53-00-55 (1542943) (AIRCR
- [SDR DALA2026041402365](https://openairdocs.org/sdr/DALA2026041402365), Apr 12, 2026: CUSP WEB. CRACKED. CRACK ON CUSP WEB BTW STA Y= 715/719 AND BTW STA X= 44/46 WING BOX AREA AT C. PAX . CUSP WEB BTW STA Y= 715/719 AND BTW STA X= 44/46 WING BOX AREA AT C. PAX WAS
- [SDR DALA2026041402342](https://openairdocs.org/sdr/DALA2026041402342), Apr 9, 2026: WEB. CORRODED. CORROSION ON RT FLOOR CUPS WEB AREA (UPPER/ LOWER SURFACES) STA 256 BTW-X =55.5 -X=44.5 APROX AT PAX CABIN. REPAIRED IAW SRM 53-00-55-2R (1536178) (AIRCRAFT GRO
- [SDR DALA2026040802225](https://openairdocs.org/sdr/DALA2026040802225), Apr 6, 2026: BEAM. CRACKED. CRACK ON BEAM NR 2 (AFT EDGE) ON L1 DOOR AT CPAX.. BEAM NR 2 (AFT EDGE) ON L1 DOOR AT CPAX WAS REPAIRED PER B717-200 S.R.M. 52-10-02 (1531786) (AIRCRAFT GROUNDE
- [SDR DALA2025122309342](https://openairdocs.org/sdr/DALA2025122309342), Dec 20, 2025: PRESSURE SWITCH. FAULTED. ATB - RIGHT ENGINE SYSTEM FAIL MESSAGE ALONG WITH A RIGHT ENGINE FUEL FILTER MESSAGE ON CLIMB OUT. INSPECTED FILTERS WITH NO DEBRIS NOTED. BOTH HIGH AND LOW PRE
- [SDR DALA2025111808419](https://openairdocs.org/sdr/DALA2025111808419), Nov 13, 2025: PIN. MISSING. SPRING AND PIN MISSING FROM L1 GIRT BAR FLOOR FITTING (AFT ONE). REPLACED L1 CABIN EVACUATION SLIDE LATCH (AFT ONE) IAW CMM 25-60-02. (7585426)
- [SDR DALA2025040902755](https://openairdocs.org/sdr/DALA2025040902755), Apr 5, 2025: SKIN. CRACKED. CRACK ON FUSELAGE EXTERNAL SKIN LOCATED ON STA Y=1037 APROX BTW L=13R AND L=14R. SUMMARY OF NRC 00056: CRACK ON FUSELAGE EXTERNAL SKIN LOCATED ON STA Y=1037 APR
- [SDR DALA2025040802701](https://openairdocs.org/sdr/DALA2025040802701), Apr 5, 2025: FASTENER. LOOSE. CRACK AND LOOSE FASTENERS (HI-LOCKS) ON EXTERNAL REPAIR DOUBLER ON STA Y=1022 AND BTW LONGERONS 13R/14R AT FUSELAGE WERE FOUND DURING REPETITIVE INSPECTION PER 
- [SDR DALA2025100807324](https://openairdocs.org/sdr/DALA2025100807324), Apr 4, 2025: LUG. CORRODED. AFTER REMOVAL OF INBOARD AND OUTBOARD BUSHINGS OF HINGES LOCATED AT XE= 206 AND XE= 223, CORROSION WAS FOUND ON INBOARD AND OUTBOARD LUGS OF HINGE XE= 206, AND 
- [SDR DALA2025033102353](https://openairdocs.org/sdr/DALA2025033102353), Mar 29, 2025: LONGERON. CRACKED. CRACK LONGERON 4LH & STA Y=1152 AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00090: LONGERON 4LH BTW STA Y=1169 AND STA Y=1138 WAS REPAIRED PER B717-200 SRM 53-0
- [SDR DALA2025033102347](https://openairdocs.org/sdr/DALA2025033102347), Mar 26, 2025: SKIN. DENTED. SEVERAL DENTS ON EXTERNAL SKIN OF FWD CARGO DOOR. SUMMARY OF NRC 00025: EXTERNAL SKIN OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-00-01-2R PROCEDURE 8 RE
- [SDR DALA2025040802695](https://openairdocs.org/sdr/DALA2025040802695), Mar 22, 2025: RELEASE MECH. OUT OF ADJUST. THE TAILCONE RELEASE MECHANISM CAM WAS FOUND TO BE INCORRECTLY ADJUSTED: PIN ALIGMENT IS MORE THAN 38.5. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE P
- [SDR DALA2025032402185](https://openairdocs.org/sdr/DALA2025032402185), Mar 22, 2025: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTALS (2 EA) AND INTERNAL DOUBLER BTW STA Y=196/212 AND BTW LONGERONS 28R/29R AT E/E COMPARTMENT. SUMMARY OF NRC 00077: CORROSION LEVEL 2. R
- [SDR DALA2024121011569](https://openairdocs.org/sdr/DALA2024121011569), Dec 9, 2024: WIRE. DAMAGED. SHIP 9501 -ATB/FUME- THE FLIGHT CREW RETURNED THE AIRCRAFT TO ATL DUE TO AN ACRID BURNING SMELL IN THE CABIN. CORRECTIVE ACTION: MAINTENANCE REPAIRED DAMAGED WI
- [SDR DALA2024120911540](https://openairdocs.org/sdr/DALA2024120911540), Dec 8, 2024: POWER SUPPLY. FAULTED. SEVERAL EMERGENCY LIGHTS ARE INOPERATIVE NEAR FWD SERVICE DOOR. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY UNIT AT CANNON PLUG P1-259 PER B717 AMM 22
- [SDR DALA2024120311396](https://openairdocs.org/sdr/DALA2024120311396), Dec 1, 2024: SHIP 9501 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC GOING INTO ATL DUE TO "PSEU FAIL" MESSAGE AND THE RESULTANT FLAPS-UP LANDING AS PER THE QRH. 
- [SDR DALA2024120211377](https://openairdocs.org/sdr/DALA2024120211377), Nov 30, 2024: SENSOR. INOPERATIVE. SHIP 9501 -MISC/DE- THE FLIGHT CREW DECLARED EMERGENCY WITH ATC INTO CHA DUE TO THE "PSEU FAIL" MESSAGE. A FLAPS-UP LANDING FOLLOWED PER THE QRH. CORRECTIVE ACT
- [SDR DALA2024120911533](https://openairdocs.org/sdr/DALA2024120911533), Nov 21, 2024: NONE. NONE. -AD- ACCOMPLISH ER/A 539703-14AD REV A SEC II. ACCOMPLISH ER/A 539703-14AD REV A SEC II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATE
- [SDR DALA2024100709735](https://openairdocs.org/sdr/DALA2024100709735), Oct 7, 2024: BATTERY PACK. INOPERATIVE. THE OVERHEAD EMERGENCY EGRESS LIGHTS ARE INOPERATIVE FROM ROW 24 THROUGH TO ROW 29. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AT 25DEF (B5-231) PER B717 A
- [SDR DALA2024100709734](https://openairdocs.org/sdr/DALA2024100709734), Oct 7, 2024: LENS. MISSING. THE OVERHEAD EMERGENCY EXIT LIGHT DIFFUSER IS MISSING AT 25/26DEF. DEFERRED 25/26DEF OVERHEAD EMERGENCY EXIT LIGHT DIFFUSER PER NEF 33-51-02. DEFERRAL REMARKS N
- [SDR DALA2024071006987](https://openairdocs.org/sdr/DALA2024071006987), Jul 7, 2024: SKIN. PUNCTURED. ON WALKAROUND FOUND PUNCTURE IN SKIN AT STATION Y256 BETWEEN LONGERONS L18 AND L17. REMOVED THE PUNCTURED REPAIR SKIN AT FR 229-FR245 BETWEEN STGR L16L & L18L P
- [SDR DALA2024040203984](https://openairdocs.org/sdr/DALA2024040203984), Mar 31, 2024: CONNECTOR. DIRTY. SHIP 9501 -MISC/DE- THE "TAILCONE UNLOCK" MASTER CAUTION ILLUMINATED THREE TIMES DURING FLIGHT. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED BY ATC F
- [SDR DALA2024011000452](https://openairdocs.org/sdr/DALA2024011000452), Jan 9, 2024: UNKNOWN. UNKNOWN. SHIP 9501 -MISC/DE- AT 13K, THE F/A REPORTED A STRONG ELECTRICAL SMELL COMING FROM FORWARD GALLEY. COCKPIT FLIGHT CREW ALSO SMELLED IT AND DONNED O2 MASKS. SOON
- [SDR DALA2023112809768](https://openairdocs.org/sdr/DALA2023112809768), Nov 28, 2023: UNKNOWN. UNKNOWN. THE GATE AGENT COULD NOT OPEN THE MAIN CABIN DOOR. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.7
- [SDR DALA2023051603854](https://openairdocs.org/sdr/DALA2023051603854), May 13, 2023: UNKNOWN. UNKNOWN. CORROSION ON AFT PRESSURE BULKHEAD FORWARD FACE LOWER SECTION STA Y=1053 BETWEEN LONGERON 27L AND 27R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00116: CORROSION 
- [SDR DALA2023051103712](https://openairdocs.org/sdr/DALA2023051103712), May 10, 2023: UNKNOWN. UNKNOWN. AFTER REMOVING DOUBLER, CORROSION WAS FOUND ON TEE CAP AFT PRESSURE GROUP BULKHEAD FORWARD FACE LOWER SECTION STA=1053 BTW LONGERON 25R AND 28R AFT CARGO COMPAR
- [SDR DALA2023051003666](https://openairdocs.org/sdr/DALA2023051003666), May 9, 2023: UNKNOWN. UNKNOWN. CORROSION ON WEB AFT FACE LOWER SECTION STA Y=1053 BETWEEN LONGERON 28L AND 28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00115: CORROSION LEVEL II. WEBS #991556
- [SDR DALA2023050903615](https://openairdocs.org/sdr/DALA2023050903615), May 9, 2023: UNKNOWN. UNKNOWN. CORROSION AT END LONGERON CLIPS STA 1032 (5 EA), 27RH, 28RH, 29RH, 28LH, AND 26RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00176: LEVEL CORROSION 2. END LONGERO

All 243: https://openairdocs.org/aircraft/N940AT/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/N940AT/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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