# N935AT: 2000 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: 55069
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 26, 2000
- Certificate issued: July 31, 2024
- Expires: July 31, 2031
- Mode S code: ACF84E
- 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=935AT
- Page: https://openairdocs.org/aircraft/N935AT

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/N935AT/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 ERA10LA041](https://openairdocs.org/ntsb/ERA10LA041), Oct 26, 2009: Boeing 717-200 (N935AT), Pleasant Grove, NC, no damage. Probable cause: The captain's excessive maneuver in response to a traffic alert and collision avoidance system (TCAS) alert, which resulted in a serious injury to a flight attendant. Contributing to the accident was…

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20091026051539A](https://openairdocs.org/incident/20091026051539A), Oct 26, 2009: Boeing 717-200 (N935AT), Kinston, NC, No damage. The event took place approximately 20 NM south of Kinston (iso), at 16:01Z. The flight was experiencing moderate turbulence at FL350 and the crew requested a…

## Service difficulty reports (219, 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 DALA2026050502818](https://openairdocs.org/sdr/DALA2026050502818), May 1, 2026: ELEC CONNECTOR. LOOSE. SEVERAL EMERGENCY LIGHTS DO NOT TURN ON, ALONG CPAX INCLUDING DOORS AND CEILING PANELS ALSO 2 UPPER LIGHTS ON AFT ACCESORIES COMPARTMENT. CONNECTOR P1-1217 AND 
- [SDR DALA2025121009013](https://openairdocs.org/sdr/DALA2025121009013), Dec 8, 2025: HOUSING. DIRTY. ATB, CREW REPORTED CABIN ODOR IN AFT CABIN ON TAKEOFF CLIMB. BORESCOPE BOTH ENGINES, NO DEFECTS NOTED. INSPECTED THE BOTH PACKS COALESCER BAGS AND FOUND THE HOU
- [SDR DALA2025120508919](https://openairdocs.org/sdr/DALA2025120508919), Dec 4, 2025: UNKNOWN. ODOR. RETURNED TO STL DUE TO BURNT OIL SMELL AT 300FT AFTER GEAR RETRACTION. UNABLE TO DUPLICATE ODOR AT GATE RUNNING APU OR ENGINES. GATHERING PARTS AND P-TRACK FROM
- [SDR DALA2024040804184](https://openairdocs.org/sdr/DALA2024040804184), Apr 8, 2024: LENS. WRONG PART. PASSENGER EXIT SIGN IS MISSING THE WORD "EXIT". MISSING FROM LIGHT NEAREST CLOSET. MAINTENANCE FOUND THAT THE SIGN HAD BEEN INSTALLED BACKWARDS. ADJUSTED FWD CA
- [SDR DALA2024032703839](https://openairdocs.org/sdr/DALA2024032703839), Mar 25, 2024: CUSP WEB. CORRODED. CORROSION ON RH CUSP ANGLE BTW STA Y=160-169 AND STA Y=200 AT PAX CABIN. SUMMARY OF NRC 00489: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=160-169 AND STA Y=200 AT 
- [SDR DALA2024032503736](https://openairdocs.org/sdr/DALA2024032503736), Mar 24, 2024: SKIN. DEBONDED. TWO DISBONDS WERE FOUND OF: 0.500 IN LENGTH .X 0.500 IN. WIDTH. ON DENTS LOWER SKIN AT LH CENTER FLAP VANE 26.500 IN. INBOARD EDGE, 12.500 IN. TRAILING EDGE AND
- [SDR DALA2024032503735](https://openairdocs.org/sdr/DALA2024032503735), Mar 24, 2024: FRAME. CORRODED. CORROSION ON FRAME FROM STA 1022 LONGERON 30 CORDENATED X=-4 TO X=4. SUMMARY OF NRC 00708: CORROSION LEVEL 2. FRAME FROM STA 1022 LONGERON 30 CORDENATED X=-4 TO
- [SDR DALA2024032503734](https://openairdocs.org/sdr/DALA2024032503734), Mar 23, 2024: SKIN. CRACKED. CRACK ON SKIN STA Y=370 BTW L20 AND L22 APROX AT FWD DOOR CARGO COMPARMENT. SUMMARY OF NRC 00227: SKIN STA Y=370 BTW L20 AND L22 APROX AT FWD DOOR CARGO COMPARM
- [SDR DALA2024050805016](https://openairdocs.org/sdr/DALA2024050805016), Mar 22, 2024: WEB. DAMAGED. ELONGATED HOLES ON WEB BTW STA 370 TO 360 AND LONGERONS 24 RH TO 26 RH AT CUT OUT FORWARD CARGO COMPARTMENT DOOR (CCD). SUMMARY OF NRC 00131: WEB BTW STA 370 TO
- [SDR DALA2024032303702](https://openairdocs.org/sdr/DALA2024032303702), Mar 22, 2024: RIB. WORN. WEAR ON RIBS (3 EA) BETWEEN STA XIS 174 TO XIS 186 INSIDE FIXED LEADING-EDGE AT LH WING. SUMMARY OF NRC 00621: RIBS (3 EA) BETWEEN STA XIS 174 TO XIS 186 INSIDE
- [SDR DALA2024032203635](https://openairdocs.org/sdr/DALA2024032203635), Mar 21, 2024: SEAT TRACK. CORRODED. CORROSION ON RH SEAT TRACKS X-54.0 BTW STA Y=200-256 AT PAX CABIN. SUMMARY OF NRC 00493: CORROSION LEVEL 2. RH SEAT TRACKS X-54.0 BTW STA Y=200-256 AT PAX CABIN
- [SDR DALA2024032103594](https://openairdocs.org/sdr/DALA2024032103594), Mar 21, 2024: DIAPHRAGM. CORRODED. CORROSION ON RIGHT DIAPHRAGM ON STA X=-44 AND X=-56 FROM STA Y 200 TO Y 218 AT W1 AREA. SUMMARY OF NRC 00697: CORROSION LEVEL 2. RIGHT DIAPHRAGM ON STA X=-44 AN
- [SDR DALA2024032103593](https://openairdocs.org/sdr/DALA2024032103593), Mar 21, 2024: GUIDE VANE. PUNCTURED. PUNCTURE ON AFT MOVABLE GUIDE VANE AT RH WING. SUMMARY OF NRC 00042: AFT MOVABLE GUIDE VANE AT RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REP
- [SDR DALA2024032103591](https://openairdocs.org/sdr/DALA2024032103591), Mar 21, 2024: SKIN. CRACKED. CRACKS ON FUSELAGE SKIN STA 1076.0 AND STA 1087 OVER LONGERON 14 RH. FUSELAGE SKIN STA 1076.0 AND STA 1087 OVER LONGERON 14 RH WAS REPAIRED PER ERA 616042-14 RE
- [SDR DALA2024032103577](https://openairdocs.org/sdr/DALA2024032103577), Mar 16, 2024: DIAPHRAGM. CRACKED. CRACK AND PUNCTURE ON DIAPHRAGM BTW STA X=-44 AND X=-56 FROM STA Y=257 APPROX AT PASSENGER CABIN. SUMMARY OF NRC 00707: DIAPHRAGM BTW STA X=-44 AND X=-56 FROM S
- [SDR DALA2024031503376](https://openairdocs.org/sdr/DALA2024031503376), Mar 15, 2024: FLOOR SUPPORT. CORRODED. CORROSION ON CABIN FLOOR SUPPORTS AT X=-53, STA Y=160 TO 200; X=-15 TO -40, STA Y=180; STA Y=200, X=-44.5 TO -55; AND X=-12 STA Y=210. SUMMARY OF NRC 00677: COR
- [SDR DALA2024031503375](https://openairdocs.org/sdr/DALA2024031503375), Mar 14, 2024: FRAME. CRACKED. CRACK ON FRAME STA Y=64 APPROX AND X=18 LH SIDE AT NLG W/W. SUMMARY OF NRC 00705: FRAME STA Y=64 APPROX AND X=18 LH SIDE AT NLG W/W WAS REPAIRED PER B717-200 SR
- [SDR DALA2024031403329](https://openairdocs.org/sdr/DALA2024031403329), Mar 14, 2024: WEB. CORRODED. CORROSION ON DIAPHRAGM MEMBRANE APPROX -X=53 STA Y=156 AT PAX CABIN. SUMMARY OF NRC 00488: CORROSION LEVEL 2. DIAPHRAGM MEMBRANE APPROX -X=53 STA Y=156 AT PAX C
- [SDR DALA2024031403328](https://openairdocs.org/sdr/DALA2024031403328), Mar 13, 2024: TEE ANGLE. CORRODED. CORROSION ON ANGLE "TEE" STA 1053 LONGERON 30 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00559: CORROSION LEVEL 2. ANGLE "TEE" STA 1053 LONGERON 30 AT AFT CARGO CO
- [SDR DALA2024031303281](https://openairdocs.org/sdr/DALA2024031303281), Mar 13, 2024: PAN. CRACKED. CRACK ON PAN BTW STA Y=427 AND BEAM 5 APROX AT FWD DOOR CARGO COMPARMENT. SUMMARY OF NRC 00226: PAN BTW STA Y=427 AND BEAM 5 APROX AT FWD DOOR CARGO COMPARMENT 
- [SDR DALA2024031303279](https://openairdocs.org/sdr/DALA2024031303279), Mar 12, 2024: FRAME. CRACKED. CRACK ON CANTED FRAME ON STA 1200 APROX. BTW L-17L AND L-18L AT AFT INTERNAL FUSELAGE. SUMMARY OF NRC 00232: CANTED FRAME ON STA 1200 APROX. BTW L-17L AND L-18L
- [SDR DALA2024030803184](https://openairdocs.org/sdr/DALA2024030803184), Mar 8, 2024: SEAT TRACK. CORRODED. CORROSION ON LH OTBD SEAT TRACK ON STA Y=636 AT CABIN PAX. SUMMARY OF NRC 00605: LH OTBD SEAT TRACK ON STA Y=636 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-2
- [SDR DALA2024030803183](https://openairdocs.org/sdr/DALA2024030803183), Mar 7, 2024: LONGERON. CORRODED. CORROSION ON LONGERON END STA Y=1050, LONG 28RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00654: CORROSION LEVEL 2. LONGERON END STA Y=1050, LONG 28RH AT AFT CAR
- [SDR DALA2024030703126](https://openairdocs.org/sdr/DALA2024030703126), Mar 6, 2024: CUSP WEB. CORRODED. CORROSION ON RH CUSP WEB UPPER AND LOWER SUARFACE FROM STA Y=489 TO STA Y=494 COORDINATES X=-44 TO COORDINATES X=-60 (CAB PAX). SUMMARY OF NRC 00668: CORROSION 
- [SDR DALA2024030603062](https://openairdocs.org/sdr/DALA2024030603062), Mar 5, 2024: INTERCOSTAL. CRACKED. CRACK INTERCOSTAL ON INNER STRUCTURE STA 184 BTW BEAMS #4 AND 5 AT PASSENGER DOOR 1L. SUMMARY OF NRC 00144: INTERCOSTAL ON INNER STRUCTURE STA 184 BTW BEAMS #4 
- [SDR DALA2024030503005](https://openairdocs.org/sdr/DALA2024030503005), Mar 4, 2024: CUSP WEB. CRACKED. CRACK ON LH CUSP WEB LOCATED ON OUTB SEAT TRACK SPLICE AREA STA 595 AT PASSENGER CABIN. SUMMARY OF NRC 00639: LH CUSP WEB STA 595 AT PASSENGER CABIN WAS REPAIRE
- [SDR DALA2024030402943](https://openairdocs.org/sdr/DALA2024030402943), Mar 3, 2024: DOUBLER. CORRODED. CORROSION ON DOUBLER BELOW TEE FITTING STA 1053 LONGERON 30 AT AFT BULKHEAD. SUMMARY OF NRC 00562: CORROSION LEVEL 2. DOUBLER BELOW TEE FITTING STA 1053 LONGERO
- [SDR DALA2024030402941](https://openairdocs.org/sdr/DALA2024030402941), Mar 3, 2024: CUSP WEB. DENTED. DENT ON RH CUSP WEB APPROX STA Y=355, Y=441 AND X-44/-60 AT PAX CABIN. SUMMARY OF NRC 00400: RH CUSP WEB APPROX STA Y=355, Y=441 AND X-44/-60 AT PAX CABIN WAS R
- [SDR DALA2024030402938](https://openairdocs.org/sdr/DALA2024030402938), Mar 2, 2024: CUSP WEB. CORRODED. CORROSION ON LH CUSP WEB STA Y 636 AT PASSENGER CABIN. SUMMARY OF NRC 00640: CORROSION LEVEL 2. LH CUSP WEB STA Y 636 AT PASSENGER CABIN WAS REPAIRED PER B717-2
- [SDR DALA2024030402934](https://openairdocs.org/sdr/DALA2024030402934), Mar 1, 2024: WEB. CORRODED. CORROSION ON WEB (2 EA) OF STA Y=1053 LONGERON 30 AT AFT COMPARTMENT (C2). SUMMARY OF NRC 00638: CORROSION LEVEL 2. SECTIONS OF THE WEB (PREVIOUSLY REPAIRED) WE
- [SDR DALA2024030402931](https://openairdocs.org/sdr/DALA2024030402931), Mar 1, 2024: BEAM. CRACKED. CRACK ON BEAM #1 ON STA 197 AT PASSENGER DOOR 1L. SUMMARY OF NRC 00138: BEAM #1 ON STA 197 AT PASSENGER DOOR 1L WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCE
- [SDR DALA2024022802765](https://openairdocs.org/sdr/DALA2024022802765), Feb 27, 2024: FRAME. CRACKED. CRACK ON FRAME STA Y1037 OVER LONG 17 RH AT CPAX. SUMMARY OF NRC 00409: FRAME STA 1037 OVER LONG 17 RH AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDU
- [SDR DALA2024022602641](https://openairdocs.org/sdr/DALA2024022602641), Feb 25, 2024: BEAM. CRACKED. CRACK ON BEAM #2 ON STA 197 AT PASSENGER DOOR 1L. SUMMARY OF NRC 00139: BEAM #2 ON STA 197 AT PASSENGER DOOR 1L WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCED
- [SDR DALA2024022602639](https://openairdocs.org/sdr/DALA2024022602639), Feb 24, 2024: CUSP WEB. CRACKED. CRACK ON LH CUSP WEB STA 716 AND X44/60 AT CAB PAX. SUMMARY OF NRC 00399: CUSP WEB STA 716 AND X44/60 AT CAB PAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 (FI
- [SDR DALA2024022602635](https://openairdocs.org/sdr/DALA2024022602635), Feb 23, 2024: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK -X=22 BTW STA Y=215-256 PAX CABIN. SUMMARY OF NRC 00580: CORROSION LEVEL 2. SEAT TRACK -X=22 BTW STA Y=215-256 PAX CABIN WAS REPAIRED PE
- [SDR DALA2024022202462](https://openairdocs.org/sdr/DALA2024022202462), Feb 22, 2024: FRAME. CRACKED. CRACK ON FRAME STA Y1037 OVER LONG 17 LH AT CPAX. SUMMARY OF NRC 00408: FRAME STA Y1037 OVER LONG 17 LH AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCED
- [SDR DALA2023083107086](https://openairdocs.org/sdr/DALA2023083107086), Aug 31, 2023: UNKNOWN. UNKNOWN. THE FORWARD OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY B5-121 PER B717 AMM 33-51. OPERATIONAL TEST WAS GOO
- [SDR DALA2023081406583](https://openairdocs.org/sdr/DALA2023081406583), Aug 11, 2023: UNKNOWN. UNKNOWN. THE OVERHEAD LIGHT FIXTURE IN THE FWD GALLEY AT R1 DOOR WITH BUILT-IN EMERGENCY LIGHTING IS MISSING LENS COVER. MAINTENANCE INSTALLED THE MISSING OVERHEAD LIGHT
- [SDR DALA2023080806441](https://openairdocs.org/sdr/DALA2023080806441), Aug 5, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY EXIT COVER DIFFUSER LENS FELL OFF AT AFT CABIN. MAINTENANCE RESECURED LENS COVER PER B717 AMM 33-51. OK FOR SERVICE. (LP #2902779)
- [SDR DALA2023021701234](https://openairdocs.org/sdr/DALA2023021701234), Feb 16, 2023: NONE. NONE. THE F/O SIDE EXIT SIGN AT THE EMERGENCY ROW FELL OFF DURING TURBULENCE. MAINTENANCE RESECURED THE EXIT SIGN LENSE COVER AT THE EMERGENCY EXIT ROW CROWN. (LP #85
- [SDR DALA2023012400523](https://openairdocs.org/sdr/DALA2023012400523), Jan 20, 2023: SPLICE. CRACKED. NOTED CRACK ON RT SIDE 2ND SCREW HOLE BELOW SPLICE 4NE 52.267. AFTER ACCOMPLISHMENT OF SEPARATION OF LAYERS, PERFORMED BHEC IAW STEP 14 OF AA5530-01048-02 AD 26
- [SDR DALA2022100406445](https://openairdocs.org/sdr/DALA2022100406445), Oct 3, 2022: NONE. NONE. THE OVERWING EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MAINTENANCE FOUND A FAULTY POWER SUPPLY. THE POWER SUPPLY B5-125 WAS REPLACED PER B717 AMM 33-51. OPE
- [SDR DALA2022083005818](https://openairdocs.org/sdr/DALA2022083005818), Aug 30, 2022: NONE. NONE. AIRCRAFT 9564, BOTH OVERWING EMERGENCY LIGHTS DO NOT ILLUMINATE. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHTS OVERWING BATTERY. LP 9128322
- [SDR DALA2022061004080](https://openairdocs.org/sdr/DALA2022061004080), Jun 9, 2022: BATTERY. INOPERATIVE. THE EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY AND REPLACED THE BATTERY REF B717 AMM 33-51-01. (LP #9247536)
- [SDR DALA2022051303315](https://openairdocs.org/sdr/DALA2022051303315), May 13, 2022: NONE. NONE. DURING THE SERVICE CHECK, SEVEN EMERGENCY LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED SEVEN EMERGENCY LIGHT BATTERIES IN THE CABIN. O
- [SDR DALA2022031601715](https://openairdocs.org/sdr/DALA2022031601715), Mar 12, 2022: NONE. NONE. FOUND CORROSION ON INTERCOSTAL AFT CARGO BILGE AREA, AFT OF STA 1022, L29R. REPLACED PER BOEING DRAWING 9936718. CORROSION LEVEL 2. (LP #2154330)
- [SDR DALA2022031501676](https://openairdocs.org/sdr/DALA2022031501676), Mar 11, 2022: NONE. NONE. FOUND LIGHT CORROSION BILGE AREA AFT CARGO, STA 1022, FWD AND AFT OF STRINGER, L29 R. "M". SUMMARY SEE NRC 045-0008:5331-2001/001 00357: REPLACED LONGERON AT BI
- [SDR DALA2022031401646](https://openairdocs.org/sdr/DALA2022031401646), Mar 10, 2022: NONE. NONE. TAILCONE SLIDE DATA TAG STATES SLIDE IS OUT OF DATE. OVERHAUL WAS DUE IN DECEMBER 2020. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN 
- [SDR DALA2022031001550](https://openairdocs.org/sdr/DALA2022031001550), Feb 20, 2022: NONE. NONE. RT WING UPPER TRAILING EDGE PANEL DAMAGED FWD OF THE OUTBRD SPOILER OUTBRD HINGE. REMOVED DAMAGED "T" AND WEB ASSY FROM AFT WING SPAR. REPLACED THE "T" AND WEB 
- [SDR DALA2019110606423](https://openairdocs.org/sdr/DALA2019110606423), Nov 5, 2019: LIGHT. DISCONNECTED. ROW 20D CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND THE LIGHT ASSEMBLY DISCONNECTED. ONCE THE LIGHT WAS RECONNECTED THE OPERATION CHECKED GOOD REF B7

All 219: https://openairdocs.org/aircraft/N935AT/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/N935AT/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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