# N937AT: 2001 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [BMW Rolls BR-700 series](https://openairdocs.org/engine/bmw-rolls-br-700-series) (registry code 09500)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55091
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 22, 2001
- Certificate issued: May 22, 2025
- Expires: May 31, 2032
- Mode S code: ACFFBC
- 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=937AT
- Page: https://openairdocs.org/aircraft/N937AT

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/N937AT/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 N937AT.

## FAA accident and incident reports

None matched to N937AT.

## Service difficulty reports (240, 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 DALA2026092905409](https://openairdocs.org/sdr/DALA2026092905409), Sep 28, 2026: DOUBLER. MISINSTALLED. FOUND PCS DOUBLER AT WRONG LOCATION. REPAIRED PER ER/A 637058-14AD. (1837396) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026092805398](https://openairdocs.org/sdr/DALA2026092805398), Sep 26, 2026: SKIN. NOT REPORTED. FUSELAGE CROWN Y503 - Y522, L-1 - L-3R EXISTING DOUBLER NEAR STC INSTALL AREA. REPAIRED PER ER/A 637058-14. (1833937) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026090204947](https://openairdocs.org/sdr/DALA2026090204947), Sep 1, 2026: SKIN. DAMAGED. FOUND DAMAGE AT AFT CARGO DOOR SKIN AFT EDGE. BLENDED MINOR SKIN EDGE DAMAGE FROM AFT CARGO AFT AREA SKIN IAW SRM 51-70-01-2R. (8313198) (AIRCRAFT GROUNDED).
- [SDR DALA2026090204946](https://openairdocs.org/sdr/DALA2026090204946), Sep 1, 2026: SKIN. DAMAGED. RAMP REPORTS DAMAGE ON SKIN EDGE OF AFT CARGO DOOR CUTOUT AFT FUSELAGE SKIN. BLENDED MINOR DAMAGE ON AFT CARGO AFT DOOR SIL IAW SRM 51- 70-01-2R. (8313197) (AIR
- [SDR DALA2026090204945](https://openairdocs.org/sdr/DALA2026090204945), Sep 1, 2026: SKIN. DAMAGED. FOUND DAMAGE ON SKIN EDGE OF AFT CARGO DOOR FWD FUSELAGE SKIN. BLENDED SURFACE IAW SRM 53-01-01-1A-1. (8313196) (AIRCRAFT GROUNDED).
- [SDR DALA2026061903681](https://openairdocs.org/sdr/DALA2026061903681), Jun 19, 2026: TIRE. FAILED. SHIP 9586-ATB- THE FLIGHT CREW REPORTED A SUSPECTED RT MAIN TIRE FAILURE ON TAKEOFF WITH AN ASSOCIATED GEAR UNSAFE LIGHT ILLUMINATED AND RETURNED FROM FLIGHT. R
- [SDR DALA2026060903441](https://openairdocs.org/sdr/DALA2026060903441), Jun 4, 2026: OIL SYSTEM. LEAKING. DIRTY SOCK ODOR ON GROUND AT GATE FROM BOTH PACKS INDEPENDENTLY ON APU AIR. T/S PER FIM 49-50 FOUND OIL INSIDE THE APU PLENUM. R & R COELESSOR BAGS IAW AMM 21-5
- [SDR DALA2026060203346](https://openairdocs.org/sdr/DALA2026060203346), May 31, 2026: OIL SYSTEM. LEAKING. FLIGHT ATTENDANTS REPORTED A MUSTY OR MILDEW SMELL DURING FLIGHT IN THE MID-CABIN. FOUND APU COMPARTMENT CONTAMINATED WITH OIL. REPLACED APU PER AMDS W/C 4900-9
- [SDR DALA2025122309341](https://openairdocs.org/sdr/DALA2025122309341), Dec 20, 2025: HINGE FITTING. CORRODED. CORROSION FOUND ON BOLT SETTLEMENT AREA (INBRD SIDE) AT RT WING FLAP FWD HINGE NR 3. RT FLAP FWD HINGE WAS REPAIRED IAW PRI 631116-14 REV 2, AND ER/A 631116-14 
- [SDR DALA2025122309340](https://openairdocs.org/sdr/DALA2025122309340), Dec 19, 2025: STRAP. CRACKED. CRACKED ANGLE STRAP BTW CANTED BS 1178, L2R AT ROOT OF VERTICAL STABILIZER. REPAIRED IAW SRM 53-30-01-2R -1. (1358667)
- [SDR DALA2025122909451](https://openairdocs.org/sdr/DALA2025122909451), Dec 18, 2025: NOT REPORTED. NOT REPORTED. DTA ER/A 631116-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL. DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-631116 (1359292)
- [SDR DALA2025121709199](https://openairdocs.org/sdr/DALA2025121709199), Dec 16, 2025: LANYARD. FRAYED. FRAYED LANDYARD CABLE FROM L1 SLIDE DOOR. LANYARD CABLE FROM L1 SLIDE DOOR WAS REPLACED AND PART NUMBER WAS VERIFIED PER AIPC 25-61-01 AND INSTALLATION IS ACCOM
- [SDR DALA2025040102422](https://openairdocs.org/sdr/DALA2025040102422), Mar 27, 2025: STRUCTURE. CRACKED. -AD- COMPLIED WITH AMDS CARD 5720-01103-01B. REQUIRES COMPLETION OF PRI 623843-14AD DUE TO CRACK INDICATION FOUND DURING INSP. COMPLIED WITH PRI 623843-14AD REV
- [SDR DALA2025033102349](https://openairdocs.org/sdr/DALA2025033102349), Mar 27, 2025: SPAR. CRACKED. -AD- CRACK FOUND IN LWR AFT LEG OF LWR REAR SPAR JUST OB OF FLAP FITTING @ XRS170 DURING LT WING REAR SPAR INSP AMDS #5720-01103-01A. COMPLIED WITH PRI 623680-1
- [SDR DALA2024060605813](https://openairdocs.org/sdr/DALA2024060605813), Jun 6, 2024: B-NUT. LOOSE. SHIP 9586 -ATB/HYD/DE- THE CREW RETURNED THE AIRCRAFT BACK TO MSP AND DECLARED AN EMERGENCY WITH ATC DURING THE APPROACH DUE TO THE LOSS OF THE RIGHT HYDRAULIC 
- [SDR DALA2024060305737](https://openairdocs.org/sdr/DALA2024060305737), Jun 2, 2024: JACKSCREW. CORRODED. -AD- FOUND CORROSION ON LOWER JACKSCREW THREADS APPROX 6"ABOVE LOWER STOP. SUMMARY SEE NRC 006-0001:2740-01114-05 /002 00007: REPLACED JACK SCREW PER AMDS 2740-
- [SDR DALA2024042204627](https://openairdocs.org/sdr/DALA2024042204627), Apr 20, 2024: BATTERY PACK. MALFUNCTIONED. THE TAIL EXIT LIGHT STAYS FLASHING WITH THE EMERGENCY POWER SWITCH ARMED. MAINTENANCE REPLACED THE BATTERY PACK AND CRADLE ASSEMBLY B5-260 PER B717 AMM 33-51. N
- [SDR DALA2024040103938](https://openairdocs.org/sdr/DALA2024040103938), Mar 29, 2024: GENERATOR. FAILED. SHIP 9586 -DIV- THE FLIGHT WAS DIVERTED TO MCO FOLLOWING THE FAILURE OF THE RIGHT GENERATOR AFTER TAKEOFF, WHILE THE APU GENERATOR WAS ON MEL. THE CAPTAIN DECLA
- [SDR DALA2023122410544](https://openairdocs.org/sdr/DALA2023122410544), Dec 24, 2023: UNKNOWN. UNKNOWN. IMPROPERLY INSTALLATION OF LATCH AND MANUAL DEPLOYMENT HANDLE OF TAIL CONE SLIDE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN CO
- [SDR DALA2023122410542](https://openairdocs.org/sdr/DALA2023122410542), Dec 23, 2023: UNKNOWN. UNKNOWN. CRACKED PLATE ON EMERGENCY DOOR INTERNAL STRUCTURE (MIDDLE SECTION) Y=1053 X=10 AT PAX CABIN. SUMMARY OF NRC 00097: PLATE (WEB) ON EMERGENCY DOOR INTERNAL STRUC
- [SDR DALA2023121510287](https://openairdocs.org/sdr/DALA2023121510287), Dec 13, 2023: UNKNOWN. UNKNOWN. CORROSION ON INNER SKIN ON STA Y 627 BTW LONG 28RH AND LONG 29RH BILGE AREA AT FWD COMPARTMENT. SUMMARY OF NRC 00072: CORROSION LEVEL 2. INNER SKIN ON STA Y 627
- [SDR DALA2023121310200](https://openairdocs.org/sdr/DALA2023121310200), Dec 12, 2023: UNKNOWN. UNKNOWN. CORROSION ON PREVIOUS REPAIR SPLICES ON DOOR JAMB STA Y=954 BTW STRINGER 26-27RH. SUMMARY OF NRC 00698: CORROSION LEVEL 2. PREVIOUS REPAIR SPLICES ON DOOR JAMB 
- [SDR DALA2023121310199](https://openairdocs.org/sdr/DALA2023121310199), Dec 11, 2023: UNKNOWN. UNKNOWN. CORROSION ON LONGERON SPLICE L30 BETWEEN Y=889 AND Y=908, AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00145: CORROSION LEVEL 2. SPLICE ON L30 BETWEEN Y=889 AND Y=9
- [SDR DALA2023121110136](https://openairdocs.org/sdr/DALA2023121110136), Dec 11, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH TRACK ABOVE R=28 BTW STA Y=427+13, Y=446+6 AT LOWER FWD CARGO COMPARTMENT. SUMMARY OF NRC 00068: CORROSION LEVEL 2. RH TRACK ABOVE R=28 BTW STA 
- [SDR DALA2023121110135](https://openairdocs.org/sdr/DALA2023121110135), Dec 11, 2023: UNKNOWN. UNKNOWN. CRACK ON FLOOR BEAM AND BEAM-WEB ATTACHED TO LH FRAME Y=674, X=57 AT PASSENGER CABIN. SUMMARY OF NRC 228: FLOOR BEAM WAS REPLACED PER B-717-200 SRM 51-41-02-0G 
- [SDR DALA2023120710007](https://openairdocs.org/sdr/DALA2023120710007), Dec 7, 2023: UNKNOWN. UNKNOWN. CORROSION ON CUSP ANGLE BTW STA Y 208 TO STA Y 164 SERVICE DOOR (R1) AT PAX CABIN. SUMMARY OF NRC 284: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y 208 TO STA Y 164 
- [SDR DALA2023120710006](https://openairdocs.org/sdr/DALA2023120710006), Dec 6, 2023: UNKNOWN. UNKNOWN. BEND AND CRACK ON CUTOUT UPPER SIDE OF AIR STAIRWELL DOOR AT APPROX STA Y 160 AND BTW LONG 18LH AND LONG 19LH ON FUSELAGE. SUMMARY OF NRC 00126: CUTOUT UPPER SI
- [SDR DALA2023120609978](https://openairdocs.org/sdr/DALA2023120609978), Dec 5, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH SEAT TRACK X=-56 BTW STA Y=215-256 AT PAX CABIN. SUMMARY OF NRC 00494: CORROSION LEVEL 2. RH SEAT TRACK X=-56 BTW STA Y=215-256 AT PAX CABIN WAS
- [SDR DALA2023120609976](https://openairdocs.org/sdr/DALA2023120609976), Dec 5, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH SEAT TRACK X=-44 BTW STA Y=199-256 AT PAX CABIN. SUMMARY OF NRC 0495: CORROSION LEVEL 2. SEAT TRACK X=-44 BTW STA Y=199-256 WAS REPLACED PER B71
- [SDR DALA2023120609975](https://openairdocs.org/sdr/DALA2023120609975), Dec 5, 2023: UNKNOWN. UNKNOWN. CORROSION ON RH CUSP WEB X=-49 TO X=-60 BTW STA 389-408 AT PAX CABIN. SUMMARY OF NRC 00509: CORROSION LEVEL 2. CUSP WEB X=-49 TO X=-60 BTW STA 389-408 AT PAX CA
- [SDR DALA2023120409904](https://openairdocs.org/sdr/DALA2023120409904), Dec 3, 2023: UNKNOWN. UNKNOWN. CORROSION ON LOWER SURFACE OF CUSP WEB STA Y 705 OVER X49 AND STA Y 676 AND X58 LH SIDE AT CPAX. SUMMARY OF NRC 00307: CORROSION LEVEL 2. CUSP WEB STA Y 655 TO 
- [SDR DALA2023120409903](https://openairdocs.org/sdr/DALA2023120409903), Dec 2, 2023: UNKNOWN. UNKNOWN. CORROSION ON LH SEAT TRACK X=22 BTW STA Y=199-256 AT PAX CABIN. SUMMARY OF NRC 00496: CORROSION LEVEL 2. SEAT TRACK X=22 BTW Y=199-265 WAS REPLACED PER DWG 5930
- [SDR DALA2023120409899](https://openairdocs.org/sdr/DALA2023120409899), Dec 2, 2023: UNKNOWN. UNKNOWN. CRACK ON EXTERNAL FUSELAGE SKIN Y=1022 BETWEEN LONGERONS L-8L AND L-7L. SUMMARY OF NRC 00368: EXTERNAL FUSELAGE SKIN Y=1022 BETWEEN LONGERONS L-8L AND L-7L WAS 
- [SDR DALA2023120109872](https://openairdocs.org/sdr/DALA2023120109872), Nov 30, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP WEP STA Y 665, STA Y 674 OVER -X58 RH SIDE AT CPAX. SUMMARY OF NRC 0293: SECTION CUSP WEB STA Y 665, STA Y 674 OVER -X58 RH SIDE AT CPAX WAS REPAI
- [SDR DALA2023112809759](https://openairdocs.org/sdr/DALA2023112809759), Nov 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON INTERCOSTAL BTW STA Y=1022 TO STAY=1037, LONGERON 30 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00543: CORROSION LEVEL 2. INTERCOSTAL BTW STA Y=
- [SDR DALA2023112809758](https://openairdocs.org/sdr/DALA2023112809758), Nov 27, 2023: UNKNOWN. UNKNOWN. CORROSION ON SLIDE LATCHES AT SERVICE DOOR (R1) IN PAX CABIN. SUMMARY OF NRC 00344: CORROSION LEVEL 2. LATCHES FOR SLIDE AT SERVICE DOOR (R1) IN PAX CABIN WERE 
- [SDR DALA2023112809751](https://openairdocs.org/sdr/DALA2023112809751), Nov 26, 2023: UNKNOWN. UNKNOWN. CORROSION ON ANGLE X=-56 RH Y=150/170 AT CABIN PASSENGER IN REF NRC 284. SUMMARY OF NRC 00518: CORROSION LEVEL 2. NEW ANGLE X=-56 RH Y=150/170 AT CABIN PASSENGE
- [SDR DALA2023112709723](https://openairdocs.org/sdr/DALA2023112709723), Nov 24, 2023: UNKNOWN. UNKNOWN. CORROSION ON VERTICAL WEB STA Y199 TO Y205 X 56.0 AT PAX CABIN. SUMMARY OF NRC 00230: CORROSION LEVEL 2. VERTICAL WEB STA Y199 TO Y205 X 56.0 AT PAX CABIN WAS R
- [SDR DALA2023112709717](https://openairdocs.org/sdr/DALA2023112709717), Nov 22, 2023: UNKNOWN. UNKNOWN. CRACK ON CUSP WEB STA Y 715 AND X44 LH SIDE AT CPAX. SUMMARY OF NRC 00305: CUSP WEB STA Y 715 AND X44 LH SIDE AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-
- [SDR DALA2023112209649](https://openairdocs.org/sdr/DALA2023112209649), Nov 21, 2023: UNKNOWN. UNKNOWN. CRACK AT STA 1086.5 AND LONGERON 13RH APROX ON EXTERIOR FUSELAGE. SUMMARY OF NRC 00014: CRACK AT STA 1086.5 AND LONGERON 13RH APROX WAS REPAIRED PER PRI 613146-
- [SDR DALA2023111409350](https://openairdocs.org/sdr/DALA2023111409350), Nov 13, 2023: UNKNOWN. UNKNOWN. CRACK UPPER CAP ON STA Y=1022 AND LONGERON 7 LH SIDE AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00188: UPPER CAP ON STA Y=1022 AND LONGERON 7LH SIDE AT PASSENGER
- [SDR DALA2023111309298](https://openairdocs.org/sdr/DALA2023111309298), Nov 9, 2023: UNKNOWN. UNKNOWN. CORROSION ON PREVIOUS REPAIR ON CUSP WEB RH SIDE ON STA Y 332 AND -X56 AT CPAX. SUMMARY OF NRC 00240: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER ON CUSP WEB RH 
- [SDR DALA2023110409090](https://openairdocs.org/sdr/DALA2023110409090), Nov 4, 2023: UNKNOWN. UNKNOWN. CRACK ON BEAMS (3 EA) OVER BEAM #1 AFT EDGE AND BEAM #2 AFT/FWD EDGE AT FWD PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00128: CRACK ON BEAMS OVER BEAM #1 AFT 
- [SDR DALA2023071305679](https://openairdocs.org/sdr/DALA2023071305679), Jul 12, 2023: UNKNOWN. UNKNOWN. AFT F/A READY LIGHT COVER MISSING. RESECURED AFT F/A EMERGENCY LIGHT LENS COVER PER B717 AMM 33-51. A/C OK FOR SVC. (LP #4984108)
- [SDR DALA2023051203750](https://openairdocs.org/sdr/DALA2023051203750), May 12, 2023: UNKNOWN. UNKNOWN. SEVERAL CABIN EMERGENCY LIGHTS AND THE MID-CABIN EXIT IDENFIER LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD AND MID-CABIN BATTERY PACKS IAW B717 AMM
- [SDR DALA2023050903617](https://openairdocs.org/sdr/DALA2023050903617), May 9, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY LIGHTS ARE INOPERATIVE IN THE CABIN. MAINTENANCE REPLACED THREE EMERGENCY LIGHT BATTERY PACKS PER B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #
- [SDR DALA2022092806347](https://openairdocs.org/sdr/DALA2022092806347), Sep 24, 2022: NONE. NONE. ON INTERIOR WALK-THROUGH, FOUND FORWARD OVERWING EXIT EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED ONE BATTERY PACK ABOVER ROW 19, FOR THE OVERWING 
- [SDR DALA2022071304854](https://openairdocs.org/sdr/DALA2022071304854), Jul 10, 2022: NONE. NONE. MAINTENANCE FOUND THAT THE EMERGENCY LIGHT OVER THE AFT EMERGENCY EXIT WAS NOT WORKING, WHEN PREFORMING LIGHTS TEST. THE POWER SUPPLY ASSOCIATED WITH THE LIGHT 
- [SDR DALA2022050103043](https://openairdocs.org/sdr/DALA2022050103043), Apr 29, 2022: SKIN. CORRODED. PROTUBERANCE PROVOKED BY CORROSION ON EXTERNAL FUSELAGE SKIN STA 650-655 BTW LONG 28LH TO 29LH. SUMMARY OF NRC 00226: LEVEL CORROSION 2, EXTERNAL FUSELAGE SKIN 
- [SDR DALA2022051203283](https://openairdocs.org/sdr/DALA2022051203283), Apr 28, 2022: NONE. NONE. FUSELAGE SKIN AND INTERNAL DOUBLER STA 630 TO 655, L-28R TO L-29L CORROSION & CRACKS. SUBJECT REPAIR REQUIRES FOLLOW-ON REPETITIVE INSPECTIONS. REVISED REPAIR L

All 240: https://openairdocs.org/aircraft/N937AT/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/N937AT/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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