# N942AT: 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: 55005
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 16, 1999
- Certificate issued: December 31, 2019
- Expires: December 31, 2029
- Mode S code: AD14A8
- 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=942AT
- Page: https://openairdocs.org/aircraft/N942AT

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/N942AT/ads.md

## Information bulletins (advisory) (4 in force)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-18-33](https://openairdocs.org/saib/NM-18-33): Engine Fuel and Control. Issued Dec 17, 2018
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA25LA139](https://openairdocs.org/ntsb/DCA25LA139), Feb 24, 2025: Boeing 717 (N942AT), Atlanta, GA, incident, minor damage, investigation ongoing

## FAA accident and incident reports

None matched to N942AT.

## Service difficulty reports (250, 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 DALA2026070904031](https://openairdocs.org/sdr/DALA2026070904031), Jul 8, 2026: SKIN. CRACKED. CRACK INNER SKIN OF SLAT NR 2 NEAR SLAT TRACK NR 5 STA XOS= 240 AT LEFT WING. REPAIRED INNER SKIN IAW SRM 57-00-00-2R. (1689281) (AIRCRAFT GROUNDED).
- [SDR DALA2025090806623](https://openairdocs.org/sdr/DALA2025090806623), Aug 31, 2025: BATTERY. INOPERATIVE. BATTERY CHARGER FAIL MSG ANNUNCIATED SHORTLY AFTER TAKEOFF IN ATL IT CLEARED IN FLIGHT DURING PRE FLIGHT FOR RETURN LEG IT RE OCCURED CB WAS RESET AT MTC DIRECT
- [SDR DALA2025070104879](https://openairdocs.org/sdr/DALA2025070104879), Jun 30, 2025: EEC. FAULTED. SHIP 9505 -ATB- DUE TO LEFT ENGINE NOT MAKING EPR ON CLIMB OUT. CORRECTIVE ACTION: REPLACE EEC, FUEL FLOW TRANSMITTER, AND FMU. NO HELP, REPLACED FUEL PUMP AND 
- [SDR DALA2025030101575](https://openairdocs.org/sdr/DALA2025030101575), Feb 27, 2025: DOOR. DAMAGED. THE RIGHT SIDE OVERWING EXIT DOOR WAS FOUND DAMAGED. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121
- [SDR DALA2025030101573](https://openairdocs.org/sdr/DALA2025030101573), Feb 27, 2025: ENGINE. FAILED. SHIP 9502 -ATB/IFSD/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC AND RETURNED TO ATL DUE TO SMOKE IN THE CABIN. CREW REPORTED RIGHT ENGINE OIL QTY WENT TO
- [SDR DALA2025020500882](https://openairdocs.org/sdr/DALA2025020500882), Feb 5, 2025: BATTERY. NO TEST. THERE ARE MULTIPLE EMERGENCY EXIT LIGHTS INOPERATIVE IN THE AFT CABIN. MAINTENANCE REPLACED THE BATTERIES IN POWER SUPPLY B5-116 AND B5-260 PER B717 AMM 33-51. 
- [SDR DALA2025010500068](https://openairdocs.org/sdr/DALA2025010500068), Dec 31, 2024: UNKNOWN. FUMES. SHIP 9502 -FUMES/DE- THE FLIGHT ATTENDANT REPORTED A "RUBBER SMELL" COMING FROM ROW 26 IN THE CABIN. SMELL STAYED FAIRLY CONTAINED BUT DID MIGRATE TO OTHER ROWS
- [SDR DALA2025010800167](https://openairdocs.org/sdr/DALA2025010800167), Dec 20, 2024: BLADES. DAMAGED. SHIP 9502 -ATB- THE CREW RETURNED THE AIRCRAFT TO PHL DUE TO MULTIPLE COMPRESSOR STALLS DURING CLIMB OUT. CORRECTIVE ACTION: INSPECTION PERFORMED BORESCOPE INSP
- [SDR DALA2024121811802](https://openairdocs.org/sdr/DALA2024121811802), Dec 18, 2024: BATTERY PACK. INOPERATIVE. BOTH OF THE AFT EMERGENCY OVERWING EXIT DOOR LIGHTS ARE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY (B5-230) PER B717 AMM 33-51-04. LIGHT OPERATIONS CHECK GOO
- [SDR DALA2024121711773](https://openairdocs.org/sdr/DALA2024121711773), Dec 17, 2024: SKIN. DAMAGED. -AD- FUEL LEAK FOUND DURING INSPECTION OF LH WING AFT LOWER SKIN AT XRS=164. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT PER A.A. 
- [SDR DALA2024121711772](https://openairdocs.org/sdr/DALA2024121711772), Dec 17, 2024: SKIN. DAMAGED. -AD- REF TO LOG PAGE #6930830. ORIGINAL WRITE UP: FUEL LEAK FOUND DURING INSPECTION OF LH WING AFT LOWER SKIN AT XRS+164. CONTACT LIAISON ENGINEERING FOR REPAIR
- [SDR DALA2024121711771](https://openairdocs.org/sdr/DALA2024121711771), Dec 16, 2024: TANK. NOT REPORTED. -AD- STEP 16 OF ER/A 622950-14AD REV 0 PRI REV 2. C/W STEP 16 A&B PR1422A2 USED AT 1700 13DEC24. C/W STEP 16 STEP B PR1422B1/2 USED 0100 15DEC24. C/W STEP 16 ST
- [SDR DALA2024121711770](https://openairdocs.org/sdr/DALA2024121711770), Dec 16, 2024: SUPPORT FITTING. CRACKED. -AD- FOUND CRACK INDICATION OF L/H INBOARD FLAP FORWARD HINGE SUPPORT FITTING #8 OPEN BUSHING HOLE DURING BHEC PER PRI 622950-14AD (REV 1) STEP 12 QC2013. REINS
- [SDR DALA2024121711769](https://openairdocs.org/sdr/DALA2024121711769), Dec 16, 2024: SUPPORT FITTING. CRACKED. -AD- FOUND CRACK INDICATION OF L/H INBOARD FLAP FORWARD HINGE SUPPORT FITTING #1 OPEN BUSHING HOLE DURING BHEC PER PRI 622950-14AD (REV 1) STEP 12 QC 2013. REIN
- [SDR DALA2024072907541](https://openairdocs.org/sdr/DALA2024072907541), Jul 27, 2024: BATTERY. INOPERATIVE. THE OVERWING EMERGENCY EVACUATION LIGHT IS INOPERATIVE. OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REPLACED PER B717 AMM 33-51-06. SATISFACTORY TEST
- [SDR DALA2024071607173](https://openairdocs.org/sdr/DALA2024071607173), Jul 15, 2024: FRAME. CRACKED. CRACK ON FRAME AT STA Y=1133 & LONG 2R AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00468: FRAME AT STA Y=1133 & LONG 2R AT AFT ACCESSORY COMPARTMENT WAS REPAIR
- [SDR DALA2024071006984](https://openairdocs.org/sdr/DALA2024071006984), Jul 9, 2024: FINGER DOUBLER. CORRODED. CORROSION ON FINGER DOUBLER BTW STA Y=867 TO STA Y=918 L26L, STA Y=946 TO STA Y=1002 L26L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00407: CORROSION LEVEL 2. FIN
- [SDR DALA2024070806851](https://openairdocs.org/sdr/DALA2024070806851), Jul 6, 2024: LONGERON. CRACKED. CRACK ON LONGERON 2L AT STA Y=1133 ON AFT ACCESORY COMPARTMENT. LONGERON 2L AT STA Y=1133 ON AFT ACCESORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R 
- [SDR DALA2024070506802](https://openairdocs.org/sdr/DALA2024070506802), Jul 3, 2024: FRAME. CRACKED. AIRCRAFT 9502, INITIAL INSPECTION: CRACKED ON CANTED FRAME AFT FACE STA 1200 CANTED, PROJECTION LONG 8LH AFT ACCESSORY COMPARTMENT. CORRECTIVE ACTION: CANTED FR
- [SDR DALA2024070306743](https://openairdocs.org/sdr/DALA2024070306743), Jul 2, 2024: FRAME. CRACKED. CRACK ON CANTED FRAME Y=1200 AND LONG 17R AT AFT ACCESORY COMPARTMENT. CANTED FRAME Y=1200 AND LONG 17R AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER B717-200 SR
- [SDR DALA2024070306742](https://openairdocs.org/sdr/DALA2024070306742), Jul 2, 2024: FRAME. CRACKED. AIRCRAFT 9502, INITIAL INSPECTION: CRACK ON CANTED FRAME Y=1200 AND LONG 17L AT AFT ACCESORY COMPARTMENT. CORRECTIVE ACTION: CANTED FRAME Y=1200 AND LONG 17L AT
- [SDR DALA2024070306741](https://openairdocs.org/sdr/DALA2024070306741), Jul 2, 2024: FRAME. CRACKED. AIRCRAFT 9502, INITIAL INSPECTION: CRACK AT FRAME STA 715 AND L27R CANTED KEEL AREA. CORRECTIVE ACTION: FRAME STA 715 AND L27R CANTED KEEL AREA WAS REPAIRED PER
- [SDR DALA2024070206724](https://openairdocs.org/sdr/DALA2024070206724), Jul 2, 2024: FRAME. CRACKED. CRACKS ON FRAME BTW STA Y=1037 L13L & L14L AT AFT CABIN PAX. FRAME BTW STA Y=1037 L13L & L14L AT AFT CABIN PAX. WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR
- [SDR DALA2024062906602](https://openairdocs.org/sdr/DALA2024062906602), Jun 28, 2024: SKIN. DAMAGED. AIRCRAFT 9502, INITIAL INSPECTION: ELONGATED HOLES 6 E/A ON PAN AND INTERNAL SKIN ON LH FWD EMERGENCY EXIT DOOR. CORRECTIVE ACTION: HOLES 6 E/A ON PAN AND INTER
- [SDR DALA2024062906600](https://openairdocs.org/sdr/DALA2024062906600), Jun 27, 2024: LONGERON. CORRODED. AIRCRAFT 9502, INITIAL INSPECTION: CORROSION ON LONGERON 25R STA Y=323 AT FWD CARGO COMPARTMENT (C1). CORRECTIVE ACTION: LONGERON 25R STA Y=323 AT FWD CARGO COM
- [SDR DALA2024062706575](https://openairdocs.org/sdr/DALA2024062706575), Jun 27, 2024: LONGERON. CRACKED. AIRCRAFT 9502, INITIAL INSPECTION: CRACK ON LONGERON 6R, LONGERON 4L AND LONGERON 5L ON STA Y=1022 AT AFT CABIN PAX. CORRECTIVE ACTION: LONGERON 6R, LONGERON 4L
- [SDR DALA2024062706574](https://openairdocs.org/sdr/DALA2024062706574), Jun 26, 2024: SKIN. CRACKED. AIRCRAFT 9502, INITIAL INSPECTION: CRACK (2EA) ON ANGLE AND INTERNAL SKIN ON LOWER AFT CORNER AT EMERGENCY EXIT DOOR FWD LH. CORRECTIVE ACTION: INTERNAL SKIN ON
- [SDR DALA2024062606514](https://openairdocs.org/sdr/DALA2024062606514), Jun 25, 2024: SKIN. GOUGED. GOUGE WAS FOUND ON SKIN BS 1013. THE SKIN WAS REPAIRED IAW SRM 53-02-01-2R REP 1 PAR 5.B(5)(C) FIG 202 SHEET 15. PERFORMED VISUAL INSPECTION, INITIAL AND REPETI
- [SDR DALA2024062506489](https://openairdocs.org/sdr/DALA2024062506489), Jun 25, 2024: LONGERON. CORRODED. CRACK ON LONGERON 6L STA Y=1022 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00544: LONGERON 6L STA Y=1022 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-0
- [SDR DALA2024062406344](https://openairdocs.org/sdr/DALA2024062406344), Jun 24, 2024: SKIN. CRACKED. CRACK ON INTERNAL SKIN NEAR TO ANGLE, BEAM 1, AT LH FWD OVERWING EMERGENCY EXIT DOOR. SUMMARY OF NRC 00307: INTERNAL SKIN NEAR TO ANGLE, BEAM 1, AT LH FWD OVERW
- [SDR DALA2024062406342](https://openairdocs.org/sdr/DALA2024062406342), Jun 22, 2024: FLOORBEAM. CRACKED. ELONGATED HOLE ON FLOOR BEAM, STA 1022 BTW X=22 TO X=44 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00701: ELONGATED HOLE ON FLOOR BEAM, STA 1022 BTW X=22 TO X
- [SDR DALA2024062106297](https://openairdocs.org/sdr/DALA2024062106297), Jun 20, 2024: LONGERON. CRACKED. CRACK ON LONGERON 8L STA Y=1022 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00543: LONGERON 8L STA Y=1022 AT PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM 
- [SDR DALA2024062106296](https://openairdocs.org/sdr/DALA2024062106296), Jun 20, 2024: LONGERON. CRACKED. CRACK ON LONGERON 13R STA Y=1032 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00545: LONGERON 13R STA Y=1032 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00
- [SDR DALA2024062106295](https://openairdocs.org/sdr/DALA2024062106295), Jun 20, 2024: WEB. CRACKED. PUNCTURE ON MEMBRANE (LWR SURFACE) STA Y=316 AND X=55 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00515: MEMBRANE (LWR SURFACE) STA Y=316 AND X=55 AT PASSENGER
- [SDR DALA2024062006269](https://openairdocs.org/sdr/DALA2024062006269), Jun 20, 2024: DOOR FRAME. CORRODED. CORROSION ON LOWER EDGE AND FWD EDGE DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00297: CORROSION LEVEL 2. DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPAIRE
- [SDR DALA2024061906216](https://openairdocs.org/sdr/DALA2024061906216), Jun 18, 2024: WINDOW FRAME. CRACKED. CRACK ON UPPER REAR CORNER AT CUTOUT OF RH SLIDING WINDOW IN REF TO NRC 00027. SUMMARY OF NRC 00661: UPPER REAR CORNER AT CUTOUT OF RH SLIDING WINDOW WAS REPAIR
- [SDR DALA2024061606114](https://openairdocs.org/sdr/DALA2024061606114), Jun 16, 2024: SEAT TRACK. CORRODED. CORROSION OUT OF LIMITS ON RH INBOARD SEAT TRACK X=-22 BTW STA Y=200-276 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00664: CORROSION LEVEL 2. SEAT TRACK X=-22
- [SDR DALA2024061606113](https://openairdocs.org/sdr/DALA2024061606113), Jun 16, 2024: WINDOW FRAME. CRACKED. DURING INSPECTION AFTER REMOVAL OF INTERNAL CAP UPPER AFT SIDE, A CRACK WAS FOUND ON THE UPPER REAR CORNER AT CUTOUT OF LH SLIDING WINDOW IN REF TO NRC 00024. S
- [SDR DALA2024061606111](https://openairdocs.org/sdr/DALA2024061606111), Jun 14, 2024: WEB. CRACKED. CORROSION ON WEB FROM STA 218 COORDINATE X=55 PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00695: CORROSION LEVEL 2. WEB FROM STA 218 COORDINATE X=55 WAS REPAIRED 
- [SDR DALA2024061406097](https://openairdocs.org/sdr/DALA2024061406097), Jun 13, 2024: CUSP WEB. CORRODED. CORROSION ON CUSP MEMBRANE FROM STA Y=794 TO 813 BTW X=-55 TO -60 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00663: CORROSION LEVEL 2. REPAIR PARTS WER
- [SDR DALA2024061306055](https://openairdocs.org/sdr/DALA2024061306055), Jun 13, 2024: BEAM. CRACKED. CRACK ON BEAM 1 APROX STA Y=192 AT PASSENGER ENTRANCE DOOR L1. SUMMARY OF NRC 00235: BEAM 1 APROX STA Y=192 AT PASSENGER ENTRANCE DOOR L1 WAS REPAIRED PER B717-
- [SDR DALA2024061306054](https://openairdocs.org/sdr/DALA2024061306054), Jun 12, 2024: PAN. CRACKED. CRACK INNER PAN OVER BEAM #3 FWD SIDE OF FWD CARGO DOOR (C1). SUMMARY OF NRC 00227: INNER PAN OVER BEAM #3 FWD SIDE OF FWD CARGO DOOR (C1) WAS REPAIRED PER B717
- [SDR DALA2024011100474](https://openairdocs.org/sdr/DALA2024011100474), Jan 10, 2024: UNKNOWN. UNKNOWN. CAPTAIN WINDSHIELD ARCED AND OUTER PANEL CRACKED ON DESCENT. MAINTENANCE REPLACED THE CAPT LH WINDSHIELD IAW B717 AMM 56-11. MAINTENANCE REPLACWD THE LH WINDSHI
- [SDR DALA2023092707960](https://openairdocs.org/sdr/DALA2023092707960), Sep 26, 2023: UNKNOWN. UNKNOWN. CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 1 DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE ACTIVATED. MAINTENANCE REPLACED THE FWD EMERGENCY LIGHT BATTERY ASSY
- [SDR DALA2023050803561](https://openairdocs.org/sdr/DALA2023050803561), May 2, 2023: UNKNOWN. UNKNOWN. SURFACE CORROSION ON SKIN CLIP STA 1022, BETWEEN STR 25-26L. - MARKED- SUMMARY NRC: 077-0001:0514-2001/010 00377 CLEANED AREA, EDGE SEALED, AND APPLIED CIC PER 
- [SDR DALA2023052204050](https://openairdocs.org/sdr/DALA2023052204050), May 1, 2023: UNKNOWN. UNKNOWN. INNER LAP SKIN HAS SURFACE CORROSION. STA 1006-1047, JUST ABOVE STR 26L. -MARKED-. SUMMARY SEE NRC 077-0001:0514-2001/008 00375: REPLACED INNER SKIN SIN LAP FIN
- [SDR DALA2023051203745](https://openairdocs.org/sdr/DALA2023051203745), May 1, 2023: UNKNOWN. UNKNOWN. FOUND STR 27L AND 28L END CLIPS CORRODED AT STA 1053. SUMMARY SEE NRC 077-0001:0514-2001/006 00369: REPLACED END CLIPS AT STR 27L AND 28L STA 1053 PER B717 SRM 
- [SDR DALA2023050203397](https://openairdocs.org/sdr/DALA2023050203397), May 1, 2023: UNKNOWN. UNKNOWN. ORROSION ON STR 26L BETWEEN STA 1022-1043. -MARKED-. INSTALLED STRINGER 26L AND SPLICE IAW B717 SRM 53-00-05-2R PROCEDURE 2. (LP #2746142)
- [SDR DALA2023050203394](https://openairdocs.org/sdr/DALA2023050203394), May 1, 2023: UNKNOWN. UNKNOWN. AREAS OF CORROSION ON STR 27L, BETWEEN STA 1022-1050. -MARKED-. INSTALLED STRINGER 27L AND SPLICE IAW B717 SRM 53-00-05-2R PROCEDURE 2. (LP #2746146)
- [SDR DALA2023042703286](https://openairdocs.org/sdr/DALA2023042703286), Apr 22, 2023: UNKNOWN. UNKNOWN. TASK CARD NUMBER: 001-0231:2520-1002/002 REF NR 00325. FOUND CORROSION ON SKIN UNDER FORWARD DRAIN MAST. CORROSION LEVEL 2. REPLACED DOUBLER AND INTERCOSTAL PER

All 250: https://openairdocs.org/aircraft/N942AT/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/N942AT/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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